2011-12-02 00:20:02 -04:00
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'''
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MAVLink protocol implementation (auto-generated by mavgen.py)
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Generated from: ardupilotmega.xml,common.xml
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Note: this file has been auto-generated. DO NOT EDIT
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'''
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import struct, array, mavutil, time
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WIRE_PROTOCOL_VERSION = "0.9"
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class MAVLink_header(object):
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'''MAVLink message header'''
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def __init__(self, msgId, mlen=0, seq=0, srcSystem=0, srcComponent=0):
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self.mlen = mlen
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self.seq = seq
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self.srcSystem = srcSystem
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self.srcComponent = srcComponent
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self.msgId = msgId
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def pack(self):
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return struct.pack('BBBBBB', 85, self.mlen, self.seq,
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self.srcSystem, self.srcComponent, self.msgId)
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class MAVLink_message(object):
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'''base MAVLink message class'''
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def __init__(self, msgId, name):
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self._header = MAVLink_header(msgId)
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self._payload = None
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self._msgbuf = None
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self._crc = None
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self._fieldnames = []
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self._type = name
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def get_msgbuf(self):
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return self._msgbuf
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def get_header(self):
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return self._header
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def get_payload(self):
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return self._payload
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def get_crc(self):
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return self._crc
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def get_fieldnames(self):
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return self._fieldnames
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def get_type(self):
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return self._type
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def get_msgId(self):
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return self._header.msgId
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def get_srcSystem(self):
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return self._header.srcSystem
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def get_srcComponent(self):
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return self._header.srcComponent
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def get_seq(self):
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return self._header.seq
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def __str__(self):
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ret = '%s {' % self._type
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for a in self._fieldnames:
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v = getattr(self, a)
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ret += '%s : %s, ' % (a, v)
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ret = ret[0:-2] + '}'
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2011-12-28 17:29:37 -04:00
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return ret
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2011-12-02 00:20:02 -04:00
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def pack(self, mav, crc_extra, payload):
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self._payload = payload
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self._header = MAVLink_header(self._header.msgId, len(payload), mav.seq,
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mav.srcSystem, mav.srcComponent)
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self._msgbuf = self._header.pack() + payload
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crc = mavutil.x25crc(self._msgbuf[1:])
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if False: # using CRC extra
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crc.accumulate(chr(crc_extra))
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self._crc = crc.crc
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self._msgbuf += struct.pack('<H', self._crc)
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return self._msgbuf
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# enums
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# MAV_MOUNT_MODE
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MAV_MOUNT_MODE_RETRACT = 0 # Load and keep safe position (Roll,Pitch,Yaw) from EEPROM and stop
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# stabilization
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MAV_MOUNT_MODE_NEUTRAL = 1 # Load and keep neutral position (Roll,Pitch,Yaw) from EEPROM.
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MAV_MOUNT_MODE_MAVLINK_TARGETING = 2 # Load neutral position and start MAVLink Roll,Pitch,Yaw control with
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# stabilization
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MAV_MOUNT_MODE_RC_TARGETING = 3 # Load neutral position and start RC Roll,Pitch,Yaw control with
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# stabilization
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MAV_MOUNT_MODE_GPS_POINT = 4 # Load neutral position and start to point to Lat,Lon,Alt
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2011-12-28 17:29:37 -04:00
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MAV_MOUNT_MODE_ENUM_END = 5 #
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2011-12-02 00:20:02 -04:00
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# MAV_CMD
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MAV_CMD_NAV_WAYPOINT = 16 # Navigate to waypoint.
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MAV_CMD_NAV_LOITER_UNLIM = 17 # Loiter around this waypoint an unlimited amount of time
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MAV_CMD_NAV_LOITER_TURNS = 18 # Loiter around this waypoint for X turns
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MAV_CMD_NAV_LOITER_TIME = 19 # Loiter around this waypoint for X seconds
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MAV_CMD_NAV_RETURN_TO_LAUNCH = 20 # Return to launch location
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MAV_CMD_NAV_LAND = 21 # Land at location
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MAV_CMD_NAV_TAKEOFF = 22 # Takeoff from ground / hand
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MAV_CMD_NAV_ROI = 80 # Sets the region of interest (ROI) for a sensor set or the
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# vehicle itself. This can then be used by the
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# vehicles control system to
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# control the vehicle attitude and the
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# attitude of various sensors such
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# as cameras.
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MAV_CMD_NAV_PATHPLANNING = 81 # Control autonomous path planning on the MAV.
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MAV_CMD_NAV_LAST = 95 # NOP - This command is only used to mark the upper limit of the
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# NAV/ACTION commands in the enumeration
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MAV_CMD_CONDITION_DELAY = 112 # Delay mission state machine.
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MAV_CMD_CONDITION_CHANGE_ALT = 113 # Ascend/descend at rate. Delay mission state machine until desired
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# altitude reached.
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MAV_CMD_CONDITION_DISTANCE = 114 # Delay mission state machine until within desired distance of next NAV
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# point.
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MAV_CMD_CONDITION_YAW = 115 # Reach a certain target angle.
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MAV_CMD_CONDITION_LAST = 159 # NOP - This command is only used to mark the upper limit of the
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# CONDITION commands in the enumeration
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MAV_CMD_DO_SET_MODE = 176 # Set system mode.
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MAV_CMD_DO_JUMP = 177 # Jump to the desired command in the mission list. Repeat this action
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# only the specified number of times
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MAV_CMD_DO_CHANGE_SPEED = 178 # Change speed and/or throttle set points.
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MAV_CMD_DO_SET_HOME = 179 # Changes the home location either to the current location or a
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# specified location.
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MAV_CMD_DO_SET_PARAMETER = 180 # Set a system parameter. Caution! Use of this command requires
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# knowledge of the numeric enumeration value
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# of the parameter.
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MAV_CMD_DO_SET_RELAY = 181 # Set a relay to a condition.
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MAV_CMD_DO_REPEAT_RELAY = 182 # Cycle a relay on and off for a desired number of cyles with a desired
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# period.
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MAV_CMD_DO_SET_SERVO = 183 # Set a servo to a desired PWM value.
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MAV_CMD_DO_REPEAT_SERVO = 184 # Cycle a between its nominal setting and a desired PWM for a desired
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# number of cycles with a desired period.
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MAV_CMD_DO_CONTROL_VIDEO = 200 # Control onboard camera capturing.
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MAV_CMD_DO_SET_ROI = 201 # Sets the region of interest (ROI) for a sensor set or the
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# vehicle itself. This can then be used by the
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# vehicles control system
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# to control the vehicle attitude and the
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# attitude of various
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# devices such as cameras.
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MAV_CMD_DO_DIGICAM_CONFIGURE = 202 # Mission command to configure an on-board camera controller system.
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MAV_CMD_DO_DIGICAM_CONTROL = 203 # Mission command to control an on-board camera controller system.
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MAV_CMD_DO_MOUNT_CONFIGURE = 204 # Mission command to configure a camera or antenna mount
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MAV_CMD_DO_MOUNT_CONTROL = 205 # Mission command to control a camera or antenna mount
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MAV_CMD_DO_LAST = 240 # NOP - This command is only used to mark the upper limit of the DO
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# commands in the enumeration
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MAV_CMD_PREFLIGHT_CALIBRATION = 241 # Trigger calibration. This command will be only accepted if in pre-
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# flight mode.
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MAV_CMD_PREFLIGHT_STORAGE = 245 # Request storage of different parameter values and logs. This command
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# will be only accepted if in pre-flight mode.
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2011-12-28 17:29:37 -04:00
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MAV_CMD_ENUM_END = 246 #
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# FENCE_ACTION
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FENCE_ACTION_NONE = 0 # Disable fenced mode
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FENCE_ACTION_GUIDED = 1 # Switched to guided mode to return point (fence point 0)
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FENCE_ACTION_ENUM_END = 2 #
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# FENCE_BREACH
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FENCE_BREACH_NONE = 0 # No last fence breach
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FENCE_BREACH_MINALT = 1 # Breached minimum altitude
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FENCE_BREACH_MAXALT = 2 # Breached minimum altitude
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FENCE_BREACH_BOUNDARY = 3 # Breached fence boundary
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FENCE_BREACH_ENUM_END = 4 #
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2011-12-02 00:20:02 -04:00
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# MAV_DATA_STREAM
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MAV_DATA_STREAM_ALL = 0 # Enable all data streams
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MAV_DATA_STREAM_RAW_SENSORS = 1 # Enable IMU_RAW, GPS_RAW, GPS_STATUS packets.
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MAV_DATA_STREAM_EXTENDED_STATUS = 2 # Enable GPS_STATUS, CONTROL_STATUS, AUX_STATUS
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MAV_DATA_STREAM_RC_CHANNELS = 3 # Enable RC_CHANNELS_SCALED, RC_CHANNELS_RAW, SERVO_OUTPUT_RAW
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MAV_DATA_STREAM_RAW_CONTROLLER = 4 # Enable ATTITUDE_CONTROLLER_OUTPUT, POSITION_CONTROLLER_OUTPUT,
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# NAV_CONTROLLER_OUTPUT.
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MAV_DATA_STREAM_POSITION = 6 # Enable LOCAL_POSITION, GLOBAL_POSITION/GLOBAL_POSITION_INT messages.
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MAV_DATA_STREAM_EXTRA1 = 10 # Dependent on the autopilot
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MAV_DATA_STREAM_EXTRA2 = 11 # Dependent on the autopilot
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MAV_DATA_STREAM_EXTRA3 = 12 # Dependent on the autopilot
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2011-12-28 17:29:37 -04:00
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MAV_DATA_STREAM_ENUM_END = 13 #
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2011-12-02 00:20:02 -04:00
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# MAV_ROI
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MAV_ROI_NONE = 0 # No region of interest.
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MAV_ROI_WPNEXT = 1 # Point toward next waypoint.
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MAV_ROI_WPINDEX = 2 # Point toward given waypoint.
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MAV_ROI_LOCATION = 3 # Point toward fixed location.
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MAV_ROI_TARGET = 4 # Point toward of given id.
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2011-12-28 17:29:37 -04:00
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MAV_ROI_ENUM_END = 5 #
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2011-12-02 00:20:02 -04:00
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# message IDs
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MAVLINK_MSG_ID_BAD_DATA = -1
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MAVLINK_MSG_ID_SENSOR_OFFSETS = 150
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MAVLINK_MSG_ID_SET_MAG_OFFSETS = 151
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MAVLINK_MSG_ID_MEMINFO = 152
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MAVLINK_MSG_ID_AP_ADC = 153
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MAVLINK_MSG_ID_DIGICAM_CONFIGURE = 154
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MAVLINK_MSG_ID_DIGICAM_CONTROL = 155
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MAVLINK_MSG_ID_MOUNT_CONFIGURE = 156
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MAVLINK_MSG_ID_MOUNT_CONTROL = 157
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MAVLINK_MSG_ID_MOUNT_STATUS = 158
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2011-12-28 17:29:37 -04:00
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MAVLINK_MSG_ID_FENCE_POINT = 160
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MAVLINK_MSG_ID_FENCE_FETCH_POINT = 161
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MAVLINK_MSG_ID_FENCE_STATUS = 162
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2011-12-02 00:20:02 -04:00
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MAVLINK_MSG_ID_HEARTBEAT = 0
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MAVLINK_MSG_ID_BOOT = 1
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MAVLINK_MSG_ID_SYSTEM_TIME = 2
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MAVLINK_MSG_ID_PING = 3
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MAVLINK_MSG_ID_SYSTEM_TIME_UTC = 4
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MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL = 5
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MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK = 6
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MAVLINK_MSG_ID_AUTH_KEY = 7
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MAVLINK_MSG_ID_ACTION_ACK = 9
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MAVLINK_MSG_ID_ACTION = 10
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MAVLINK_MSG_ID_SET_MODE = 11
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MAVLINK_MSG_ID_SET_NAV_MODE = 12
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MAVLINK_MSG_ID_PARAM_REQUEST_READ = 20
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MAVLINK_MSG_ID_PARAM_REQUEST_LIST = 21
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MAVLINK_MSG_ID_PARAM_VALUE = 22
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MAVLINK_MSG_ID_PARAM_SET = 23
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MAVLINK_MSG_ID_GPS_RAW_INT = 25
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MAVLINK_MSG_ID_SCALED_IMU = 26
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MAVLINK_MSG_ID_GPS_STATUS = 27
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MAVLINK_MSG_ID_RAW_IMU = 28
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MAVLINK_MSG_ID_RAW_PRESSURE = 29
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MAVLINK_MSG_ID_SCALED_PRESSURE = 38
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MAVLINK_MSG_ID_ATTITUDE = 30
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MAVLINK_MSG_ID_LOCAL_POSITION = 31
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MAVLINK_MSG_ID_GLOBAL_POSITION = 33
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MAVLINK_MSG_ID_GPS_RAW = 32
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MAVLINK_MSG_ID_SYS_STATUS = 34
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MAVLINK_MSG_ID_RC_CHANNELS_RAW = 35
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MAVLINK_MSG_ID_RC_CHANNELS_SCALED = 36
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MAVLINK_MSG_ID_SERVO_OUTPUT_RAW = 37
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MAVLINK_MSG_ID_WAYPOINT = 39
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MAVLINK_MSG_ID_WAYPOINT_REQUEST = 40
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MAVLINK_MSG_ID_WAYPOINT_SET_CURRENT = 41
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MAVLINK_MSG_ID_WAYPOINT_CURRENT = 42
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MAVLINK_MSG_ID_WAYPOINT_REQUEST_LIST = 43
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MAVLINK_MSG_ID_WAYPOINT_COUNT = 44
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MAVLINK_MSG_ID_WAYPOINT_CLEAR_ALL = 45
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MAVLINK_MSG_ID_WAYPOINT_REACHED = 46
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MAVLINK_MSG_ID_WAYPOINT_ACK = 47
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MAVLINK_MSG_ID_GPS_SET_GLOBAL_ORIGIN = 48
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MAVLINK_MSG_ID_GPS_LOCAL_ORIGIN_SET = 49
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MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT_SET = 50
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MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT = 51
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MAVLINK_MSG_ID_CONTROL_STATUS = 52
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MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA = 53
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MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA = 54
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MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST = 55
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MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST = 56
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MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT = 57
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MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT = 58
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MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT = 62
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MAVLINK_MSG_ID_POSITION_TARGET = 63
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MAVLINK_MSG_ID_STATE_CORRECTION = 64
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MAVLINK_MSG_ID_SET_ALTITUDE = 65
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MAVLINK_MSG_ID_REQUEST_DATA_STREAM = 66
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MAVLINK_MSG_ID_HIL_STATE = 67
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MAVLINK_MSG_ID_HIL_CONTROLS = 68
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MAVLINK_MSG_ID_MANUAL_CONTROL = 69
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MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE = 70
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MAVLINK_MSG_ID_GLOBAL_POSITION_INT = 73
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MAVLINK_MSG_ID_VFR_HUD = 74
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MAVLINK_MSG_ID_COMMAND = 75
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MAVLINK_MSG_ID_COMMAND_ACK = 76
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MAVLINK_MSG_ID_OPTICAL_FLOW = 100
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MAVLINK_MSG_ID_OBJECT_DETECTION_EVENT = 140
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MAVLINK_MSG_ID_DEBUG_VECT = 251
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MAVLINK_MSG_ID_NAMED_VALUE_FLOAT = 252
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MAVLINK_MSG_ID_NAMED_VALUE_INT = 253
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MAVLINK_MSG_ID_STATUSTEXT = 254
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MAVLINK_MSG_ID_DEBUG = 255
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class MAVLink_sensor_offsets_message(MAVLink_message):
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'''
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Offsets and calibrations values for hardware sensors.
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This makes it easier to debug the calibration process.
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'''
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def __init__(self, mag_ofs_x, mag_ofs_y, mag_ofs_z, mag_declination, raw_press, raw_temp, gyro_cal_x, gyro_cal_y, gyro_cal_z, accel_cal_x, accel_cal_y, accel_cal_z):
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MAVLink_message.__init__(self, MAVLINK_MSG_ID_SENSOR_OFFSETS, 'SENSOR_OFFSETS')
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self._fieldnames = ['mag_ofs_x', 'mag_ofs_y', 'mag_ofs_z', 'mag_declination', 'raw_press', 'raw_temp', 'gyro_cal_x', 'gyro_cal_y', 'gyro_cal_z', 'accel_cal_x', 'accel_cal_y', 'accel_cal_z']
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self.mag_ofs_x = mag_ofs_x
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self.mag_ofs_y = mag_ofs_y
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self.mag_ofs_z = mag_ofs_z
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self.mag_declination = mag_declination
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self.raw_press = raw_press
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self.raw_temp = raw_temp
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self.gyro_cal_x = gyro_cal_x
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self.gyro_cal_y = gyro_cal_y
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self.gyro_cal_z = gyro_cal_z
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self.accel_cal_x = accel_cal_x
|
|
|
|
self.accel_cal_y = accel_cal_y
|
|
|
|
self.accel_cal_z = accel_cal_z
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 143, struct.pack('>hhhfiiffffff', self.mag_ofs_x, self.mag_ofs_y, self.mag_ofs_z, self.mag_declination, self.raw_press, self.raw_temp, self.gyro_cal_x, self.gyro_cal_y, self.gyro_cal_z, self.accel_cal_x, self.accel_cal_y, self.accel_cal_z))
|
|
|
|
|
|
|
|
class MAVLink_set_mag_offsets_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
set the magnetometer offsets
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, mag_ofs_x, mag_ofs_y, mag_ofs_z):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SET_MAG_OFFSETS, 'SET_MAG_OFFSETS')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'mag_ofs_x', 'mag_ofs_y', 'mag_ofs_z']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.mag_ofs_x = mag_ofs_x
|
|
|
|
self.mag_ofs_y = mag_ofs_y
|
|
|
|
self.mag_ofs_z = mag_ofs_z
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 29, struct.pack('>BBhhh', self.target_system, self.target_component, self.mag_ofs_x, self.mag_ofs_y, self.mag_ofs_z))
|
|
|
|
|
|
|
|
class MAVLink_meminfo_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
state of APM memory
|
|
|
|
'''
|
|
|
|
def __init__(self, brkval, freemem):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_MEMINFO, 'MEMINFO')
|
|
|
|
self._fieldnames = ['brkval', 'freemem']
|
|
|
|
self.brkval = brkval
|
|
|
|
self.freemem = freemem
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 208, struct.pack('>HH', self.brkval, self.freemem))
|
|
|
|
|
|
|
|
class MAVLink_ap_adc_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
raw ADC output
|
|
|
|
'''
|
|
|
|
def __init__(self, adc1, adc2, adc3, adc4, adc5, adc6):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_AP_ADC, 'AP_ADC')
|
|
|
|
self._fieldnames = ['adc1', 'adc2', 'adc3', 'adc4', 'adc5', 'adc6']
|
|
|
|
self.adc1 = adc1
|
|
|
|
self.adc2 = adc2
|
|
|
|
self.adc3 = adc3
|
|
|
|
self.adc4 = adc4
|
|
|
|
self.adc5 = adc5
|
|
|
|
self.adc6 = adc6
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 188, struct.pack('>HHHHHH', self.adc1, self.adc2, self.adc3, self.adc4, self.adc5, self.adc6))
|
|
|
|
|
|
|
|
class MAVLink_digicam_configure_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Configure on-board Camera Control System.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, mode, shutter_speed, aperture, iso, exposure_type, command_id, engine_cut_off, extra_param, extra_value):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_DIGICAM_CONFIGURE, 'DIGICAM_CONFIGURE')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'mode', 'shutter_speed', 'aperture', 'iso', 'exposure_type', 'command_id', 'engine_cut_off', 'extra_param', 'extra_value']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.mode = mode
|
|
|
|
self.shutter_speed = shutter_speed
|
|
|
|
self.aperture = aperture
|
|
|
|
self.iso = iso
|
|
|
|
self.exposure_type = exposure_type
|
|
|
|
self.command_id = command_id
|
|
|
|
self.engine_cut_off = engine_cut_off
|
|
|
|
self.extra_param = extra_param
|
|
|
|
self.extra_value = extra_value
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 118, struct.pack('>BBBHBBBBBBf', self.target_system, self.target_component, self.mode, self.shutter_speed, self.aperture, self.iso, self.exposure_type, self.command_id, self.engine_cut_off, self.extra_param, self.extra_value))
|
|
|
|
|
|
|
|
class MAVLink_digicam_control_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Control on-board Camera Control System to take shots.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, session, zoom_pos, zoom_step, focus_lock, shot, command_id, extra_param, extra_value):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_DIGICAM_CONTROL, 'DIGICAM_CONTROL')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'session', 'zoom_pos', 'zoom_step', 'focus_lock', 'shot', 'command_id', 'extra_param', 'extra_value']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.session = session
|
|
|
|
self.zoom_pos = zoom_pos
|
|
|
|
self.zoom_step = zoom_step
|
|
|
|
self.focus_lock = focus_lock
|
|
|
|
self.shot = shot
|
|
|
|
self.command_id = command_id
|
|
|
|
self.extra_param = extra_param
|
|
|
|
self.extra_value = extra_value
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 242, struct.pack('>BBBBbBBBBf', self.target_system, self.target_component, self.session, self.zoom_pos, self.zoom_step, self.focus_lock, self.shot, self.command_id, self.extra_param, self.extra_value))
|
|
|
|
|
|
|
|
class MAVLink_mount_configure_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Message to configure a camera mount, directional antenna, etc.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, mount_mode, stab_roll, stab_pitch, stab_yaw):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_MOUNT_CONFIGURE, 'MOUNT_CONFIGURE')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'mount_mode', 'stab_roll', 'stab_pitch', 'stab_yaw']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.mount_mode = mount_mode
|
|
|
|
self.stab_roll = stab_roll
|
|
|
|
self.stab_pitch = stab_pitch
|
|
|
|
self.stab_yaw = stab_yaw
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 19, struct.pack('>BBBBBB', self.target_system, self.target_component, self.mount_mode, self.stab_roll, self.stab_pitch, self.stab_yaw))
|
|
|
|
|
|
|
|
class MAVLink_mount_control_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Message to control a camera mount, directional antenna, etc.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, input_a, input_b, input_c, save_position):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_MOUNT_CONTROL, 'MOUNT_CONTROL')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'input_a', 'input_b', 'input_c', 'save_position']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.input_a = input_a
|
|
|
|
self.input_b = input_b
|
|
|
|
self.input_c = input_c
|
|
|
|
self.save_position = save_position
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 97, struct.pack('>BBiiiB', self.target_system, self.target_component, self.input_a, self.input_b, self.input_c, self.save_position))
|
|
|
|
|
|
|
|
class MAVLink_mount_status_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Message with some status from APM to GCS about camera or
|
|
|
|
antenna mount
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, pointing_a, pointing_b, pointing_c):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_MOUNT_STATUS, 'MOUNT_STATUS')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'pointing_a', 'pointing_b', 'pointing_c']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.pointing_a = pointing_a
|
|
|
|
self.pointing_b = pointing_b
|
|
|
|
self.pointing_c = pointing_c
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 233, struct.pack('>BBiii', self.target_system, self.target_component, self.pointing_a, self.pointing_b, self.pointing_c))
|
|
|
|
|
2011-12-28 17:29:37 -04:00
|
|
|
class MAVLink_fence_point_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
A fence point. Used to set a point when from GCS
|
|
|
|
-> MAV. Also used to return a point from MAV -> GCS
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, idx, count, lat, lng):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_FENCE_POINT, 'FENCE_POINT')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'idx', 'count', 'lat', 'lng']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.idx = idx
|
|
|
|
self.count = count
|
|
|
|
self.lat = lat
|
|
|
|
self.lng = lng
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 18, struct.pack('>BBBBff', self.target_system, self.target_component, self.idx, self.count, self.lat, self.lng))
|
|
|
|
|
|
|
|
class MAVLink_fence_fetch_point_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Request a current fence point from MAV
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, idx):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_FENCE_FETCH_POINT, 'FENCE_FETCH_POINT')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'idx']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.idx = idx
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 68, struct.pack('>BBB', self.target_system, self.target_component, self.idx))
|
|
|
|
|
|
|
|
class MAVLink_fence_status_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Status of geo-fencing. Sent in extended status
|
|
|
|
stream when fencing enabled
|
|
|
|
'''
|
|
|
|
def __init__(self, breach_status, breach_count, breach_type, breach_time):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_FENCE_STATUS, 'FENCE_STATUS')
|
|
|
|
self._fieldnames = ['breach_status', 'breach_count', 'breach_type', 'breach_time']
|
|
|
|
self.breach_status = breach_status
|
|
|
|
self.breach_count = breach_count
|
|
|
|
self.breach_type = breach_type
|
|
|
|
self.breach_time = breach_time
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 136, struct.pack('>BHBI', self.breach_status, self.breach_count, self.breach_type, self.breach_time))
|
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
class MAVLink_heartbeat_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The heartbeat message shows that a system is present and
|
|
|
|
responding. The type of the MAV and Autopilot hardware allow
|
|
|
|
the receiving system to treat further messages from this
|
|
|
|
system appropriate (e.g. by laying out the user interface
|
|
|
|
based on the autopilot).
|
|
|
|
'''
|
|
|
|
def __init__(self, type, autopilot, mavlink_version):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_HEARTBEAT, 'HEARTBEAT')
|
|
|
|
self._fieldnames = ['type', 'autopilot', 'mavlink_version']
|
|
|
|
self.type = type
|
|
|
|
self.autopilot = autopilot
|
|
|
|
self.mavlink_version = mavlink_version
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 72, struct.pack('>BBB', self.type, self.autopilot, self.mavlink_version))
|
|
|
|
|
|
|
|
class MAVLink_boot_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The boot message indicates that a system is starting. The
|
|
|
|
onboard software version allows to keep track of onboard
|
|
|
|
soft/firmware revisions.
|
|
|
|
'''
|
|
|
|
def __init__(self, version):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_BOOT, 'BOOT')
|
|
|
|
self._fieldnames = ['version']
|
|
|
|
self.version = version
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 39, struct.pack('>I', self.version))
|
|
|
|
|
|
|
|
class MAVLink_system_time_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The system time is the time of the master clock, typically the
|
|
|
|
computer clock of the main onboard computer.
|
|
|
|
'''
|
|
|
|
def __init__(self, time_usec):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SYSTEM_TIME, 'SYSTEM_TIME')
|
|
|
|
self._fieldnames = ['time_usec']
|
|
|
|
self.time_usec = time_usec
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 190, struct.pack('>Q', self.time_usec))
|
|
|
|
|
|
|
|
class MAVLink_ping_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
A ping message either requesting or responding to a ping. This
|
|
|
|
allows to measure the system latencies, including serial port,
|
|
|
|
radio modem and UDP connections.
|
|
|
|
'''
|
|
|
|
def __init__(self, seq, target_system, target_component, time):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_PING, 'PING')
|
|
|
|
self._fieldnames = ['seq', 'target_system', 'target_component', 'time']
|
|
|
|
self.seq = seq
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.time = time
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 92, struct.pack('>IBBQ', self.seq, self.target_system, self.target_component, self.time))
|
|
|
|
|
|
|
|
class MAVLink_system_time_utc_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
UTC date and time from GPS module
|
|
|
|
'''
|
|
|
|
def __init__(self, utc_date, utc_time):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SYSTEM_TIME_UTC, 'SYSTEM_TIME_UTC')
|
|
|
|
self._fieldnames = ['utc_date', 'utc_time']
|
|
|
|
self.utc_date = utc_date
|
|
|
|
self.utc_time = utc_time
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 191, struct.pack('>II', self.utc_date, self.utc_time))
|
|
|
|
|
|
|
|
class MAVLink_change_operator_control_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Request to control this MAV
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, control_request, version, passkey):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL, 'CHANGE_OPERATOR_CONTROL')
|
|
|
|
self._fieldnames = ['target_system', 'control_request', 'version', 'passkey']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.control_request = control_request
|
|
|
|
self.version = version
|
|
|
|
self.passkey = passkey
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 217, struct.pack('>BBB25s', self.target_system, self.control_request, self.version, self.passkey))
|
|
|
|
|
|
|
|
class MAVLink_change_operator_control_ack_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Accept / deny control of this MAV
|
|
|
|
'''
|
|
|
|
def __init__(self, gcs_system_id, control_request, ack):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK, 'CHANGE_OPERATOR_CONTROL_ACK')
|
|
|
|
self._fieldnames = ['gcs_system_id', 'control_request', 'ack']
|
|
|
|
self.gcs_system_id = gcs_system_id
|
|
|
|
self.control_request = control_request
|
|
|
|
self.ack = ack
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 104, struct.pack('>BBB', self.gcs_system_id, self.control_request, self.ack))
|
|
|
|
|
|
|
|
class MAVLink_auth_key_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Emit an encrypted signature / key identifying this system.
|
|
|
|
PLEASE NOTE: This protocol has been kept simple, so
|
|
|
|
transmitting the key requires an encrypted channel for true
|
|
|
|
safety.
|
|
|
|
'''
|
|
|
|
def __init__(self, key):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_AUTH_KEY, 'AUTH_KEY')
|
|
|
|
self._fieldnames = ['key']
|
|
|
|
self.key = key
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 119, struct.pack('>32s', self.key))
|
|
|
|
|
|
|
|
class MAVLink_action_ack_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
This message acknowledges an action. IMPORTANT: The
|
|
|
|
acknowledgement can be also negative, e.g. the MAV rejects a
|
|
|
|
reset message because it is in-flight. The action ids are
|
|
|
|
defined in ENUM MAV_ACTION in mavlink/include/mavlink_types.h
|
|
|
|
'''
|
|
|
|
def __init__(self, action, result):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_ACTION_ACK, 'ACTION_ACK')
|
|
|
|
self._fieldnames = ['action', 'result']
|
|
|
|
self.action = action
|
|
|
|
self.result = result
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 219, struct.pack('>BB', self.action, self.result))
|
|
|
|
|
|
|
|
class MAVLink_action_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
An action message allows to execute a certain onboard action.
|
|
|
|
These include liftoff, land, storing parameters too EEPROM,
|
|
|
|
shutddown, etc. The action ids are defined in ENUM MAV_ACTION
|
|
|
|
in mavlink/include/mavlink_types.h
|
|
|
|
'''
|
|
|
|
def __init__(self, target, target_component, action):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_ACTION, 'ACTION')
|
|
|
|
self._fieldnames = ['target', 'target_component', 'action']
|
|
|
|
self.target = target
|
|
|
|
self.target_component = target_component
|
|
|
|
self.action = action
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 60, struct.pack('>BBB', self.target, self.target_component, self.action))
|
|
|
|
|
|
|
|
class MAVLink_set_mode_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Set the system mode, as defined by enum MAV_MODE in
|
|
|
|
mavlink/include/mavlink_types.h. There is no target component
|
|
|
|
id as the mode is by definition for the overall aircraft, not
|
|
|
|
only for one component.
|
|
|
|
'''
|
|
|
|
def __init__(self, target, mode):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SET_MODE, 'SET_MODE')
|
|
|
|
self._fieldnames = ['target', 'mode']
|
|
|
|
self.target = target
|
|
|
|
self.mode = mode
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 186, struct.pack('>BB', self.target, self.mode))
|
|
|
|
|
|
|
|
class MAVLink_set_nav_mode_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Set the system navigation mode, as defined by enum
|
|
|
|
MAV_NAV_MODE in mavlink/include/mavlink_types.h. The
|
|
|
|
navigation mode applies to the whole aircraft and thus all
|
|
|
|
components.
|
|
|
|
'''
|
|
|
|
def __init__(self, target, nav_mode):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SET_NAV_MODE, 'SET_NAV_MODE')
|
|
|
|
self._fieldnames = ['target', 'nav_mode']
|
|
|
|
self.target = target
|
|
|
|
self.nav_mode = nav_mode
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 10, struct.pack('>BB', self.target, self.nav_mode))
|
|
|
|
|
|
|
|
class MAVLink_param_request_read_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Request to read the onboard parameter with the param_id string
|
|
|
|
id. Onboard parameters are stored as key[const char*] ->
|
|
|
|
value[float]. This allows to send a parameter to any other
|
|
|
|
component (such as the GCS) without the need of previous
|
|
|
|
knowledge of possible parameter names. Thus the same GCS can
|
|
|
|
store different parameters for different autopilots. See also
|
|
|
|
http://qgroundcontrol.org/parameter_interface for a full
|
|
|
|
documentation of QGroundControl and IMU code.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, param_id, param_index):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_PARAM_REQUEST_READ, 'PARAM_REQUEST_READ')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'param_id', 'param_index']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.param_id = param_id
|
|
|
|
self.param_index = param_index
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 89, struct.pack('>BB15sh', self.target_system, self.target_component, self.param_id, self.param_index))
|
|
|
|
|
|
|
|
class MAVLink_param_request_list_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Request all parameters of this component. After his request,
|
|
|
|
all parameters are emitted.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_PARAM_REQUEST_LIST, 'PARAM_REQUEST_LIST')
|
|
|
|
self._fieldnames = ['target_system', 'target_component']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 159, struct.pack('>BB', self.target_system, self.target_component))
|
|
|
|
|
|
|
|
class MAVLink_param_value_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Emit the value of a onboard parameter. The inclusion of
|
|
|
|
param_count and param_index in the message allows the
|
|
|
|
recipient to keep track of received parameters and allows him
|
|
|
|
to re-request missing parameters after a loss or timeout.
|
|
|
|
'''
|
|
|
|
def __init__(self, param_id, param_value, param_count, param_index):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_PARAM_VALUE, 'PARAM_VALUE')
|
|
|
|
self._fieldnames = ['param_id', 'param_value', 'param_count', 'param_index']
|
|
|
|
self.param_id = param_id
|
|
|
|
self.param_value = param_value
|
|
|
|
self.param_count = param_count
|
|
|
|
self.param_index = param_index
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 162, struct.pack('>15sfHH', self.param_id, self.param_value, self.param_count, self.param_index))
|
|
|
|
|
|
|
|
class MAVLink_param_set_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Set a parameter value TEMPORARILY to RAM. It will be reset to
|
|
|
|
default on system reboot. Send the ACTION
|
|
|
|
MAV_ACTION_STORAGE_WRITE to PERMANENTLY write the RAM contents
|
|
|
|
to EEPROM. IMPORTANT: The receiving component should
|
|
|
|
acknowledge the new parameter value by sending a param_value
|
|
|
|
message to all communication partners. This will also ensure
|
|
|
|
that multiple GCS all have an up-to-date list of all
|
|
|
|
parameters. If the sending GCS did not receive a PARAM_VALUE
|
|
|
|
message within its timeout time, it should re-send the
|
|
|
|
PARAM_SET message.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, param_id, param_value):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_PARAM_SET, 'PARAM_SET')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'param_id', 'param_value']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.param_id = param_id
|
|
|
|
self.param_value = param_value
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 121, struct.pack('>BB15sf', self.target_system, self.target_component, self.param_id, self.param_value))
|
|
|
|
|
|
|
|
class MAVLink_gps_raw_int_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The global position, as returned by the Global Positioning
|
|
|
|
System (GPS). This is NOT the global position estimate of the
|
|
|
|
sytem, but rather a RAW sensor value. See message
|
|
|
|
GLOBAL_POSITION for the global position estimate. Coordinate
|
|
|
|
frame is right-handed, Z-axis up (GPS frame)
|
|
|
|
'''
|
|
|
|
def __init__(self, usec, fix_type, lat, lon, alt, eph, epv, v, hdg):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_GPS_RAW_INT, 'GPS_RAW_INT')
|
|
|
|
self._fieldnames = ['usec', 'fix_type', 'lat', 'lon', 'alt', 'eph', 'epv', 'v', 'hdg']
|
|
|
|
self.usec = usec
|
|
|
|
self.fix_type = fix_type
|
|
|
|
self.lat = lat
|
|
|
|
self.lon = lon
|
|
|
|
self.alt = alt
|
|
|
|
self.eph = eph
|
|
|
|
self.epv = epv
|
|
|
|
self.v = v
|
|
|
|
self.hdg = hdg
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 149, struct.pack('>QBiiiffff', self.usec, self.fix_type, self.lat, self.lon, self.alt, self.eph, self.epv, self.v, self.hdg))
|
|
|
|
|
|
|
|
class MAVLink_scaled_imu_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The RAW IMU readings for the usual 9DOF sensor setup. This
|
|
|
|
message should contain the scaled values to the described
|
|
|
|
units
|
|
|
|
'''
|
|
|
|
def __init__(self, usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SCALED_IMU, 'SCALED_IMU')
|
|
|
|
self._fieldnames = ['usec', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag']
|
|
|
|
self.usec = usec
|
|
|
|
self.xacc = xacc
|
|
|
|
self.yacc = yacc
|
|
|
|
self.zacc = zacc
|
|
|
|
self.xgyro = xgyro
|
|
|
|
self.ygyro = ygyro
|
|
|
|
self.zgyro = zgyro
|
|
|
|
self.xmag = xmag
|
|
|
|
self.ymag = ymag
|
|
|
|
self.zmag = zmag
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 222, struct.pack('>Qhhhhhhhhh', self.usec, self.xacc, self.yacc, self.zacc, self.xgyro, self.ygyro, self.zgyro, self.xmag, self.ymag, self.zmag))
|
|
|
|
|
|
|
|
class MAVLink_gps_status_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The positioning status, as reported by GPS. This message is
|
|
|
|
intended to display status information about each satellite
|
|
|
|
visible to the receiver. See message GLOBAL_POSITION for the
|
|
|
|
global position estimate. This message can contain information
|
|
|
|
for up to 20 satellites.
|
|
|
|
'''
|
|
|
|
def __init__(self, satellites_visible, satellite_prn, satellite_used, satellite_elevation, satellite_azimuth, satellite_snr):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_GPS_STATUS, 'GPS_STATUS')
|
|
|
|
self._fieldnames = ['satellites_visible', 'satellite_prn', 'satellite_used', 'satellite_elevation', 'satellite_azimuth', 'satellite_snr']
|
|
|
|
self.satellites_visible = satellites_visible
|
|
|
|
self.satellite_prn = satellite_prn
|
|
|
|
self.satellite_used = satellite_used
|
|
|
|
self.satellite_elevation = satellite_elevation
|
|
|
|
self.satellite_azimuth = satellite_azimuth
|
|
|
|
self.satellite_snr = satellite_snr
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 110, struct.pack('>B20s20s20s20s20s', self.satellites_visible, self.satellite_prn, self.satellite_used, self.satellite_elevation, self.satellite_azimuth, self.satellite_snr))
|
|
|
|
|
|
|
|
class MAVLink_raw_imu_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The RAW IMU readings for the usual 9DOF sensor setup. This
|
|
|
|
message should always contain the true raw values without any
|
|
|
|
scaling to allow data capture and system debugging.
|
|
|
|
'''
|
|
|
|
def __init__(self, usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_RAW_IMU, 'RAW_IMU')
|
|
|
|
self._fieldnames = ['usec', 'xacc', 'yacc', 'zacc', 'xgyro', 'ygyro', 'zgyro', 'xmag', 'ymag', 'zmag']
|
|
|
|
self.usec = usec
|
|
|
|
self.xacc = xacc
|
|
|
|
self.yacc = yacc
|
|
|
|
self.zacc = zacc
|
|
|
|
self.xgyro = xgyro
|
|
|
|
self.ygyro = ygyro
|
|
|
|
self.zgyro = zgyro
|
|
|
|
self.xmag = xmag
|
|
|
|
self.ymag = ymag
|
|
|
|
self.zmag = zmag
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 179, struct.pack('>Qhhhhhhhhh', self.usec, self.xacc, self.yacc, self.zacc, self.xgyro, self.ygyro, self.zgyro, self.xmag, self.ymag, self.zmag))
|
|
|
|
|
|
|
|
class MAVLink_raw_pressure_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The RAW pressure readings for the typical setup of one
|
|
|
|
absolute pressure and one differential pressure sensor. The
|
|
|
|
sensor values should be the raw, UNSCALED ADC values.
|
|
|
|
'''
|
|
|
|
def __init__(self, usec, press_abs, press_diff1, press_diff2, temperature):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_RAW_PRESSURE, 'RAW_PRESSURE')
|
|
|
|
self._fieldnames = ['usec', 'press_abs', 'press_diff1', 'press_diff2', 'temperature']
|
|
|
|
self.usec = usec
|
|
|
|
self.press_abs = press_abs
|
|
|
|
self.press_diff1 = press_diff1
|
|
|
|
self.press_diff2 = press_diff2
|
|
|
|
self.temperature = temperature
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 136, struct.pack('>Qhhhh', self.usec, self.press_abs, self.press_diff1, self.press_diff2, self.temperature))
|
|
|
|
|
|
|
|
class MAVLink_scaled_pressure_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The pressure readings for the typical setup of one absolute
|
|
|
|
and differential pressure sensor. The units are as specified
|
|
|
|
in each field.
|
|
|
|
'''
|
|
|
|
def __init__(self, usec, press_abs, press_diff, temperature):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SCALED_PRESSURE, 'SCALED_PRESSURE')
|
|
|
|
self._fieldnames = ['usec', 'press_abs', 'press_diff', 'temperature']
|
|
|
|
self.usec = usec
|
|
|
|
self.press_abs = press_abs
|
|
|
|
self.press_diff = press_diff
|
|
|
|
self.temperature = temperature
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 229, struct.pack('>Qffh', self.usec, self.press_abs, self.press_diff, self.temperature))
|
|
|
|
|
|
|
|
class MAVLink_attitude_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The attitude in the aeronautical frame (right-handed, Z-down,
|
|
|
|
X-front, Y-right).
|
|
|
|
'''
|
|
|
|
def __init__(self, usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_ATTITUDE, 'ATTITUDE')
|
|
|
|
self._fieldnames = ['usec', 'roll', 'pitch', 'yaw', 'rollspeed', 'pitchspeed', 'yawspeed']
|
|
|
|
self.usec = usec
|
|
|
|
self.roll = roll
|
|
|
|
self.pitch = pitch
|
|
|
|
self.yaw = yaw
|
|
|
|
self.rollspeed = rollspeed
|
|
|
|
self.pitchspeed = pitchspeed
|
|
|
|
self.yawspeed = yawspeed
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 66, struct.pack('>Qffffff', self.usec, self.roll, self.pitch, self.yaw, self.rollspeed, self.pitchspeed, self.yawspeed))
|
|
|
|
|
|
|
|
class MAVLink_local_position_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The filtered local position (e.g. fused computer vision and
|
|
|
|
accelerometers). Coordinate frame is right-handed, Z-axis down
|
|
|
|
(aeronautical frame)
|
|
|
|
'''
|
|
|
|
def __init__(self, usec, x, y, z, vx, vy, vz):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_LOCAL_POSITION, 'LOCAL_POSITION')
|
|
|
|
self._fieldnames = ['usec', 'x', 'y', 'z', 'vx', 'vy', 'vz']
|
|
|
|
self.usec = usec
|
|
|
|
self.x = x
|
|
|
|
self.y = y
|
|
|
|
self.z = z
|
|
|
|
self.vx = vx
|
|
|
|
self.vy = vy
|
|
|
|
self.vz = vz
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 126, struct.pack('>Qffffff', self.usec, self.x, self.y, self.z, self.vx, self.vy, self.vz))
|
|
|
|
|
|
|
|
class MAVLink_global_position_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The filtered global position (e.g. fused GPS and
|
|
|
|
accelerometers). Coordinate frame is right-handed, Z-axis up
|
|
|
|
(GPS frame)
|
|
|
|
'''
|
|
|
|
def __init__(self, usec, lat, lon, alt, vx, vy, vz):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_GLOBAL_POSITION, 'GLOBAL_POSITION')
|
|
|
|
self._fieldnames = ['usec', 'lat', 'lon', 'alt', 'vx', 'vy', 'vz']
|
|
|
|
self.usec = usec
|
|
|
|
self.lat = lat
|
|
|
|
self.lon = lon
|
|
|
|
self.alt = alt
|
|
|
|
self.vx = vx
|
|
|
|
self.vy = vy
|
|
|
|
self.vz = vz
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 147, struct.pack('>Qffffff', self.usec, self.lat, self.lon, self.alt, self.vx, self.vy, self.vz))
|
|
|
|
|
|
|
|
class MAVLink_gps_raw_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The global position, as returned by the Global Positioning
|
|
|
|
System (GPS). This is NOT the global position estimate of the
|
|
|
|
sytem, but rather a RAW sensor value. See message
|
|
|
|
GLOBAL_POSITION for the global position estimate. Coordinate
|
|
|
|
frame is right-handed, Z-axis up (GPS frame)
|
|
|
|
'''
|
|
|
|
def __init__(self, usec, fix_type, lat, lon, alt, eph, epv, v, hdg):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_GPS_RAW, 'GPS_RAW')
|
|
|
|
self._fieldnames = ['usec', 'fix_type', 'lat', 'lon', 'alt', 'eph', 'epv', 'v', 'hdg']
|
|
|
|
self.usec = usec
|
|
|
|
self.fix_type = fix_type
|
|
|
|
self.lat = lat
|
|
|
|
self.lon = lon
|
|
|
|
self.alt = alt
|
|
|
|
self.eph = eph
|
|
|
|
self.epv = epv
|
|
|
|
self.v = v
|
|
|
|
self.hdg = hdg
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 185, struct.pack('>QBfffffff', self.usec, self.fix_type, self.lat, self.lon, self.alt, self.eph, self.epv, self.v, self.hdg))
|
|
|
|
|
|
|
|
class MAVLink_sys_status_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The general system state. If the system is following the
|
|
|
|
MAVLink standard, the system state is mainly defined by three
|
|
|
|
orthogonal states/modes: The system mode, which is either
|
|
|
|
LOCKED (motors shut down and locked), MANUAL (system under RC
|
|
|
|
control), GUIDED (system with autonomous position control,
|
|
|
|
position setpoint controlled manually) or AUTO (system guided
|
|
|
|
by path/waypoint planner). The NAV_MODE defined the current
|
|
|
|
flight state: LIFTOFF (often an open-loop maneuver), LANDING,
|
|
|
|
WAYPOINTS or VECTOR. This represents the internal navigation
|
|
|
|
state machine. The system status shows wether the system is
|
|
|
|
currently active or not and if an emergency occured. During
|
|
|
|
the CRITICAL and EMERGENCY states the MAV is still considered
|
|
|
|
to be active, but should start emergency procedures
|
|
|
|
autonomously. After a failure occured it should first move
|
|
|
|
from active to critical to allow manual intervention and then
|
|
|
|
move to emergency after a certain timeout.
|
|
|
|
'''
|
|
|
|
def __init__(self, mode, nav_mode, status, load, vbat, battery_remaining, packet_drop):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SYS_STATUS, 'SYS_STATUS')
|
|
|
|
self._fieldnames = ['mode', 'nav_mode', 'status', 'load', 'vbat', 'battery_remaining', 'packet_drop']
|
|
|
|
self.mode = mode
|
|
|
|
self.nav_mode = nav_mode
|
|
|
|
self.status = status
|
|
|
|
self.load = load
|
|
|
|
self.vbat = vbat
|
|
|
|
self.battery_remaining = battery_remaining
|
|
|
|
self.packet_drop = packet_drop
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 112, struct.pack('>BBBHHHH', self.mode, self.nav_mode, self.status, self.load, self.vbat, self.battery_remaining, self.packet_drop))
|
|
|
|
|
|
|
|
class MAVLink_rc_channels_raw_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The RAW values of the RC channels received. The standard PPM
|
|
|
|
modulation is as follows: 1000 microseconds: 0%, 2000
|
|
|
|
microseconds: 100%. Individual receivers/transmitters might
|
|
|
|
violate this specification.
|
|
|
|
'''
|
|
|
|
def __init__(self, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, rssi):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_RC_CHANNELS_RAW, 'RC_CHANNELS_RAW')
|
|
|
|
self._fieldnames = ['chan1_raw', 'chan2_raw', 'chan3_raw', 'chan4_raw', 'chan5_raw', 'chan6_raw', 'chan7_raw', 'chan8_raw', 'rssi']
|
|
|
|
self.chan1_raw = chan1_raw
|
|
|
|
self.chan2_raw = chan2_raw
|
|
|
|
self.chan3_raw = chan3_raw
|
|
|
|
self.chan4_raw = chan4_raw
|
|
|
|
self.chan5_raw = chan5_raw
|
|
|
|
self.chan6_raw = chan6_raw
|
|
|
|
self.chan7_raw = chan7_raw
|
|
|
|
self.chan8_raw = chan8_raw
|
|
|
|
self.rssi = rssi
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 252, struct.pack('>HHHHHHHHB', self.chan1_raw, self.chan2_raw, self.chan3_raw, self.chan4_raw, self.chan5_raw, self.chan6_raw, self.chan7_raw, self.chan8_raw, self.rssi))
|
|
|
|
|
|
|
|
class MAVLink_rc_channels_scaled_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The scaled values of the RC channels received. (-100%) -10000,
|
|
|
|
(0%) 0, (100%) 10000
|
|
|
|
'''
|
|
|
|
def __init__(self, chan1_scaled, chan2_scaled, chan3_scaled, chan4_scaled, chan5_scaled, chan6_scaled, chan7_scaled, chan8_scaled, rssi):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_RC_CHANNELS_SCALED, 'RC_CHANNELS_SCALED')
|
|
|
|
self._fieldnames = ['chan1_scaled', 'chan2_scaled', 'chan3_scaled', 'chan4_scaled', 'chan5_scaled', 'chan6_scaled', 'chan7_scaled', 'chan8_scaled', 'rssi']
|
|
|
|
self.chan1_scaled = chan1_scaled
|
|
|
|
self.chan2_scaled = chan2_scaled
|
|
|
|
self.chan3_scaled = chan3_scaled
|
|
|
|
self.chan4_scaled = chan4_scaled
|
|
|
|
self.chan5_scaled = chan5_scaled
|
|
|
|
self.chan6_scaled = chan6_scaled
|
|
|
|
self.chan7_scaled = chan7_scaled
|
|
|
|
self.chan8_scaled = chan8_scaled
|
|
|
|
self.rssi = rssi
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 162, struct.pack('>hhhhhhhhB', self.chan1_scaled, self.chan2_scaled, self.chan3_scaled, self.chan4_scaled, self.chan5_scaled, self.chan6_scaled, self.chan7_scaled, self.chan8_scaled, self.rssi))
|
|
|
|
|
|
|
|
class MAVLink_servo_output_raw_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The RAW values of the servo outputs (for RC input from the
|
|
|
|
remote, use the RC_CHANNELS messages). The standard PPM
|
|
|
|
modulation is as follows: 1000 microseconds: 0%, 2000
|
|
|
|
microseconds: 100%.
|
|
|
|
'''
|
|
|
|
def __init__(self, servo1_raw, servo2_raw, servo3_raw, servo4_raw, servo5_raw, servo6_raw, servo7_raw, servo8_raw):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SERVO_OUTPUT_RAW, 'SERVO_OUTPUT_RAW')
|
|
|
|
self._fieldnames = ['servo1_raw', 'servo2_raw', 'servo3_raw', 'servo4_raw', 'servo5_raw', 'servo6_raw', 'servo7_raw', 'servo8_raw']
|
|
|
|
self.servo1_raw = servo1_raw
|
|
|
|
self.servo2_raw = servo2_raw
|
|
|
|
self.servo3_raw = servo3_raw
|
|
|
|
self.servo4_raw = servo4_raw
|
|
|
|
self.servo5_raw = servo5_raw
|
|
|
|
self.servo6_raw = servo6_raw
|
|
|
|
self.servo7_raw = servo7_raw
|
|
|
|
self.servo8_raw = servo8_raw
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 215, struct.pack('>HHHHHHHH', self.servo1_raw, self.servo2_raw, self.servo3_raw, self.servo4_raw, self.servo5_raw, self.servo6_raw, self.servo7_raw, self.servo8_raw))
|
|
|
|
|
|
|
|
class MAVLink_waypoint_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Message encoding a waypoint. This message is emitted to
|
|
|
|
announce the presence of a waypoint and to set a waypoint
|
|
|
|
on the system. The waypoint can be either in x, y, z meters
|
|
|
|
(type: LOCAL) or x:lat, y:lon, z:altitude. Local frame is
|
|
|
|
Z-down, right handed, global frame is Z-up, right handed
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_WAYPOINT, 'WAYPOINT')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'seq', 'frame', 'command', 'current', 'autocontinue', 'param1', 'param2', 'param3', 'param4', 'x', 'y', 'z']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.seq = seq
|
|
|
|
self.frame = frame
|
|
|
|
self.command = command
|
|
|
|
self.current = current
|
|
|
|
self.autocontinue = autocontinue
|
|
|
|
self.param1 = param1
|
|
|
|
self.param2 = param2
|
|
|
|
self.param3 = param3
|
|
|
|
self.param4 = param4
|
|
|
|
self.x = x
|
|
|
|
self.y = y
|
|
|
|
self.z = z
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 128, struct.pack('>BBHBBBBfffffff', self.target_system, self.target_component, self.seq, self.frame, self.command, self.current, self.autocontinue, self.param1, self.param2, self.param3, self.param4, self.x, self.y, self.z))
|
|
|
|
|
|
|
|
class MAVLink_waypoint_request_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Request the information of the waypoint with the sequence
|
|
|
|
number seq. The response of the system to this message should
|
|
|
|
be a WAYPOINT message.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, seq):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_WAYPOINT_REQUEST, 'WAYPOINT_REQUEST')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'seq']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.seq = seq
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 9, struct.pack('>BBH', self.target_system, self.target_component, self.seq))
|
|
|
|
|
|
|
|
class MAVLink_waypoint_set_current_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Set the waypoint with sequence number seq as current waypoint.
|
|
|
|
This means that the MAV will continue to this waypoint on the
|
|
|
|
shortest path (not following the waypoints in-between).
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, seq):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_WAYPOINT_SET_CURRENT, 'WAYPOINT_SET_CURRENT')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'seq']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.seq = seq
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 106, struct.pack('>BBH', self.target_system, self.target_component, self.seq))
|
|
|
|
|
|
|
|
class MAVLink_waypoint_current_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Message that announces the sequence number of the current
|
|
|
|
active waypoint. The MAV will fly towards this waypoint.
|
|
|
|
'''
|
|
|
|
def __init__(self, seq):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_WAYPOINT_CURRENT, 'WAYPOINT_CURRENT')
|
|
|
|
self._fieldnames = ['seq']
|
|
|
|
self.seq = seq
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 101, struct.pack('>H', self.seq))
|
|
|
|
|
|
|
|
class MAVLink_waypoint_request_list_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Request the overall list of waypoints from the
|
|
|
|
system/component.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_WAYPOINT_REQUEST_LIST, 'WAYPOINT_REQUEST_LIST')
|
|
|
|
self._fieldnames = ['target_system', 'target_component']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 213, struct.pack('>BB', self.target_system, self.target_component))
|
|
|
|
|
|
|
|
class MAVLink_waypoint_count_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
This message is emitted as response to WAYPOINT_REQUEST_LIST
|
|
|
|
by the MAV. The GCS can then request the individual waypoints
|
|
|
|
based on the knowledge of the total number of waypoints.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, count):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_WAYPOINT_COUNT, 'WAYPOINT_COUNT')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'count']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.count = count
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 4, struct.pack('>BBH', self.target_system, self.target_component, self.count))
|
|
|
|
|
|
|
|
class MAVLink_waypoint_clear_all_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Delete all waypoints at once.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_WAYPOINT_CLEAR_ALL, 'WAYPOINT_CLEAR_ALL')
|
|
|
|
self._fieldnames = ['target_system', 'target_component']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 229, struct.pack('>BB', self.target_system, self.target_component))
|
|
|
|
|
|
|
|
class MAVLink_waypoint_reached_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
A certain waypoint has been reached. The system will either
|
|
|
|
hold this position (or circle on the orbit) or (if the
|
|
|
|
autocontinue on the WP was set) continue to the next waypoint.
|
|
|
|
'''
|
|
|
|
def __init__(self, seq):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_WAYPOINT_REACHED, 'WAYPOINT_REACHED')
|
|
|
|
self._fieldnames = ['seq']
|
|
|
|
self.seq = seq
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 21, struct.pack('>H', self.seq))
|
|
|
|
|
|
|
|
class MAVLink_waypoint_ack_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Ack message during waypoint handling. The type field states if
|
|
|
|
this message is a positive ack (type=0) or if an error
|
|
|
|
happened (type=non-zero).
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, type):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_WAYPOINT_ACK, 'WAYPOINT_ACK')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'type']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.type = type
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 214, struct.pack('>BBB', self.target_system, self.target_component, self.type))
|
|
|
|
|
|
|
|
class MAVLink_gps_set_global_origin_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
As local waypoints exist, the global waypoint reference allows
|
|
|
|
to transform between the local coordinate frame and the global
|
|
|
|
(GPS) coordinate frame. This can be necessary when e.g. in-
|
|
|
|
and outdoor settings are connected and the MAV should move
|
|
|
|
from in- to outdoor.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, latitude, longitude, altitude):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_GPS_SET_GLOBAL_ORIGIN, 'GPS_SET_GLOBAL_ORIGIN')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'latitude', 'longitude', 'altitude']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.latitude = latitude
|
|
|
|
self.longitude = longitude
|
|
|
|
self.altitude = altitude
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 215, struct.pack('>BBiii', self.target_system, self.target_component, self.latitude, self.longitude, self.altitude))
|
|
|
|
|
|
|
|
class MAVLink_gps_local_origin_set_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Once the MAV sets a new GPS-Local correspondence, this message
|
|
|
|
announces the origin (0,0,0) position
|
|
|
|
'''
|
|
|
|
def __init__(self, latitude, longitude, altitude):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_GPS_LOCAL_ORIGIN_SET, 'GPS_LOCAL_ORIGIN_SET')
|
|
|
|
self._fieldnames = ['latitude', 'longitude', 'altitude']
|
|
|
|
self.latitude = latitude
|
|
|
|
self.longitude = longitude
|
|
|
|
self.altitude = altitude
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 14, struct.pack('>iii', self.latitude, self.longitude, self.altitude))
|
|
|
|
|
|
|
|
class MAVLink_local_position_setpoint_set_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Set the setpoint for a local position controller. This is the
|
|
|
|
position in local coordinates the MAV should fly to. This
|
|
|
|
message is sent by the path/waypoint planner to the onboard
|
|
|
|
position controller. As some MAVs have a degree of freedom in
|
|
|
|
yaw (e.g. all helicopters/quadrotors), the desired yaw angle
|
|
|
|
is part of the message.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, x, y, z, yaw):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT_SET, 'LOCAL_POSITION_SETPOINT_SET')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'x', 'y', 'z', 'yaw']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.x = x
|
|
|
|
self.y = y
|
|
|
|
self.z = z
|
|
|
|
self.yaw = yaw
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 206, struct.pack('>BBffff', self.target_system, self.target_component, self.x, self.y, self.z, self.yaw))
|
|
|
|
|
|
|
|
class MAVLink_local_position_setpoint_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Transmit the current local setpoint of the controller to other
|
|
|
|
MAVs (collision avoidance) and to the GCS.
|
|
|
|
'''
|
|
|
|
def __init__(self, x, y, z, yaw):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT, 'LOCAL_POSITION_SETPOINT')
|
|
|
|
self._fieldnames = ['x', 'y', 'z', 'yaw']
|
|
|
|
self.x = x
|
|
|
|
self.y = y
|
|
|
|
self.z = z
|
|
|
|
self.yaw = yaw
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 50, struct.pack('>ffff', self.x, self.y, self.z, self.yaw))
|
|
|
|
|
|
|
|
class MAVLink_control_status_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
|
|
|
|
'''
|
|
|
|
def __init__(self, position_fix, vision_fix, gps_fix, ahrs_health, control_att, control_pos_xy, control_pos_z, control_pos_yaw):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_CONTROL_STATUS, 'CONTROL_STATUS')
|
|
|
|
self._fieldnames = ['position_fix', 'vision_fix', 'gps_fix', 'ahrs_health', 'control_att', 'control_pos_xy', 'control_pos_z', 'control_pos_yaw']
|
|
|
|
self.position_fix = position_fix
|
|
|
|
self.vision_fix = vision_fix
|
|
|
|
self.gps_fix = gps_fix
|
|
|
|
self.ahrs_health = ahrs_health
|
|
|
|
self.control_att = control_att
|
|
|
|
self.control_pos_xy = control_pos_xy
|
|
|
|
self.control_pos_z = control_pos_z
|
|
|
|
self.control_pos_yaw = control_pos_yaw
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 157, struct.pack('>BBBBBBBB', self.position_fix, self.vision_fix, self.gps_fix, self.ahrs_health, self.control_att, self.control_pos_xy, self.control_pos_z, self.control_pos_yaw))
|
|
|
|
|
|
|
|
class MAVLink_safety_set_allowed_area_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Set a safety zone (volume), which is defined by two corners of
|
|
|
|
a cube. This message can be used to tell the MAV which
|
|
|
|
setpoints/waypoints to accept and which to reject. Safety
|
|
|
|
areas are often enforced by national or competition
|
|
|
|
regulations.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, frame, p1x, p1y, p1z, p2x, p2y, p2z):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA, 'SAFETY_SET_ALLOWED_AREA')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'frame', 'p1x', 'p1y', 'p1z', 'p2x', 'p2y', 'p2z']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.frame = frame
|
|
|
|
self.p1x = p1x
|
|
|
|
self.p1y = p1y
|
|
|
|
self.p1z = p1z
|
|
|
|
self.p2x = p2x
|
|
|
|
self.p2y = p2y
|
|
|
|
self.p2z = p2z
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 126, struct.pack('>BBBffffff', self.target_system, self.target_component, self.frame, self.p1x, self.p1y, self.p1z, self.p2x, self.p2y, self.p2z))
|
|
|
|
|
|
|
|
class MAVLink_safety_allowed_area_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Read out the safety zone the MAV currently assumes.
|
|
|
|
'''
|
|
|
|
def __init__(self, frame, p1x, p1y, p1z, p2x, p2y, p2z):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA, 'SAFETY_ALLOWED_AREA')
|
|
|
|
self._fieldnames = ['frame', 'p1x', 'p1y', 'p1z', 'p2x', 'p2y', 'p2z']
|
|
|
|
self.frame = frame
|
|
|
|
self.p1x = p1x
|
|
|
|
self.p1y = p1y
|
|
|
|
self.p1z = p1z
|
|
|
|
self.p2x = p2x
|
|
|
|
self.p2y = p2y
|
|
|
|
self.p2z = p2z
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 108, struct.pack('>Bffffff', self.frame, self.p1x, self.p1y, self.p1z, self.p2x, self.p2y, self.p2z))
|
|
|
|
|
|
|
|
class MAVLink_set_roll_pitch_yaw_thrust_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Set roll, pitch and yaw.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, roll, pitch, yaw, thrust):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST, 'SET_ROLL_PITCH_YAW_THRUST')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'roll', 'pitch', 'yaw', 'thrust']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.roll = roll
|
|
|
|
self.pitch = pitch
|
|
|
|
self.yaw = yaw
|
|
|
|
self.thrust = thrust
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 213, struct.pack('>BBffff', self.target_system, self.target_component, self.roll, self.pitch, self.yaw, self.thrust))
|
|
|
|
|
|
|
|
class MAVLink_set_roll_pitch_yaw_speed_thrust_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Set roll, pitch and yaw.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, roll_speed, pitch_speed, yaw_speed, thrust):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST, 'SET_ROLL_PITCH_YAW_SPEED_THRUST')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'roll_speed', 'pitch_speed', 'yaw_speed', 'thrust']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.roll_speed = roll_speed
|
|
|
|
self.pitch_speed = pitch_speed
|
|
|
|
self.yaw_speed = yaw_speed
|
|
|
|
self.thrust = thrust
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 95, struct.pack('>BBffff', self.target_system, self.target_component, self.roll_speed, self.pitch_speed, self.yaw_speed, self.thrust))
|
|
|
|
|
|
|
|
class MAVLink_roll_pitch_yaw_thrust_setpoint_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Setpoint in roll, pitch, yaw currently active on the system.
|
|
|
|
'''
|
|
|
|
def __init__(self, time_us, roll, pitch, yaw, thrust):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT, 'ROLL_PITCH_YAW_THRUST_SETPOINT')
|
|
|
|
self._fieldnames = ['time_us', 'roll', 'pitch', 'yaw', 'thrust']
|
|
|
|
self.time_us = time_us
|
|
|
|
self.roll = roll
|
|
|
|
self.pitch = pitch
|
|
|
|
self.yaw = yaw
|
|
|
|
self.thrust = thrust
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 5, struct.pack('>Qffff', self.time_us, self.roll, self.pitch, self.yaw, self.thrust))
|
|
|
|
|
|
|
|
class MAVLink_roll_pitch_yaw_speed_thrust_setpoint_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Setpoint in rollspeed, pitchspeed, yawspeed currently active
|
|
|
|
on the system.
|
|
|
|
'''
|
|
|
|
def __init__(self, time_us, roll_speed, pitch_speed, yaw_speed, thrust):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT, 'ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT')
|
|
|
|
self._fieldnames = ['time_us', 'roll_speed', 'pitch_speed', 'yaw_speed', 'thrust']
|
|
|
|
self.time_us = time_us
|
|
|
|
self.roll_speed = roll_speed
|
|
|
|
self.pitch_speed = pitch_speed
|
|
|
|
self.yaw_speed = yaw_speed
|
|
|
|
self.thrust = thrust
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 127, struct.pack('>Qffff', self.time_us, self.roll_speed, self.pitch_speed, self.yaw_speed, self.thrust))
|
|
|
|
|
|
|
|
class MAVLink_nav_controller_output_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Outputs of the APM navigation controller. The primary use of
|
|
|
|
this message is to check the response and signs of the
|
|
|
|
controller before actual flight and to assist with tuning
|
|
|
|
controller parameters
|
|
|
|
'''
|
|
|
|
def __init__(self, nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT, 'NAV_CONTROLLER_OUTPUT')
|
|
|
|
self._fieldnames = ['nav_roll', 'nav_pitch', 'nav_bearing', 'target_bearing', 'wp_dist', 'alt_error', 'aspd_error', 'xtrack_error']
|
|
|
|
self.nav_roll = nav_roll
|
|
|
|
self.nav_pitch = nav_pitch
|
|
|
|
self.nav_bearing = nav_bearing
|
|
|
|
self.target_bearing = target_bearing
|
|
|
|
self.wp_dist = wp_dist
|
|
|
|
self.alt_error = alt_error
|
|
|
|
self.aspd_error = aspd_error
|
|
|
|
self.xtrack_error = xtrack_error
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 57, struct.pack('>ffhhHfff', self.nav_roll, self.nav_pitch, self.nav_bearing, self.target_bearing, self.wp_dist, self.alt_error, self.aspd_error, self.xtrack_error))
|
|
|
|
|
|
|
|
class MAVLink_position_target_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The goal position of the system. This position is the input to
|
|
|
|
any navigation or path planning algorithm and does NOT
|
|
|
|
represent the current controller setpoint.
|
|
|
|
'''
|
|
|
|
def __init__(self, x, y, z, yaw):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_POSITION_TARGET, 'POSITION_TARGET')
|
|
|
|
self._fieldnames = ['x', 'y', 'z', 'yaw']
|
|
|
|
self.x = x
|
|
|
|
self.y = y
|
|
|
|
self.z = z
|
|
|
|
self.yaw = yaw
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 126, struct.pack('>ffff', self.x, self.y, self.z, self.yaw))
|
|
|
|
|
|
|
|
class MAVLink_state_correction_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Corrects the systems state by adding an error correction term
|
|
|
|
to the position and velocity, and by rotating the attitude by
|
|
|
|
a correction angle.
|
|
|
|
'''
|
|
|
|
def __init__(self, xErr, yErr, zErr, rollErr, pitchErr, yawErr, vxErr, vyErr, vzErr):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_STATE_CORRECTION, 'STATE_CORRECTION')
|
|
|
|
self._fieldnames = ['xErr', 'yErr', 'zErr', 'rollErr', 'pitchErr', 'yawErr', 'vxErr', 'vyErr', 'vzErr']
|
|
|
|
self.xErr = xErr
|
|
|
|
self.yErr = yErr
|
|
|
|
self.zErr = zErr
|
|
|
|
self.rollErr = rollErr
|
|
|
|
self.pitchErr = pitchErr
|
|
|
|
self.yawErr = yawErr
|
|
|
|
self.vxErr = vxErr
|
|
|
|
self.vyErr = vyErr
|
|
|
|
self.vzErr = vzErr
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 130, struct.pack('>fffffffff', self.xErr, self.yErr, self.zErr, self.rollErr, self.pitchErr, self.yawErr, self.vxErr, self.vyErr, self.vzErr))
|
|
|
|
|
|
|
|
class MAVLink_set_altitude_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
|
|
|
|
'''
|
|
|
|
def __init__(self, target, mode):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_SET_ALTITUDE, 'SET_ALTITUDE')
|
|
|
|
self._fieldnames = ['target', 'mode']
|
|
|
|
self.target = target
|
|
|
|
self.mode = mode
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 119, struct.pack('>BI', self.target, self.mode))
|
|
|
|
|
|
|
|
class MAVLink_request_data_stream_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, req_stream_id, req_message_rate, start_stop):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_REQUEST_DATA_STREAM, 'REQUEST_DATA_STREAM')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'req_stream_id', 'req_message_rate', 'start_stop']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.req_stream_id = req_stream_id
|
|
|
|
self.req_message_rate = req_message_rate
|
|
|
|
self.start_stop = start_stop
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 193, struct.pack('>BBBHB', self.target_system, self.target_component, self.req_stream_id, self.req_message_rate, self.start_stop))
|
|
|
|
|
|
|
|
class MAVLink_hil_state_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
This packet is useful for high throughput
|
|
|
|
applications such as hardware in the loop simulations.
|
|
|
|
'''
|
|
|
|
def __init__(self, usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, xacc, yacc, zacc):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_HIL_STATE, 'HIL_STATE')
|
|
|
|
self._fieldnames = ['usec', 'roll', 'pitch', 'yaw', 'rollspeed', 'pitchspeed', 'yawspeed', 'lat', 'lon', 'alt', 'vx', 'vy', 'vz', 'xacc', 'yacc', 'zacc']
|
|
|
|
self.usec = usec
|
|
|
|
self.roll = roll
|
|
|
|
self.pitch = pitch
|
|
|
|
self.yaw = yaw
|
|
|
|
self.rollspeed = rollspeed
|
|
|
|
self.pitchspeed = pitchspeed
|
|
|
|
self.yawspeed = yawspeed
|
|
|
|
self.lat = lat
|
|
|
|
self.lon = lon
|
|
|
|
self.alt = alt
|
|
|
|
self.vx = vx
|
|
|
|
self.vy = vy
|
|
|
|
self.vz = vz
|
|
|
|
self.xacc = xacc
|
|
|
|
self.yacc = yacc
|
|
|
|
self.zacc = zacc
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 191, struct.pack('>Qffffffiiihhhhhh', self.usec, self.roll, self.pitch, self.yaw, self.rollspeed, self.pitchspeed, self.yawspeed, self.lat, self.lon, self.alt, self.vx, self.vy, self.vz, self.xacc, self.yacc, self.zacc))
|
|
|
|
|
|
|
|
class MAVLink_hil_controls_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Hardware in the loop control outputs
|
|
|
|
'''
|
|
|
|
def __init__(self, time_us, roll_ailerons, pitch_elevator, yaw_rudder, throttle, mode, nav_mode):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_HIL_CONTROLS, 'HIL_CONTROLS')
|
|
|
|
self._fieldnames = ['time_us', 'roll_ailerons', 'pitch_elevator', 'yaw_rudder', 'throttle', 'mode', 'nav_mode']
|
|
|
|
self.time_us = time_us
|
|
|
|
self.roll_ailerons = roll_ailerons
|
|
|
|
self.pitch_elevator = pitch_elevator
|
|
|
|
self.yaw_rudder = yaw_rudder
|
|
|
|
self.throttle = throttle
|
|
|
|
self.mode = mode
|
|
|
|
self.nav_mode = nav_mode
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 236, struct.pack('>QffffBB', self.time_us, self.roll_ailerons, self.pitch_elevator, self.yaw_rudder, self.throttle, self.mode, self.nav_mode))
|
|
|
|
|
|
|
|
class MAVLink_manual_control_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
|
|
|
|
'''
|
|
|
|
def __init__(self, target, roll, pitch, yaw, thrust, roll_manual, pitch_manual, yaw_manual, thrust_manual):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_MANUAL_CONTROL, 'MANUAL_CONTROL')
|
|
|
|
self._fieldnames = ['target', 'roll', 'pitch', 'yaw', 'thrust', 'roll_manual', 'pitch_manual', 'yaw_manual', 'thrust_manual']
|
|
|
|
self.target = target
|
|
|
|
self.roll = roll
|
|
|
|
self.pitch = pitch
|
|
|
|
self.yaw = yaw
|
|
|
|
self.thrust = thrust
|
|
|
|
self.roll_manual = roll_manual
|
|
|
|
self.pitch_manual = pitch_manual
|
|
|
|
self.yaw_manual = yaw_manual
|
|
|
|
self.thrust_manual = thrust_manual
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 158, struct.pack('>BffffBBBB', self.target, self.roll, self.pitch, self.yaw, self.thrust, self.roll_manual, self.pitch_manual, self.yaw_manual, self.thrust_manual))
|
|
|
|
|
|
|
|
class MAVLink_rc_channels_override_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The RAW values of the RC channels sent to the MAV to override
|
|
|
|
info received from the RC radio. A value of -1 means no change
|
|
|
|
to that channel. A value of 0 means control of that channel
|
|
|
|
should be released back to the RC radio. The standard PPM
|
|
|
|
modulation is as follows: 1000 microseconds: 0%, 2000
|
|
|
|
microseconds: 100%. Individual receivers/transmitters might
|
|
|
|
violate this specification.
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE, 'RC_CHANNELS_OVERRIDE')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'chan1_raw', 'chan2_raw', 'chan3_raw', 'chan4_raw', 'chan5_raw', 'chan6_raw', 'chan7_raw', 'chan8_raw']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.chan1_raw = chan1_raw
|
|
|
|
self.chan2_raw = chan2_raw
|
|
|
|
self.chan3_raw = chan3_raw
|
|
|
|
self.chan4_raw = chan4_raw
|
|
|
|
self.chan5_raw = chan5_raw
|
|
|
|
self.chan6_raw = chan6_raw
|
|
|
|
self.chan7_raw = chan7_raw
|
|
|
|
self.chan8_raw = chan8_raw
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 143, struct.pack('>BBHHHHHHHH', self.target_system, self.target_component, self.chan1_raw, self.chan2_raw, self.chan3_raw, self.chan4_raw, self.chan5_raw, self.chan6_raw, self.chan7_raw, self.chan8_raw))
|
|
|
|
|
|
|
|
class MAVLink_global_position_int_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
The filtered global position (e.g. fused GPS and
|
|
|
|
accelerometers). The position is in GPS-frame (right-handed,
|
|
|
|
Z-up)
|
|
|
|
'''
|
|
|
|
def __init__(self, lat, lon, alt, vx, vy, vz):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_GLOBAL_POSITION_INT, 'GLOBAL_POSITION_INT')
|
|
|
|
self._fieldnames = ['lat', 'lon', 'alt', 'vx', 'vy', 'vz']
|
|
|
|
self.lat = lat
|
|
|
|
self.lon = lon
|
|
|
|
self.alt = alt
|
|
|
|
self.vx = vx
|
|
|
|
self.vy = vy
|
|
|
|
self.vz = vz
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 104, struct.pack('>iiihhh', self.lat, self.lon, self.alt, self.vx, self.vy, self.vz))
|
|
|
|
|
|
|
|
class MAVLink_vfr_hud_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Metrics typically displayed on a HUD for fixed wing aircraft
|
|
|
|
'''
|
|
|
|
def __init__(self, airspeed, groundspeed, heading, throttle, alt, climb):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_VFR_HUD, 'VFR_HUD')
|
|
|
|
self._fieldnames = ['airspeed', 'groundspeed', 'heading', 'throttle', 'alt', 'climb']
|
|
|
|
self.airspeed = airspeed
|
|
|
|
self.groundspeed = groundspeed
|
|
|
|
self.heading = heading
|
|
|
|
self.throttle = throttle
|
|
|
|
self.alt = alt
|
|
|
|
self.climb = climb
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 123, struct.pack('>ffhHff', self.airspeed, self.groundspeed, self.heading, self.throttle, self.alt, self.climb))
|
|
|
|
|
|
|
|
class MAVLink_command_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Send a command with up to four parameters to the MAV
|
|
|
|
'''
|
|
|
|
def __init__(self, target_system, target_component, command, confirmation, param1, param2, param3, param4):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_COMMAND, 'COMMAND')
|
|
|
|
self._fieldnames = ['target_system', 'target_component', 'command', 'confirmation', 'param1', 'param2', 'param3', 'param4']
|
|
|
|
self.target_system = target_system
|
|
|
|
self.target_component = target_component
|
|
|
|
self.command = command
|
|
|
|
self.confirmation = confirmation
|
|
|
|
self.param1 = param1
|
|
|
|
self.param2 = param2
|
|
|
|
self.param3 = param3
|
|
|
|
self.param4 = param4
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 131, struct.pack('>BBBBffff', self.target_system, self.target_component, self.command, self.confirmation, self.param1, self.param2, self.param3, self.param4))
|
|
|
|
|
|
|
|
class MAVLink_command_ack_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Report status of a command. Includes feedback wether the
|
|
|
|
command was executed
|
|
|
|
'''
|
|
|
|
def __init__(self, command, result):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_COMMAND_ACK, 'COMMAND_ACK')
|
|
|
|
self._fieldnames = ['command', 'result']
|
|
|
|
self.command = command
|
|
|
|
self.result = result
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 8, struct.pack('>ff', self.command, self.result))
|
|
|
|
|
|
|
|
class MAVLink_optical_flow_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Optical flow from a flow sensor (e.g. optical mouse sensor)
|
|
|
|
'''
|
|
|
|
def __init__(self, time, sensor_id, flow_x, flow_y, quality, ground_distance):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_OPTICAL_FLOW, 'OPTICAL_FLOW')
|
|
|
|
self._fieldnames = ['time', 'sensor_id', 'flow_x', 'flow_y', 'quality', 'ground_distance']
|
|
|
|
self.time = time
|
|
|
|
self.sensor_id = sensor_id
|
|
|
|
self.flow_x = flow_x
|
|
|
|
self.flow_y = flow_y
|
|
|
|
self.quality = quality
|
|
|
|
self.ground_distance = ground_distance
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 174, struct.pack('>QBhhBf', self.time, self.sensor_id, self.flow_x, self.flow_y, self.quality, self.ground_distance))
|
|
|
|
|
|
|
|
class MAVLink_object_detection_event_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Object has been detected
|
|
|
|
'''
|
|
|
|
def __init__(self, time, object_id, type, name, quality, bearing, distance):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_OBJECT_DETECTION_EVENT, 'OBJECT_DETECTION_EVENT')
|
|
|
|
self._fieldnames = ['time', 'object_id', 'type', 'name', 'quality', 'bearing', 'distance']
|
|
|
|
self.time = time
|
|
|
|
self.object_id = object_id
|
|
|
|
self.type = type
|
|
|
|
self.name = name
|
|
|
|
self.quality = quality
|
|
|
|
self.bearing = bearing
|
|
|
|
self.distance = distance
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 155, struct.pack('>IHB20sBff', self.time, self.object_id, self.type, self.name, self.quality, self.bearing, self.distance))
|
|
|
|
|
|
|
|
class MAVLink_debug_vect_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
|
|
|
|
'''
|
|
|
|
def __init__(self, name, usec, x, y, z):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_DEBUG_VECT, 'DEBUG_VECT')
|
|
|
|
self._fieldnames = ['name', 'usec', 'x', 'y', 'z']
|
|
|
|
self.name = name
|
|
|
|
self.usec = usec
|
|
|
|
self.x = x
|
|
|
|
self.y = y
|
|
|
|
self.z = z
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 178, struct.pack('>10sQfff', self.name, self.usec, self.x, self.y, self.z))
|
|
|
|
|
|
|
|
class MAVLink_named_value_float_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Send a key-value pair as float. The use of this message is
|
|
|
|
discouraged for normal packets, but a quite efficient way for
|
|
|
|
testing new messages and getting experimental debug output.
|
|
|
|
'''
|
|
|
|
def __init__(self, name, value):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_NAMED_VALUE_FLOAT, 'NAMED_VALUE_FLOAT')
|
|
|
|
self._fieldnames = ['name', 'value']
|
|
|
|
self.name = name
|
|
|
|
self.value = value
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 224, struct.pack('>10sf', self.name, self.value))
|
|
|
|
|
|
|
|
class MAVLink_named_value_int_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Send a key-value pair as integer. The use of this message is
|
|
|
|
discouraged for normal packets, but a quite efficient way for
|
|
|
|
testing new messages and getting experimental debug output.
|
|
|
|
'''
|
|
|
|
def __init__(self, name, value):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_NAMED_VALUE_INT, 'NAMED_VALUE_INT')
|
|
|
|
self._fieldnames = ['name', 'value']
|
|
|
|
self.name = name
|
|
|
|
self.value = value
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 60, struct.pack('>10si', self.name, self.value))
|
|
|
|
|
|
|
|
class MAVLink_statustext_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Status text message. These messages are printed in yellow in
|
|
|
|
the COMM console of QGroundControl. WARNING: They consume
|
|
|
|
quite some bandwidth, so use only for important status and
|
|
|
|
error messages. If implemented wisely, these messages are
|
|
|
|
buffered on the MCU and sent only at a limited rate (e.g. 10
|
|
|
|
Hz).
|
|
|
|
'''
|
|
|
|
def __init__(self, severity, text):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_STATUSTEXT, 'STATUSTEXT')
|
|
|
|
self._fieldnames = ['severity', 'text']
|
|
|
|
self.severity = severity
|
|
|
|
self.text = text
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 106, struct.pack('>B50s', self.severity, self.text))
|
|
|
|
|
|
|
|
class MAVLink_debug_message(MAVLink_message):
|
|
|
|
'''
|
|
|
|
Send a debug value. The index is used to discriminate between
|
|
|
|
values. These values show up in the plot of QGroundControl as
|
|
|
|
DEBUG N.
|
|
|
|
'''
|
|
|
|
def __init__(self, ind, value):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_DEBUG, 'DEBUG')
|
|
|
|
self._fieldnames = ['ind', 'value']
|
|
|
|
self.ind = ind
|
|
|
|
self.value = value
|
|
|
|
|
|
|
|
def pack(self, mav):
|
|
|
|
return MAVLink_message.pack(self, mav, 7, struct.pack('>Bf', self.ind, self.value))
|
|
|
|
|
|
|
|
|
|
|
|
mavlink_map = {
|
|
|
|
MAVLINK_MSG_ID_SENSOR_OFFSETS : ( '>hhhfiiffffff', MAVLink_sensor_offsets_message, [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11], 143 ),
|
|
|
|
MAVLINK_MSG_ID_SET_MAG_OFFSETS : ( '>BBhhh', MAVLink_set_mag_offsets_message, [0, 1, 2, 3, 4], 29 ),
|
|
|
|
MAVLINK_MSG_ID_MEMINFO : ( '>HH', MAVLink_meminfo_message, [0, 1], 208 ),
|
|
|
|
MAVLINK_MSG_ID_AP_ADC : ( '>HHHHHH', MAVLink_ap_adc_message, [0, 1, 2, 3, 4, 5], 188 ),
|
|
|
|
MAVLINK_MSG_ID_DIGICAM_CONFIGURE : ( '>BBBHBBBBBBf', MAVLink_digicam_configure_message, [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10], 118 ),
|
|
|
|
MAVLINK_MSG_ID_DIGICAM_CONTROL : ( '>BBBBbBBBBf', MAVLink_digicam_control_message, [0, 1, 2, 3, 4, 5, 6, 7, 8, 9], 242 ),
|
|
|
|
MAVLINK_MSG_ID_MOUNT_CONFIGURE : ( '>BBBBBB', MAVLink_mount_configure_message, [0, 1, 2, 3, 4, 5], 19 ),
|
|
|
|
MAVLINK_MSG_ID_MOUNT_CONTROL : ( '>BBiiiB', MAVLink_mount_control_message, [0, 1, 2, 3, 4, 5], 97 ),
|
|
|
|
MAVLINK_MSG_ID_MOUNT_STATUS : ( '>BBiii', MAVLink_mount_status_message, [0, 1, 2, 3, 4], 233 ),
|
2011-12-28 17:29:37 -04:00
|
|
|
MAVLINK_MSG_ID_FENCE_POINT : ( '>BBBBff', MAVLink_fence_point_message, [0, 1, 2, 3, 4, 5], 18 ),
|
|
|
|
MAVLINK_MSG_ID_FENCE_FETCH_POINT : ( '>BBB', MAVLink_fence_fetch_point_message, [0, 1, 2], 68 ),
|
|
|
|
MAVLINK_MSG_ID_FENCE_STATUS : ( '>BHBI', MAVLink_fence_status_message, [0, 1, 2, 3], 136 ),
|
2011-12-02 00:20:02 -04:00
|
|
|
MAVLINK_MSG_ID_HEARTBEAT : ( '>BBB', MAVLink_heartbeat_message, [0, 1, 2], 72 ),
|
|
|
|
MAVLINK_MSG_ID_BOOT : ( '>I', MAVLink_boot_message, [0], 39 ),
|
|
|
|
MAVLINK_MSG_ID_SYSTEM_TIME : ( '>Q', MAVLink_system_time_message, [0], 190 ),
|
|
|
|
MAVLINK_MSG_ID_PING : ( '>IBBQ', MAVLink_ping_message, [0, 1, 2, 3], 92 ),
|
|
|
|
MAVLINK_MSG_ID_SYSTEM_TIME_UTC : ( '>II', MAVLink_system_time_utc_message, [0, 1], 191 ),
|
|
|
|
MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL : ( '>BBB25s', MAVLink_change_operator_control_message, [0, 1, 2, 3], 217 ),
|
|
|
|
MAVLINK_MSG_ID_CHANGE_OPERATOR_CONTROL_ACK : ( '>BBB', MAVLink_change_operator_control_ack_message, [0, 1, 2], 104 ),
|
|
|
|
MAVLINK_MSG_ID_AUTH_KEY : ( '>32s', MAVLink_auth_key_message, [0], 119 ),
|
|
|
|
MAVLINK_MSG_ID_ACTION_ACK : ( '>BB', MAVLink_action_ack_message, [0, 1], 219 ),
|
|
|
|
MAVLINK_MSG_ID_ACTION : ( '>BBB', MAVLink_action_message, [0, 1, 2], 60 ),
|
|
|
|
MAVLINK_MSG_ID_SET_MODE : ( '>BB', MAVLink_set_mode_message, [0, 1], 186 ),
|
|
|
|
MAVLINK_MSG_ID_SET_NAV_MODE : ( '>BB', MAVLink_set_nav_mode_message, [0, 1], 10 ),
|
|
|
|
MAVLINK_MSG_ID_PARAM_REQUEST_READ : ( '>BB15sh', MAVLink_param_request_read_message, [0, 1, 2, 3], 89 ),
|
|
|
|
MAVLINK_MSG_ID_PARAM_REQUEST_LIST : ( '>BB', MAVLink_param_request_list_message, [0, 1], 159 ),
|
|
|
|
MAVLINK_MSG_ID_PARAM_VALUE : ( '>15sfHH', MAVLink_param_value_message, [0, 1, 2, 3], 162 ),
|
|
|
|
MAVLINK_MSG_ID_PARAM_SET : ( '>BB15sf', MAVLink_param_set_message, [0, 1, 2, 3], 121 ),
|
|
|
|
MAVLINK_MSG_ID_GPS_RAW_INT : ( '>QBiiiffff', MAVLink_gps_raw_int_message, [0, 1, 2, 3, 4, 5, 6, 7, 8], 149 ),
|
|
|
|
MAVLINK_MSG_ID_SCALED_IMU : ( '>Qhhhhhhhhh', MAVLink_scaled_imu_message, [0, 1, 2, 3, 4, 5, 6, 7, 8, 9], 222 ),
|
|
|
|
MAVLINK_MSG_ID_GPS_STATUS : ( '>B20s20s20s20s20s', MAVLink_gps_status_message, [0, 1, 2, 3, 4, 5], 110 ),
|
|
|
|
MAVLINK_MSG_ID_RAW_IMU : ( '>Qhhhhhhhhh', MAVLink_raw_imu_message, [0, 1, 2, 3, 4, 5, 6, 7, 8, 9], 179 ),
|
|
|
|
MAVLINK_MSG_ID_RAW_PRESSURE : ( '>Qhhhh', MAVLink_raw_pressure_message, [0, 1, 2, 3, 4], 136 ),
|
|
|
|
MAVLINK_MSG_ID_SCALED_PRESSURE : ( '>Qffh', MAVLink_scaled_pressure_message, [0, 1, 2, 3], 229 ),
|
|
|
|
MAVLINK_MSG_ID_ATTITUDE : ( '>Qffffff', MAVLink_attitude_message, [0, 1, 2, 3, 4, 5, 6], 66 ),
|
|
|
|
MAVLINK_MSG_ID_LOCAL_POSITION : ( '>Qffffff', MAVLink_local_position_message, [0, 1, 2, 3, 4, 5, 6], 126 ),
|
|
|
|
MAVLINK_MSG_ID_GLOBAL_POSITION : ( '>Qffffff', MAVLink_global_position_message, [0, 1, 2, 3, 4, 5, 6], 147 ),
|
|
|
|
MAVLINK_MSG_ID_GPS_RAW : ( '>QBfffffff', MAVLink_gps_raw_message, [0, 1, 2, 3, 4, 5, 6, 7, 8], 185 ),
|
|
|
|
MAVLINK_MSG_ID_SYS_STATUS : ( '>BBBHHHH', MAVLink_sys_status_message, [0, 1, 2, 3, 4, 5, 6], 112 ),
|
|
|
|
MAVLINK_MSG_ID_RC_CHANNELS_RAW : ( '>HHHHHHHHB', MAVLink_rc_channels_raw_message, [0, 1, 2, 3, 4, 5, 6, 7, 8], 252 ),
|
|
|
|
MAVLINK_MSG_ID_RC_CHANNELS_SCALED : ( '>hhhhhhhhB', MAVLink_rc_channels_scaled_message, [0, 1, 2, 3, 4, 5, 6, 7, 8], 162 ),
|
|
|
|
MAVLINK_MSG_ID_SERVO_OUTPUT_RAW : ( '>HHHHHHHH', MAVLink_servo_output_raw_message, [0, 1, 2, 3, 4, 5, 6, 7], 215 ),
|
|
|
|
MAVLINK_MSG_ID_WAYPOINT : ( '>BBHBBBBfffffff', MAVLink_waypoint_message, [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13], 128 ),
|
|
|
|
MAVLINK_MSG_ID_WAYPOINT_REQUEST : ( '>BBH', MAVLink_waypoint_request_message, [0, 1, 2], 9 ),
|
|
|
|
MAVLINK_MSG_ID_WAYPOINT_SET_CURRENT : ( '>BBH', MAVLink_waypoint_set_current_message, [0, 1, 2], 106 ),
|
|
|
|
MAVLINK_MSG_ID_WAYPOINT_CURRENT : ( '>H', MAVLink_waypoint_current_message, [0], 101 ),
|
|
|
|
MAVLINK_MSG_ID_WAYPOINT_REQUEST_LIST : ( '>BB', MAVLink_waypoint_request_list_message, [0, 1], 213 ),
|
|
|
|
MAVLINK_MSG_ID_WAYPOINT_COUNT : ( '>BBH', MAVLink_waypoint_count_message, [0, 1, 2], 4 ),
|
|
|
|
MAVLINK_MSG_ID_WAYPOINT_CLEAR_ALL : ( '>BB', MAVLink_waypoint_clear_all_message, [0, 1], 229 ),
|
|
|
|
MAVLINK_MSG_ID_WAYPOINT_REACHED : ( '>H', MAVLink_waypoint_reached_message, [0], 21 ),
|
|
|
|
MAVLINK_MSG_ID_WAYPOINT_ACK : ( '>BBB', MAVLink_waypoint_ack_message, [0, 1, 2], 214 ),
|
|
|
|
MAVLINK_MSG_ID_GPS_SET_GLOBAL_ORIGIN : ( '>BBiii', MAVLink_gps_set_global_origin_message, [0, 1, 2, 3, 4], 215 ),
|
|
|
|
MAVLINK_MSG_ID_GPS_LOCAL_ORIGIN_SET : ( '>iii', MAVLink_gps_local_origin_set_message, [0, 1, 2], 14 ),
|
|
|
|
MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT_SET : ( '>BBffff', MAVLink_local_position_setpoint_set_message, [0, 1, 2, 3, 4, 5], 206 ),
|
|
|
|
MAVLINK_MSG_ID_LOCAL_POSITION_SETPOINT : ( '>ffff', MAVLink_local_position_setpoint_message, [0, 1, 2, 3], 50 ),
|
|
|
|
MAVLINK_MSG_ID_CONTROL_STATUS : ( '>BBBBBBBB', MAVLink_control_status_message, [0, 1, 2, 3, 4, 5, 6, 7], 157 ),
|
|
|
|
MAVLINK_MSG_ID_SAFETY_SET_ALLOWED_AREA : ( '>BBBffffff', MAVLink_safety_set_allowed_area_message, [0, 1, 2, 3, 4, 5, 6, 7, 8], 126 ),
|
|
|
|
MAVLINK_MSG_ID_SAFETY_ALLOWED_AREA : ( '>Bffffff', MAVLink_safety_allowed_area_message, [0, 1, 2, 3, 4, 5, 6], 108 ),
|
|
|
|
MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_THRUST : ( '>BBffff', MAVLink_set_roll_pitch_yaw_thrust_message, [0, 1, 2, 3, 4, 5], 213 ),
|
|
|
|
MAVLINK_MSG_ID_SET_ROLL_PITCH_YAW_SPEED_THRUST : ( '>BBffff', MAVLink_set_roll_pitch_yaw_speed_thrust_message, [0, 1, 2, 3, 4, 5], 95 ),
|
|
|
|
MAVLINK_MSG_ID_ROLL_PITCH_YAW_THRUST_SETPOINT : ( '>Qffff', MAVLink_roll_pitch_yaw_thrust_setpoint_message, [0, 1, 2, 3, 4], 5 ),
|
|
|
|
MAVLINK_MSG_ID_ROLL_PITCH_YAW_SPEED_THRUST_SETPOINT : ( '>Qffff', MAVLink_roll_pitch_yaw_speed_thrust_setpoint_message, [0, 1, 2, 3, 4], 127 ),
|
|
|
|
MAVLINK_MSG_ID_NAV_CONTROLLER_OUTPUT : ( '>ffhhHfff', MAVLink_nav_controller_output_message, [0, 1, 2, 3, 4, 5, 6, 7], 57 ),
|
|
|
|
MAVLINK_MSG_ID_POSITION_TARGET : ( '>ffff', MAVLink_position_target_message, [0, 1, 2, 3], 126 ),
|
|
|
|
MAVLINK_MSG_ID_STATE_CORRECTION : ( '>fffffffff', MAVLink_state_correction_message, [0, 1, 2, 3, 4, 5, 6, 7, 8], 130 ),
|
|
|
|
MAVLINK_MSG_ID_SET_ALTITUDE : ( '>BI', MAVLink_set_altitude_message, [0, 1], 119 ),
|
|
|
|
MAVLINK_MSG_ID_REQUEST_DATA_STREAM : ( '>BBBHB', MAVLink_request_data_stream_message, [0, 1, 2, 3, 4], 193 ),
|
|
|
|
MAVLINK_MSG_ID_HIL_STATE : ( '>Qffffffiiihhhhhh', MAVLink_hil_state_message, [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15], 191 ),
|
|
|
|
MAVLINK_MSG_ID_HIL_CONTROLS : ( '>QffffBB', MAVLink_hil_controls_message, [0, 1, 2, 3, 4, 5, 6], 236 ),
|
|
|
|
MAVLINK_MSG_ID_MANUAL_CONTROL : ( '>BffffBBBB', MAVLink_manual_control_message, [0, 1, 2, 3, 4, 5, 6, 7, 8], 158 ),
|
|
|
|
MAVLINK_MSG_ID_RC_CHANNELS_OVERRIDE : ( '>BBHHHHHHHH', MAVLink_rc_channels_override_message, [0, 1, 2, 3, 4, 5, 6, 7, 8, 9], 143 ),
|
|
|
|
MAVLINK_MSG_ID_GLOBAL_POSITION_INT : ( '>iiihhh', MAVLink_global_position_int_message, [0, 1, 2, 3, 4, 5], 104 ),
|
|
|
|
MAVLINK_MSG_ID_VFR_HUD : ( '>ffhHff', MAVLink_vfr_hud_message, [0, 1, 2, 3, 4, 5], 123 ),
|
|
|
|
MAVLINK_MSG_ID_COMMAND : ( '>BBBBffff', MAVLink_command_message, [0, 1, 2, 3, 4, 5, 6, 7], 131 ),
|
|
|
|
MAVLINK_MSG_ID_COMMAND_ACK : ( '>ff', MAVLink_command_ack_message, [0, 1], 8 ),
|
|
|
|
MAVLINK_MSG_ID_OPTICAL_FLOW : ( '>QBhhBf', MAVLink_optical_flow_message, [0, 1, 2, 3, 4, 5], 174 ),
|
|
|
|
MAVLINK_MSG_ID_OBJECT_DETECTION_EVENT : ( '>IHB20sBff', MAVLink_object_detection_event_message, [0, 1, 2, 3, 4, 5, 6], 155 ),
|
|
|
|
MAVLINK_MSG_ID_DEBUG_VECT : ( '>10sQfff', MAVLink_debug_vect_message, [0, 1, 2, 3, 4], 178 ),
|
|
|
|
MAVLINK_MSG_ID_NAMED_VALUE_FLOAT : ( '>10sf', MAVLink_named_value_float_message, [0, 1], 224 ),
|
|
|
|
MAVLINK_MSG_ID_NAMED_VALUE_INT : ( '>10si', MAVLink_named_value_int_message, [0, 1], 60 ),
|
|
|
|
MAVLINK_MSG_ID_STATUSTEXT : ( '>B50s', MAVLink_statustext_message, [0, 1], 106 ),
|
|
|
|
MAVLINK_MSG_ID_DEBUG : ( '>Bf', MAVLink_debug_message, [0, 1], 7 ),
|
|
|
|
}
|
|
|
|
|
|
|
|
class MAVError(Exception):
|
|
|
|
'''MAVLink error class'''
|
|
|
|
def __init__(self, msg):
|
|
|
|
Exception.__init__(self, msg)
|
|
|
|
self.message = msg
|
|
|
|
|
|
|
|
class MAVString(str):
|
|
|
|
'''NUL terminated string'''
|
|
|
|
def __init__(self, s):
|
|
|
|
str.__init__(self)
|
|
|
|
def __str__(self):
|
|
|
|
i = self.find(chr(0))
|
|
|
|
if i == -1:
|
|
|
|
return self[:]
|
|
|
|
return self[0:i]
|
|
|
|
|
|
|
|
class MAVLink_bad_data(MAVLink_message):
|
|
|
|
'''
|
|
|
|
a piece of bad data in a mavlink stream
|
|
|
|
'''
|
|
|
|
def __init__(self, data, reason):
|
|
|
|
MAVLink_message.__init__(self, MAVLINK_MSG_ID_BAD_DATA, 'BAD_DATA')
|
|
|
|
self._fieldnames = ['data', 'reason']
|
|
|
|
self.data = data
|
|
|
|
self.reason = reason
|
|
|
|
self._msgbuf = data
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
class MAVLink(object):
|
|
|
|
'''MAVLink protocol handling class'''
|
|
|
|
def __init__(self, file, srcSystem=0, srcComponent=0):
|
|
|
|
self.seq = 0
|
|
|
|
self.file = file
|
|
|
|
self.srcSystem = srcSystem
|
|
|
|
self.srcComponent = srcComponent
|
|
|
|
self.callback = None
|
|
|
|
self.callback_args = None
|
|
|
|
self.callback_kwargs = None
|
|
|
|
self.buf = array.array('B')
|
|
|
|
self.expected_length = 6
|
|
|
|
self.have_prefix_error = False
|
|
|
|
self.robust_parsing = False
|
|
|
|
self.protocol_marker = 85
|
|
|
|
self.little_endian = False
|
|
|
|
self.crc_extra = False
|
|
|
|
self.sort_fields = False
|
|
|
|
self.total_packets_sent = 0
|
|
|
|
self.total_bytes_sent = 0
|
|
|
|
self.total_packets_received = 0
|
|
|
|
self.total_bytes_received = 0
|
|
|
|
self.total_receive_errors = 0
|
|
|
|
self.startup_time = time.time()
|
|
|
|
|
|
|
|
def set_callback(self, callback, *args, **kwargs):
|
|
|
|
self.callback = callback
|
|
|
|
self.callback_args = args
|
|
|
|
self.callback_kwargs = kwargs
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def send(self, mavmsg):
|
|
|
|
'''send a MAVLink message'''
|
|
|
|
buf = mavmsg.pack(self)
|
|
|
|
self.file.write(buf)
|
|
|
|
self.seq = (self.seq + 1) % 255
|
|
|
|
self.total_packets_sent += 1
|
|
|
|
self.total_bytes_sent += len(buf)
|
|
|
|
|
|
|
|
def bytes_needed(self):
|
|
|
|
'''return number of bytes needed for next parsing stage'''
|
|
|
|
ret = self.expected_length - len(self.buf)
|
|
|
|
if ret <= 0:
|
|
|
|
return 1
|
|
|
|
return ret
|
|
|
|
|
|
|
|
def parse_char(self, c):
|
|
|
|
'''input some data bytes, possibly returning a new message'''
|
|
|
|
if isinstance(c, str):
|
|
|
|
self.buf.fromstring(c)
|
|
|
|
else:
|
|
|
|
self.buf.extend(c)
|
|
|
|
self.total_bytes_received += len(c)
|
|
|
|
if len(self.buf) >= 1 and self.buf[0] != 85:
|
|
|
|
magic = self.buf[0]
|
|
|
|
self.buf = self.buf[1:]
|
|
|
|
if self.robust_parsing:
|
|
|
|
m = MAVLink_bad_data(chr(magic), "Bad prefix")
|
|
|
|
if self.callback:
|
|
|
|
self.callback(m, *self.callback_args, **self.callback_kwargs)
|
|
|
|
self.expected_length = 6
|
|
|
|
self.total_receive_errors += 1
|
|
|
|
return m
|
|
|
|
if self.have_prefix_error:
|
|
|
|
return None
|
|
|
|
self.have_prefix_error = True
|
|
|
|
self.total_receive_errors += 1
|
2011-12-28 17:29:37 -04:00
|
|
|
raise MAVError("invalid MAVLink prefix '%s'" % magic)
|
2011-12-02 00:20:02 -04:00
|
|
|
self.have_prefix_error = False
|
|
|
|
if len(self.buf) >= 2:
|
|
|
|
(magic, self.expected_length) = struct.unpack('BB', self.buf[0:2])
|
|
|
|
self.expected_length += 8
|
|
|
|
if self.expected_length >= 8 and len(self.buf) >= self.expected_length:
|
|
|
|
mbuf = self.buf[0:self.expected_length]
|
|
|
|
self.buf = self.buf[self.expected_length:]
|
|
|
|
self.expected_length = 6
|
|
|
|
if self.robust_parsing:
|
|
|
|
try:
|
|
|
|
m = self.decode(mbuf)
|
|
|
|
self.total_packets_received += 1
|
|
|
|
except MAVError as reason:
|
|
|
|
m = MAVLink_bad_data(mbuf, reason.message)
|
|
|
|
self.total_receive_errors += 1
|
|
|
|
else:
|
|
|
|
m = self.decode(mbuf)
|
|
|
|
self.total_packets_received += 1
|
|
|
|
if self.callback:
|
|
|
|
self.callback(m, *self.callback_args, **self.callback_kwargs)
|
|
|
|
return m
|
|
|
|
return None
|
|
|
|
|
|
|
|
def parse_buffer(self, s):
|
|
|
|
'''input some data bytes, possibly returning a list of new messages'''
|
|
|
|
m = self.parse_char(s)
|
|
|
|
if m is None:
|
|
|
|
return None
|
|
|
|
ret = [m]
|
|
|
|
while True:
|
|
|
|
m = self.parse_char("")
|
|
|
|
if m is None:
|
|
|
|
return ret
|
|
|
|
ret.append(m)
|
|
|
|
return ret
|
|
|
|
|
|
|
|
def decode(self, msgbuf):
|
|
|
|
'''decode a buffer as a MAVLink message'''
|
|
|
|
# decode the header
|
|
|
|
try:
|
|
|
|
magic, mlen, seq, srcSystem, srcComponent, msgId = struct.unpack('cBBBBB', msgbuf[:6])
|
|
|
|
except struct.error as emsg:
|
|
|
|
raise MAVError('Unable to unpack MAVLink header: %s' % emsg)
|
|
|
|
if ord(magic) != 85:
|
|
|
|
raise MAVError("invalid MAVLink prefix '%s'" % magic)
|
|
|
|
if mlen != len(msgbuf)-8:
|
|
|
|
raise MAVError('invalid MAVLink message length. Got %u expected %u, msgId=%u' % (len(msgbuf)-8, mlen, msgId))
|
|
|
|
|
|
|
|
if not msgId in mavlink_map:
|
|
|
|
raise MAVError('unknown MAVLink message ID %u' % msgId)
|
|
|
|
|
|
|
|
# decode the payload
|
|
|
|
(fmt, type, order_map, crc_extra) = mavlink_map[msgId]
|
|
|
|
|
|
|
|
# decode the checksum
|
|
|
|
try:
|
|
|
|
crc, = struct.unpack('<H', msgbuf[-2:])
|
|
|
|
except struct.error as emsg:
|
|
|
|
raise MAVError('Unable to unpack MAVLink CRC: %s' % emsg)
|
|
|
|
crc2 = mavutil.x25crc(msgbuf[1:-2])
|
2011-12-28 17:29:37 -04:00
|
|
|
if False: # using CRC extra
|
2011-12-02 00:20:02 -04:00
|
|
|
crc2.accumulate(chr(crc_extra))
|
|
|
|
if crc != crc2.crc:
|
|
|
|
raise MAVError('invalid MAVLink CRC in msgID %u 0x%04x should be 0x%04x' % (msgId, crc, crc2.crc))
|
|
|
|
|
|
|
|
try:
|
|
|
|
t = struct.unpack(fmt, msgbuf[6:-2])
|
|
|
|
except struct.error as emsg:
|
|
|
|
raise MAVError('Unable to unpack MAVLink payload type=%s fmt=%s payloadLength=%u: %s' % (
|
|
|
|
type, fmt, len(msgbuf[6:-2]), emsg))
|
|
|
|
|
|
|
|
tlist = list(t)
|
|
|
|
# handle sorted fields
|
|
|
|
if False:
|
|
|
|
t = tlist[:]
|
|
|
|
for i in range(0, len(tlist)):
|
|
|
|
tlist[i] = t[order_map[i]]
|
|
|
|
|
|
|
|
# terminate any strings
|
|
|
|
for i in range(0, len(tlist)):
|
|
|
|
if isinstance(tlist[i], str):
|
|
|
|
tlist[i] = MAVString(tlist[i])
|
|
|
|
t = tuple(tlist)
|
|
|
|
# construct the message object
|
|
|
|
try:
|
|
|
|
m = type(*t)
|
|
|
|
except Exception as emsg:
|
|
|
|
raise MAVError('Unable to instantiate MAVLink message of type %s : %s' % (type, emsg))
|
|
|
|
m._msgbuf = msgbuf
|
|
|
|
m._payload = msgbuf[6:-2]
|
|
|
|
m._crc = crc
|
|
|
|
m._header = MAVLink_header(msgId, mlen, seq, srcSystem, srcComponent)
|
|
|
|
return m
|
|
|
|
def sensor_offsets_encode(self, mag_ofs_x, mag_ofs_y, mag_ofs_z, mag_declination, raw_press, raw_temp, gyro_cal_x, gyro_cal_y, gyro_cal_z, accel_cal_x, accel_cal_y, accel_cal_z):
|
|
|
|
'''
|
|
|
|
Offsets and calibrations values for hardware sensors. This
|
|
|
|
makes it easier to debug the calibration process.
|
|
|
|
|
|
|
|
mag_ofs_x : magnetometer X offset (int16_t)
|
|
|
|
mag_ofs_y : magnetometer Y offset (int16_t)
|
|
|
|
mag_ofs_z : magnetometer Z offset (int16_t)
|
|
|
|
mag_declination : magnetic declination (radians) (float)
|
|
|
|
raw_press : raw pressure from barometer (int32_t)
|
|
|
|
raw_temp : raw temperature from barometer (int32_t)
|
|
|
|
gyro_cal_x : gyro X calibration (float)
|
|
|
|
gyro_cal_y : gyro Y calibration (float)
|
|
|
|
gyro_cal_z : gyro Z calibration (float)
|
|
|
|
accel_cal_x : accel X calibration (float)
|
|
|
|
accel_cal_y : accel Y calibration (float)
|
|
|
|
accel_cal_z : accel Z calibration (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_sensor_offsets_message(mag_ofs_x, mag_ofs_y, mag_ofs_z, mag_declination, raw_press, raw_temp, gyro_cal_x, gyro_cal_y, gyro_cal_z, accel_cal_x, accel_cal_y, accel_cal_z)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def sensor_offsets_send(self, mag_ofs_x, mag_ofs_y, mag_ofs_z, mag_declination, raw_press, raw_temp, gyro_cal_x, gyro_cal_y, gyro_cal_z, accel_cal_x, accel_cal_y, accel_cal_z):
|
|
|
|
'''
|
|
|
|
Offsets and calibrations values for hardware sensors. This
|
|
|
|
makes it easier to debug the calibration process.
|
|
|
|
|
|
|
|
mag_ofs_x : magnetometer X offset (int16_t)
|
|
|
|
mag_ofs_y : magnetometer Y offset (int16_t)
|
|
|
|
mag_ofs_z : magnetometer Z offset (int16_t)
|
|
|
|
mag_declination : magnetic declination (radians) (float)
|
|
|
|
raw_press : raw pressure from barometer (int32_t)
|
|
|
|
raw_temp : raw temperature from barometer (int32_t)
|
|
|
|
gyro_cal_x : gyro X calibration (float)
|
|
|
|
gyro_cal_y : gyro Y calibration (float)
|
|
|
|
gyro_cal_z : gyro Z calibration (float)
|
|
|
|
accel_cal_x : accel X calibration (float)
|
|
|
|
accel_cal_y : accel Y calibration (float)
|
|
|
|
accel_cal_z : accel Z calibration (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.sensor_offsets_encode(mag_ofs_x, mag_ofs_y, mag_ofs_z, mag_declination, raw_press, raw_temp, gyro_cal_x, gyro_cal_y, gyro_cal_z, accel_cal_x, accel_cal_y, accel_cal_z))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def set_mag_offsets_encode(self, target_system, target_component, mag_ofs_x, mag_ofs_y, mag_ofs_z):
|
|
|
|
'''
|
|
|
|
set the magnetometer offsets
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
mag_ofs_x : magnetometer X offset (int16_t)
|
|
|
|
mag_ofs_y : magnetometer Y offset (int16_t)
|
|
|
|
mag_ofs_z : magnetometer Z offset (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_set_mag_offsets_message(target_system, target_component, mag_ofs_x, mag_ofs_y, mag_ofs_z)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def set_mag_offsets_send(self, target_system, target_component, mag_ofs_x, mag_ofs_y, mag_ofs_z):
|
|
|
|
'''
|
|
|
|
set the magnetometer offsets
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
mag_ofs_x : magnetometer X offset (int16_t)
|
|
|
|
mag_ofs_y : magnetometer Y offset (int16_t)
|
|
|
|
mag_ofs_z : magnetometer Z offset (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.set_mag_offsets_encode(target_system, target_component, mag_ofs_x, mag_ofs_y, mag_ofs_z))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def meminfo_encode(self, brkval, freemem):
|
|
|
|
'''
|
|
|
|
state of APM memory
|
|
|
|
|
|
|
|
brkval : heap top (uint16_t)
|
|
|
|
freemem : free memory (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_meminfo_message(brkval, freemem)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def meminfo_send(self, brkval, freemem):
|
|
|
|
'''
|
|
|
|
state of APM memory
|
|
|
|
|
|
|
|
brkval : heap top (uint16_t)
|
|
|
|
freemem : free memory (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.meminfo_encode(brkval, freemem))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def ap_adc_encode(self, adc1, adc2, adc3, adc4, adc5, adc6):
|
|
|
|
'''
|
|
|
|
raw ADC output
|
|
|
|
|
|
|
|
adc1 : ADC output 1 (uint16_t)
|
|
|
|
adc2 : ADC output 2 (uint16_t)
|
|
|
|
adc3 : ADC output 3 (uint16_t)
|
|
|
|
adc4 : ADC output 4 (uint16_t)
|
|
|
|
adc5 : ADC output 5 (uint16_t)
|
|
|
|
adc6 : ADC output 6 (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_ap_adc_message(adc1, adc2, adc3, adc4, adc5, adc6)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def ap_adc_send(self, adc1, adc2, adc3, adc4, adc5, adc6):
|
|
|
|
'''
|
|
|
|
raw ADC output
|
|
|
|
|
|
|
|
adc1 : ADC output 1 (uint16_t)
|
|
|
|
adc2 : ADC output 2 (uint16_t)
|
|
|
|
adc3 : ADC output 3 (uint16_t)
|
|
|
|
adc4 : ADC output 4 (uint16_t)
|
|
|
|
adc5 : ADC output 5 (uint16_t)
|
|
|
|
adc6 : ADC output 6 (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.ap_adc_encode(adc1, adc2, adc3, adc4, adc5, adc6))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def digicam_configure_encode(self, target_system, target_component, mode, shutter_speed, aperture, iso, exposure_type, command_id, engine_cut_off, extra_param, extra_value):
|
|
|
|
'''
|
|
|
|
Configure on-board Camera Control System.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
mode : Mode enumeration from 1 to N //P, TV, AV, M, Etc (0 means ignore) (uint8_t)
|
|
|
|
shutter_speed : Divisor number //e.g. 1000 means 1/1000 (0 means ignore) (uint16_t)
|
|
|
|
aperture : F stop number x 10 //e.g. 28 means 2.8 (0 means ignore) (uint8_t)
|
|
|
|
iso : ISO enumeration from 1 to N //e.g. 80, 100, 200, Etc (0 means ignore) (uint8_t)
|
|
|
|
exposure_type : Exposure type enumeration from 1 to N (0 means ignore) (uint8_t)
|
|
|
|
command_id : Command Identity (incremental loop: 0 to 255)//A command sent multiple times will be executed or pooled just once (uint8_t)
|
|
|
|
engine_cut_off : Main engine cut-off time before camera trigger in seconds/10 (0 means no cut-off) (uint8_t)
|
|
|
|
extra_param : Extra parameters enumeration (0 means ignore) (uint8_t)
|
|
|
|
extra_value : Correspondent value to given extra_param (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_digicam_configure_message(target_system, target_component, mode, shutter_speed, aperture, iso, exposure_type, command_id, engine_cut_off, extra_param, extra_value)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def digicam_configure_send(self, target_system, target_component, mode, shutter_speed, aperture, iso, exposure_type, command_id, engine_cut_off, extra_param, extra_value):
|
|
|
|
'''
|
|
|
|
Configure on-board Camera Control System.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
mode : Mode enumeration from 1 to N //P, TV, AV, M, Etc (0 means ignore) (uint8_t)
|
|
|
|
shutter_speed : Divisor number //e.g. 1000 means 1/1000 (0 means ignore) (uint16_t)
|
|
|
|
aperture : F stop number x 10 //e.g. 28 means 2.8 (0 means ignore) (uint8_t)
|
|
|
|
iso : ISO enumeration from 1 to N //e.g. 80, 100, 200, Etc (0 means ignore) (uint8_t)
|
|
|
|
exposure_type : Exposure type enumeration from 1 to N (0 means ignore) (uint8_t)
|
|
|
|
command_id : Command Identity (incremental loop: 0 to 255)//A command sent multiple times will be executed or pooled just once (uint8_t)
|
|
|
|
engine_cut_off : Main engine cut-off time before camera trigger in seconds/10 (0 means no cut-off) (uint8_t)
|
|
|
|
extra_param : Extra parameters enumeration (0 means ignore) (uint8_t)
|
|
|
|
extra_value : Correspondent value to given extra_param (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.digicam_configure_encode(target_system, target_component, mode, shutter_speed, aperture, iso, exposure_type, command_id, engine_cut_off, extra_param, extra_value))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def digicam_control_encode(self, target_system, target_component, session, zoom_pos, zoom_step, focus_lock, shot, command_id, extra_param, extra_value):
|
|
|
|
'''
|
|
|
|
Control on-board Camera Control System to take shots.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
session : 0: stop, 1: start or keep it up //Session control e.g. show/hide lens (uint8_t)
|
|
|
|
zoom_pos : 1 to N //Zoom's absolute position (0 means ignore) (uint8_t)
|
|
|
|
zoom_step : -100 to 100 //Zooming step value to offset zoom from the current position (int8_t)
|
|
|
|
focus_lock : 0: unlock focus or keep unlocked, 1: lock focus or keep locked, 3: re-lock focus (uint8_t)
|
|
|
|
shot : 0: ignore, 1: shot or start filming (uint8_t)
|
|
|
|
command_id : Command Identity (incremental loop: 0 to 255)//A command sent multiple times will be executed or pooled just once (uint8_t)
|
|
|
|
extra_param : Extra parameters enumeration (0 means ignore) (uint8_t)
|
|
|
|
extra_value : Correspondent value to given extra_param (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_digicam_control_message(target_system, target_component, session, zoom_pos, zoom_step, focus_lock, shot, command_id, extra_param, extra_value)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def digicam_control_send(self, target_system, target_component, session, zoom_pos, zoom_step, focus_lock, shot, command_id, extra_param, extra_value):
|
|
|
|
'''
|
|
|
|
Control on-board Camera Control System to take shots.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
session : 0: stop, 1: start or keep it up //Session control e.g. show/hide lens (uint8_t)
|
|
|
|
zoom_pos : 1 to N //Zoom's absolute position (0 means ignore) (uint8_t)
|
|
|
|
zoom_step : -100 to 100 //Zooming step value to offset zoom from the current position (int8_t)
|
|
|
|
focus_lock : 0: unlock focus or keep unlocked, 1: lock focus or keep locked, 3: re-lock focus (uint8_t)
|
|
|
|
shot : 0: ignore, 1: shot or start filming (uint8_t)
|
|
|
|
command_id : Command Identity (incremental loop: 0 to 255)//A command sent multiple times will be executed or pooled just once (uint8_t)
|
|
|
|
extra_param : Extra parameters enumeration (0 means ignore) (uint8_t)
|
|
|
|
extra_value : Correspondent value to given extra_param (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.digicam_control_encode(target_system, target_component, session, zoom_pos, zoom_step, focus_lock, shot, command_id, extra_param, extra_value))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def mount_configure_encode(self, target_system, target_component, mount_mode, stab_roll, stab_pitch, stab_yaw):
|
|
|
|
'''
|
|
|
|
Message to configure a camera mount, directional antenna, etc.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
mount_mode : mount operating mode (see MAV_MOUNT_MODE enum) (uint8_t)
|
|
|
|
stab_roll : (1 = yes, 0 = no) (uint8_t)
|
|
|
|
stab_pitch : (1 = yes, 0 = no) (uint8_t)
|
|
|
|
stab_yaw : (1 = yes, 0 = no) (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_mount_configure_message(target_system, target_component, mount_mode, stab_roll, stab_pitch, stab_yaw)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def mount_configure_send(self, target_system, target_component, mount_mode, stab_roll, stab_pitch, stab_yaw):
|
|
|
|
'''
|
|
|
|
Message to configure a camera mount, directional antenna, etc.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
mount_mode : mount operating mode (see MAV_MOUNT_MODE enum) (uint8_t)
|
|
|
|
stab_roll : (1 = yes, 0 = no) (uint8_t)
|
|
|
|
stab_pitch : (1 = yes, 0 = no) (uint8_t)
|
|
|
|
stab_yaw : (1 = yes, 0 = no) (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.mount_configure_encode(target_system, target_component, mount_mode, stab_roll, stab_pitch, stab_yaw))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def mount_control_encode(self, target_system, target_component, input_a, input_b, input_c, save_position):
|
|
|
|
'''
|
|
|
|
Message to control a camera mount, directional antenna, etc.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
input_a : pitch(deg*100) or lat, depending on mount mode (int32_t)
|
|
|
|
input_b : roll(deg*100) or lon depending on mount mode (int32_t)
|
|
|
|
input_c : yaw(deg*100) or alt (in cm) depending on mount mode (int32_t)
|
|
|
|
save_position : if "1" it will save current trimmed position on EEPROM (just valid for NEUTRAL and LANDING) (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_mount_control_message(target_system, target_component, input_a, input_b, input_c, save_position)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def mount_control_send(self, target_system, target_component, input_a, input_b, input_c, save_position):
|
|
|
|
'''
|
|
|
|
Message to control a camera mount, directional antenna, etc.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
input_a : pitch(deg*100) or lat, depending on mount mode (int32_t)
|
|
|
|
input_b : roll(deg*100) or lon depending on mount mode (int32_t)
|
|
|
|
input_c : yaw(deg*100) or alt (in cm) depending on mount mode (int32_t)
|
|
|
|
save_position : if "1" it will save current trimmed position on EEPROM (just valid for NEUTRAL and LANDING) (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.mount_control_encode(target_system, target_component, input_a, input_b, input_c, save_position))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def mount_status_encode(self, target_system, target_component, pointing_a, pointing_b, pointing_c):
|
|
|
|
'''
|
|
|
|
Message with some status from APM to GCS about camera or antenna mount
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
pointing_a : pitch(deg*100) or lat, depending on mount mode (int32_t)
|
|
|
|
pointing_b : roll(deg*100) or lon depending on mount mode (int32_t)
|
|
|
|
pointing_c : yaw(deg*100) or alt (in cm) depending on mount mode (int32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_mount_status_message(target_system, target_component, pointing_a, pointing_b, pointing_c)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def mount_status_send(self, target_system, target_component, pointing_a, pointing_b, pointing_c):
|
|
|
|
'''
|
|
|
|
Message with some status from APM to GCS about camera or antenna mount
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
pointing_a : pitch(deg*100) or lat, depending on mount mode (int32_t)
|
|
|
|
pointing_b : roll(deg*100) or lon depending on mount mode (int32_t)
|
|
|
|
pointing_c : yaw(deg*100) or alt (in cm) depending on mount mode (int32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.mount_status_encode(target_system, target_component, pointing_a, pointing_b, pointing_c))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
|
|
|
def fence_point_encode(self, target_system, target_component, idx, count, lat, lng):
|
|
|
|
'''
|
|
|
|
A fence point. Used to set a point when from GCS -> MAV.
|
|
|
|
Also used to return a point from MAV -> GCS
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
idx : point index (first point is 1, 0 is for return point) (uint8_t)
|
|
|
|
count : total number of points (for sanity checking) (uint8_t)
|
|
|
|
lat : Latitude of point (float)
|
|
|
|
lng : Longitude of point (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_fence_point_message(target_system, target_component, idx, count, lat, lng)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
|
|
|
|
|
|
|
def fence_point_send(self, target_system, target_component, idx, count, lat, lng):
|
|
|
|
'''
|
|
|
|
A fence point. Used to set a point when from GCS -> MAV.
|
|
|
|
Also used to return a point from MAV -> GCS
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
idx : point index (first point is 1, 0 is for return point) (uint8_t)
|
|
|
|
count : total number of points (for sanity checking) (uint8_t)
|
|
|
|
lat : Latitude of point (float)
|
|
|
|
lng : Longitude of point (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.fence_point_encode(target_system, target_component, idx, count, lat, lng))
|
|
|
|
|
|
|
|
def fence_fetch_point_encode(self, target_system, target_component, idx):
|
|
|
|
'''
|
|
|
|
Request a current fence point from MAV
|
2011-12-02 00:20:02 -04:00
|
|
|
|
2011-12-28 17:29:37 -04:00
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
idx : point index (first point is 1, 0 is for return point) (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_fence_fetch_point_message(target_system, target_component, idx)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
|
|
|
|
|
|
|
def fence_fetch_point_send(self, target_system, target_component, idx):
|
|
|
|
'''
|
|
|
|
Request a current fence point from MAV
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
idx : point index (first point is 1, 0 is for return point) (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.fence_fetch_point_encode(target_system, target_component, idx))
|
|
|
|
|
|
|
|
def fence_status_encode(self, breach_status, breach_count, breach_type, breach_time):
|
|
|
|
'''
|
|
|
|
Status of geo-fencing. Sent in extended status stream when
|
|
|
|
fencing enabled
|
|
|
|
|
|
|
|
breach_status : 0 if currently inside fence, 1 if outside (uint8_t)
|
|
|
|
breach_count : number of fence breaches (uint16_t)
|
|
|
|
breach_type : last breach type (see FENCE_BREACH_* enum) (uint8_t)
|
|
|
|
breach_time : time of last breach in milliseconds since boot (uint32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_fence_status_message(breach_status, breach_count, breach_type, breach_time)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
|
|
|
|
|
|
|
def fence_status_send(self, breach_status, breach_count, breach_type, breach_time):
|
|
|
|
'''
|
|
|
|
Status of geo-fencing. Sent in extended status stream when
|
|
|
|
fencing enabled
|
|
|
|
|
|
|
|
breach_status : 0 if currently inside fence, 1 if outside (uint8_t)
|
|
|
|
breach_count : number of fence breaches (uint16_t)
|
|
|
|
breach_type : last breach type (see FENCE_BREACH_* enum) (uint8_t)
|
|
|
|
breach_time : time of last breach in milliseconds since boot (uint32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.fence_status_encode(breach_status, breach_count, breach_type, breach_time))
|
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def heartbeat_encode(self, type, autopilot, mavlink_version=2):
|
|
|
|
'''
|
|
|
|
The heartbeat message shows that a system is present and responding.
|
|
|
|
The type of the MAV and Autopilot hardware allow the
|
|
|
|
receiving system to treat further messages from this
|
|
|
|
system appropriate (e.g. by laying out the user
|
|
|
|
interface based on the autopilot).
|
|
|
|
|
|
|
|
type : Type of the MAV (quadrotor, helicopter, etc., up to 15 types, defined in MAV_TYPE ENUM) (uint8_t)
|
|
|
|
autopilot : Type of the Autopilot: 0: Generic, 1: PIXHAWK, 2: SLUGS, 3: Ardupilot (up to 15 types), defined in MAV_AUTOPILOT_TYPE ENUM (uint8_t)
|
|
|
|
mavlink_version : MAVLink version (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_heartbeat_message(type, autopilot, mavlink_version)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def heartbeat_send(self, type, autopilot, mavlink_version=2):
|
|
|
|
'''
|
|
|
|
The heartbeat message shows that a system is present and responding.
|
|
|
|
The type of the MAV and Autopilot hardware allow the
|
|
|
|
receiving system to treat further messages from this
|
|
|
|
system appropriate (e.g. by laying out the user
|
|
|
|
interface based on the autopilot).
|
|
|
|
|
|
|
|
type : Type of the MAV (quadrotor, helicopter, etc., up to 15 types, defined in MAV_TYPE ENUM) (uint8_t)
|
|
|
|
autopilot : Type of the Autopilot: 0: Generic, 1: PIXHAWK, 2: SLUGS, 3: Ardupilot (up to 15 types), defined in MAV_AUTOPILOT_TYPE ENUM (uint8_t)
|
|
|
|
mavlink_version : MAVLink version (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.heartbeat_encode(type, autopilot, mavlink_version))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def boot_encode(self, version):
|
|
|
|
'''
|
|
|
|
The boot message indicates that a system is starting. The onboard
|
|
|
|
software version allows to keep track of onboard
|
|
|
|
soft/firmware revisions.
|
|
|
|
|
|
|
|
version : The onboard software version (uint32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_boot_message(version)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def boot_send(self, version):
|
|
|
|
'''
|
|
|
|
The boot message indicates that a system is starting. The onboard
|
|
|
|
software version allows to keep track of onboard
|
|
|
|
soft/firmware revisions.
|
|
|
|
|
|
|
|
version : The onboard software version (uint32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.boot_encode(version))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def system_time_encode(self, time_usec):
|
|
|
|
'''
|
|
|
|
The system time is the time of the master clock, typically the
|
|
|
|
computer clock of the main onboard computer.
|
|
|
|
|
|
|
|
time_usec : Timestamp of the master clock in microseconds since UNIX epoch. (uint64_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_system_time_message(time_usec)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def system_time_send(self, time_usec):
|
|
|
|
'''
|
|
|
|
The system time is the time of the master clock, typically the
|
|
|
|
computer clock of the main onboard computer.
|
|
|
|
|
|
|
|
time_usec : Timestamp of the master clock in microseconds since UNIX epoch. (uint64_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.system_time_encode(time_usec))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def ping_encode(self, seq, target_system, target_component, time):
|
|
|
|
'''
|
|
|
|
A ping message either requesting or responding to a ping. This allows
|
|
|
|
to measure the system latencies, including serial
|
|
|
|
port, radio modem and UDP connections.
|
|
|
|
|
|
|
|
seq : PING sequence (uint32_t)
|
|
|
|
target_system : 0: request ping from all receiving systems, if greater than 0: message is a ping response and number is the system id of the requesting system (uint8_t)
|
|
|
|
target_component : 0: request ping from all receiving components, if greater than 0: message is a ping response and number is the system id of the requesting system (uint8_t)
|
|
|
|
time : Unix timestamp in microseconds (uint64_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_ping_message(seq, target_system, target_component, time)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def ping_send(self, seq, target_system, target_component, time):
|
|
|
|
'''
|
|
|
|
A ping message either requesting or responding to a ping. This allows
|
|
|
|
to measure the system latencies, including serial
|
|
|
|
port, radio modem and UDP connections.
|
|
|
|
|
|
|
|
seq : PING sequence (uint32_t)
|
|
|
|
target_system : 0: request ping from all receiving systems, if greater than 0: message is a ping response and number is the system id of the requesting system (uint8_t)
|
|
|
|
target_component : 0: request ping from all receiving components, if greater than 0: message is a ping response and number is the system id of the requesting system (uint8_t)
|
|
|
|
time : Unix timestamp in microseconds (uint64_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.ping_encode(seq, target_system, target_component, time))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def system_time_utc_encode(self, utc_date, utc_time):
|
|
|
|
'''
|
|
|
|
UTC date and time from GPS module
|
|
|
|
|
|
|
|
utc_date : GPS UTC date ddmmyy (uint32_t)
|
|
|
|
utc_time : GPS UTC time hhmmss (uint32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_system_time_utc_message(utc_date, utc_time)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def system_time_utc_send(self, utc_date, utc_time):
|
|
|
|
'''
|
|
|
|
UTC date and time from GPS module
|
|
|
|
|
|
|
|
utc_date : GPS UTC date ddmmyy (uint32_t)
|
|
|
|
utc_time : GPS UTC time hhmmss (uint32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.system_time_utc_encode(utc_date, utc_time))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def change_operator_control_encode(self, target_system, control_request, version, passkey):
|
|
|
|
'''
|
|
|
|
Request to control this MAV
|
|
|
|
|
|
|
|
target_system : System the GCS requests control for (uint8_t)
|
|
|
|
control_request : 0: request control of this MAV, 1: Release control of this MAV (uint8_t)
|
|
|
|
version : 0: key as plaintext, 1-255: future, different hashing/encryption variants. The GCS should in general use the safest mode possible initially and then gradually move down the encryption level if it gets a NACK message indicating an encryption mismatch. (uint8_t)
|
|
|
|
passkey : Password / Key, depending on version plaintext or encrypted. 25 or less characters, NULL terminated. The characters may involve A-Z, a-z, 0-9, and "!?,.-" (char)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_change_operator_control_message(target_system, control_request, version, passkey)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def change_operator_control_send(self, target_system, control_request, version, passkey):
|
|
|
|
'''
|
|
|
|
Request to control this MAV
|
|
|
|
|
|
|
|
target_system : System the GCS requests control for (uint8_t)
|
|
|
|
control_request : 0: request control of this MAV, 1: Release control of this MAV (uint8_t)
|
|
|
|
version : 0: key as plaintext, 1-255: future, different hashing/encryption variants. The GCS should in general use the safest mode possible initially and then gradually move down the encryption level if it gets a NACK message indicating an encryption mismatch. (uint8_t)
|
|
|
|
passkey : Password / Key, depending on version plaintext or encrypted. 25 or less characters, NULL terminated. The characters may involve A-Z, a-z, 0-9, and "!?,.-" (char)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.change_operator_control_encode(target_system, control_request, version, passkey))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def change_operator_control_ack_encode(self, gcs_system_id, control_request, ack):
|
|
|
|
'''
|
|
|
|
Accept / deny control of this MAV
|
|
|
|
|
|
|
|
gcs_system_id : ID of the GCS this message (uint8_t)
|
|
|
|
control_request : 0: request control of this MAV, 1: Release control of this MAV (uint8_t)
|
|
|
|
ack : 0: ACK, 1: NACK: Wrong passkey, 2: NACK: Unsupported passkey encryption method, 3: NACK: Already under control (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_change_operator_control_ack_message(gcs_system_id, control_request, ack)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def change_operator_control_ack_send(self, gcs_system_id, control_request, ack):
|
|
|
|
'''
|
|
|
|
Accept / deny control of this MAV
|
|
|
|
|
|
|
|
gcs_system_id : ID of the GCS this message (uint8_t)
|
|
|
|
control_request : 0: request control of this MAV, 1: Release control of this MAV (uint8_t)
|
|
|
|
ack : 0: ACK, 1: NACK: Wrong passkey, 2: NACK: Unsupported passkey encryption method, 3: NACK: Already under control (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.change_operator_control_ack_encode(gcs_system_id, control_request, ack))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def auth_key_encode(self, key):
|
|
|
|
'''
|
|
|
|
Emit an encrypted signature / key identifying this system. PLEASE
|
|
|
|
NOTE: This protocol has been kept simple, so
|
|
|
|
transmitting the key requires an encrypted channel for
|
|
|
|
true safety.
|
|
|
|
|
|
|
|
key : key (char)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_auth_key_message(key)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def auth_key_send(self, key):
|
|
|
|
'''
|
|
|
|
Emit an encrypted signature / key identifying this system. PLEASE
|
|
|
|
NOTE: This protocol has been kept simple, so
|
|
|
|
transmitting the key requires an encrypted channel for
|
|
|
|
true safety.
|
|
|
|
|
|
|
|
key : key (char)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.auth_key_encode(key))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def action_ack_encode(self, action, result):
|
|
|
|
'''
|
|
|
|
This message acknowledges an action. IMPORTANT: The acknowledgement
|
|
|
|
can be also negative, e.g. the MAV rejects a reset
|
|
|
|
message because it is in-flight. The action ids are
|
|
|
|
defined in ENUM MAV_ACTION in
|
|
|
|
mavlink/include/mavlink_types.h
|
|
|
|
|
|
|
|
action : The action id (uint8_t)
|
|
|
|
result : 0: Action DENIED, 1: Action executed (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_action_ack_message(action, result)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def action_ack_send(self, action, result):
|
|
|
|
'''
|
|
|
|
This message acknowledges an action. IMPORTANT: The acknowledgement
|
|
|
|
can be also negative, e.g. the MAV rejects a reset
|
|
|
|
message because it is in-flight. The action ids are
|
|
|
|
defined in ENUM MAV_ACTION in
|
|
|
|
mavlink/include/mavlink_types.h
|
|
|
|
|
|
|
|
action : The action id (uint8_t)
|
|
|
|
result : 0: Action DENIED, 1: Action executed (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.action_ack_encode(action, result))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def action_encode(self, target, target_component, action):
|
|
|
|
'''
|
|
|
|
An action message allows to execute a certain onboard action. These
|
|
|
|
include liftoff, land, storing parameters too EEPROM,
|
|
|
|
shutddown, etc. The action ids are defined in ENUM
|
|
|
|
MAV_ACTION in mavlink/include/mavlink_types.h
|
|
|
|
|
|
|
|
target : The system executing the action (uint8_t)
|
|
|
|
target_component : The component executing the action (uint8_t)
|
|
|
|
action : The action id (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_action_message(target, target_component, action)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def action_send(self, target, target_component, action):
|
|
|
|
'''
|
|
|
|
An action message allows to execute a certain onboard action. These
|
|
|
|
include liftoff, land, storing parameters too EEPROM,
|
|
|
|
shutddown, etc. The action ids are defined in ENUM
|
|
|
|
MAV_ACTION in mavlink/include/mavlink_types.h
|
|
|
|
|
|
|
|
target : The system executing the action (uint8_t)
|
|
|
|
target_component : The component executing the action (uint8_t)
|
|
|
|
action : The action id (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.action_encode(target, target_component, action))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def set_mode_encode(self, target, mode):
|
|
|
|
'''
|
|
|
|
Set the system mode, as defined by enum MAV_MODE in
|
|
|
|
mavlink/include/mavlink_types.h. There is no target
|
|
|
|
component id as the mode is by definition for the
|
|
|
|
overall aircraft, not only for one component.
|
|
|
|
|
|
|
|
target : The system setting the mode (uint8_t)
|
|
|
|
mode : The new mode (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_set_mode_message(target, mode)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def set_mode_send(self, target, mode):
|
|
|
|
'''
|
|
|
|
Set the system mode, as defined by enum MAV_MODE in
|
|
|
|
mavlink/include/mavlink_types.h. There is no target
|
|
|
|
component id as the mode is by definition for the
|
|
|
|
overall aircraft, not only for one component.
|
|
|
|
|
|
|
|
target : The system setting the mode (uint8_t)
|
|
|
|
mode : The new mode (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.set_mode_encode(target, mode))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def set_nav_mode_encode(self, target, nav_mode):
|
|
|
|
'''
|
|
|
|
Set the system navigation mode, as defined by enum MAV_NAV_MODE in
|
|
|
|
mavlink/include/mavlink_types.h. The navigation mode
|
|
|
|
applies to the whole aircraft and thus all components.
|
|
|
|
|
|
|
|
target : The system setting the mode (uint8_t)
|
|
|
|
nav_mode : The new navigation mode (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_set_nav_mode_message(target, nav_mode)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def set_nav_mode_send(self, target, nav_mode):
|
|
|
|
'''
|
|
|
|
Set the system navigation mode, as defined by enum MAV_NAV_MODE in
|
|
|
|
mavlink/include/mavlink_types.h. The navigation mode
|
|
|
|
applies to the whole aircraft and thus all components.
|
|
|
|
|
|
|
|
target : The system setting the mode (uint8_t)
|
|
|
|
nav_mode : The new navigation mode (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.set_nav_mode_encode(target, nav_mode))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def param_request_read_encode(self, target_system, target_component, param_id, param_index):
|
|
|
|
'''
|
|
|
|
Request to read the onboard parameter with the param_id string id.
|
|
|
|
Onboard parameters are stored as key[const char*] ->
|
|
|
|
value[float]. This allows to send a parameter to any
|
|
|
|
other component (such as the GCS) without the need of
|
|
|
|
previous knowledge of possible parameter names. Thus
|
|
|
|
the same GCS can store different parameters for
|
|
|
|
different autopilots. See also
|
|
|
|
http://qgroundcontrol.org/parameter_interface for a
|
|
|
|
full documentation of QGroundControl and IMU code.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
param_id : Onboard parameter id (int8_t)
|
|
|
|
param_index : Parameter index. Send -1 to use the param ID field as identifier (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_param_request_read_message(target_system, target_component, param_id, param_index)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def param_request_read_send(self, target_system, target_component, param_id, param_index):
|
|
|
|
'''
|
|
|
|
Request to read the onboard parameter with the param_id string id.
|
|
|
|
Onboard parameters are stored as key[const char*] ->
|
|
|
|
value[float]. This allows to send a parameter to any
|
|
|
|
other component (such as the GCS) without the need of
|
|
|
|
previous knowledge of possible parameter names. Thus
|
|
|
|
the same GCS can store different parameters for
|
|
|
|
different autopilots. See also
|
|
|
|
http://qgroundcontrol.org/parameter_interface for a
|
|
|
|
full documentation of QGroundControl and IMU code.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
param_id : Onboard parameter id (int8_t)
|
|
|
|
param_index : Parameter index. Send -1 to use the param ID field as identifier (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.param_request_read_encode(target_system, target_component, param_id, param_index))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def param_request_list_encode(self, target_system, target_component):
|
|
|
|
'''
|
|
|
|
Request all parameters of this component. After his request, all
|
|
|
|
parameters are emitted.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_param_request_list_message(target_system, target_component)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def param_request_list_send(self, target_system, target_component):
|
|
|
|
'''
|
|
|
|
Request all parameters of this component. After his request, all
|
|
|
|
parameters are emitted.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.param_request_list_encode(target_system, target_component))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def param_value_encode(self, param_id, param_value, param_count, param_index):
|
|
|
|
'''
|
|
|
|
Emit the value of a onboard parameter. The inclusion of param_count
|
|
|
|
and param_index in the message allows the recipient to
|
|
|
|
keep track of received parameters and allows him to
|
|
|
|
re-request missing parameters after a loss or timeout.
|
|
|
|
|
|
|
|
param_id : Onboard parameter id (int8_t)
|
|
|
|
param_value : Onboard parameter value (float)
|
|
|
|
param_count : Total number of onboard parameters (uint16_t)
|
|
|
|
param_index : Index of this onboard parameter (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_param_value_message(param_id, param_value, param_count, param_index)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def param_value_send(self, param_id, param_value, param_count, param_index):
|
|
|
|
'''
|
|
|
|
Emit the value of a onboard parameter. The inclusion of param_count
|
|
|
|
and param_index in the message allows the recipient to
|
|
|
|
keep track of received parameters and allows him to
|
|
|
|
re-request missing parameters after a loss or timeout.
|
|
|
|
|
|
|
|
param_id : Onboard parameter id (int8_t)
|
|
|
|
param_value : Onboard parameter value (float)
|
|
|
|
param_count : Total number of onboard parameters (uint16_t)
|
|
|
|
param_index : Index of this onboard parameter (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.param_value_encode(param_id, param_value, param_count, param_index))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def param_set_encode(self, target_system, target_component, param_id, param_value):
|
|
|
|
'''
|
|
|
|
Set a parameter value TEMPORARILY to RAM. It will be reset to default
|
|
|
|
on system reboot. Send the ACTION
|
|
|
|
MAV_ACTION_STORAGE_WRITE to PERMANENTLY write the RAM
|
|
|
|
contents to EEPROM. IMPORTANT: The receiving component
|
|
|
|
should acknowledge the new parameter value by sending
|
|
|
|
a param_value message to all communication partners.
|
|
|
|
This will also ensure that multiple GCS all have an
|
|
|
|
up-to-date list of all parameters. If the sending GCS
|
|
|
|
did not receive a PARAM_VALUE message within its
|
|
|
|
timeout time, it should re-send the PARAM_SET message.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
param_id : Onboard parameter id (int8_t)
|
|
|
|
param_value : Onboard parameter value (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_param_set_message(target_system, target_component, param_id, param_value)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def param_set_send(self, target_system, target_component, param_id, param_value):
|
|
|
|
'''
|
|
|
|
Set a parameter value TEMPORARILY to RAM. It will be reset to default
|
|
|
|
on system reboot. Send the ACTION
|
|
|
|
MAV_ACTION_STORAGE_WRITE to PERMANENTLY write the RAM
|
|
|
|
contents to EEPROM. IMPORTANT: The receiving component
|
|
|
|
should acknowledge the new parameter value by sending
|
|
|
|
a param_value message to all communication partners.
|
|
|
|
This will also ensure that multiple GCS all have an
|
|
|
|
up-to-date list of all parameters. If the sending GCS
|
|
|
|
did not receive a PARAM_VALUE message within its
|
|
|
|
timeout time, it should re-send the PARAM_SET message.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
param_id : Onboard parameter id (int8_t)
|
|
|
|
param_value : Onboard parameter value (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.param_set_encode(target_system, target_component, param_id, param_value))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def gps_raw_int_encode(self, usec, fix_type, lat, lon, alt, eph, epv, v, hdg):
|
|
|
|
'''
|
|
|
|
The global position, as returned by the Global Positioning System
|
|
|
|
(GPS). This is NOT the global position estimate of the
|
|
|
|
sytem, but rather a RAW sensor value. See message
|
|
|
|
GLOBAL_POSITION for the global position estimate.
|
|
|
|
Coordinate frame is right-handed, Z-axis up (GPS
|
|
|
|
frame)
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
fix_type : 0-1: no fix, 2: 2D fix, 3: 3D fix. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. (uint8_t)
|
|
|
|
lat : Latitude in 1E7 degrees (int32_t)
|
|
|
|
lon : Longitude in 1E7 degrees (int32_t)
|
|
|
|
alt : Altitude in 1E3 meters (millimeters) (int32_t)
|
|
|
|
eph : GPS HDOP (float)
|
|
|
|
epv : GPS VDOP (float)
|
|
|
|
v : GPS ground speed (m/s) (float)
|
|
|
|
hdg : Compass heading in degrees, 0..360 degrees (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_gps_raw_int_message(usec, fix_type, lat, lon, alt, eph, epv, v, hdg)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def gps_raw_int_send(self, usec, fix_type, lat, lon, alt, eph, epv, v, hdg):
|
|
|
|
'''
|
|
|
|
The global position, as returned by the Global Positioning System
|
|
|
|
(GPS). This is NOT the global position estimate of the
|
|
|
|
sytem, but rather a RAW sensor value. See message
|
|
|
|
GLOBAL_POSITION for the global position estimate.
|
|
|
|
Coordinate frame is right-handed, Z-axis up (GPS
|
|
|
|
frame)
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
fix_type : 0-1: no fix, 2: 2D fix, 3: 3D fix. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. (uint8_t)
|
|
|
|
lat : Latitude in 1E7 degrees (int32_t)
|
|
|
|
lon : Longitude in 1E7 degrees (int32_t)
|
|
|
|
alt : Altitude in 1E3 meters (millimeters) (int32_t)
|
|
|
|
eph : GPS HDOP (float)
|
|
|
|
epv : GPS VDOP (float)
|
|
|
|
v : GPS ground speed (m/s) (float)
|
|
|
|
hdg : Compass heading in degrees, 0..360 degrees (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.gps_raw_int_encode(usec, fix_type, lat, lon, alt, eph, epv, v, hdg))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def scaled_imu_encode(self, usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
|
|
|
|
'''
|
|
|
|
The RAW IMU readings for the usual 9DOF sensor setup. This message
|
|
|
|
should contain the scaled values to the described
|
|
|
|
units
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
xacc : X acceleration (mg) (int16_t)
|
|
|
|
yacc : Y acceleration (mg) (int16_t)
|
|
|
|
zacc : Z acceleration (mg) (int16_t)
|
|
|
|
xgyro : Angular speed around X axis (millirad /sec) (int16_t)
|
|
|
|
ygyro : Angular speed around Y axis (millirad /sec) (int16_t)
|
|
|
|
zgyro : Angular speed around Z axis (millirad /sec) (int16_t)
|
|
|
|
xmag : X Magnetic field (milli tesla) (int16_t)
|
|
|
|
ymag : Y Magnetic field (milli tesla) (int16_t)
|
|
|
|
zmag : Z Magnetic field (milli tesla) (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_scaled_imu_message(usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def scaled_imu_send(self, usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
|
|
|
|
'''
|
|
|
|
The RAW IMU readings for the usual 9DOF sensor setup. This message
|
|
|
|
should contain the scaled values to the described
|
|
|
|
units
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
xacc : X acceleration (mg) (int16_t)
|
|
|
|
yacc : Y acceleration (mg) (int16_t)
|
|
|
|
zacc : Z acceleration (mg) (int16_t)
|
|
|
|
xgyro : Angular speed around X axis (millirad /sec) (int16_t)
|
|
|
|
ygyro : Angular speed around Y axis (millirad /sec) (int16_t)
|
|
|
|
zgyro : Angular speed around Z axis (millirad /sec) (int16_t)
|
|
|
|
xmag : X Magnetic field (milli tesla) (int16_t)
|
|
|
|
ymag : Y Magnetic field (milli tesla) (int16_t)
|
|
|
|
zmag : Z Magnetic field (milli tesla) (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.scaled_imu_encode(usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def gps_status_encode(self, satellites_visible, satellite_prn, satellite_used, satellite_elevation, satellite_azimuth, satellite_snr):
|
|
|
|
'''
|
|
|
|
The positioning status, as reported by GPS. This message is intended
|
|
|
|
to display status information about each satellite
|
|
|
|
visible to the receiver. See message GLOBAL_POSITION
|
|
|
|
for the global position estimate. This message can
|
|
|
|
contain information for up to 20 satellites.
|
|
|
|
|
|
|
|
satellites_visible : Number of satellites visible (uint8_t)
|
|
|
|
satellite_prn : Global satellite ID (int8_t)
|
|
|
|
satellite_used : 0: Satellite not used, 1: used for localization (int8_t)
|
|
|
|
satellite_elevation : Elevation (0: right on top of receiver, 90: on the horizon) of satellite (int8_t)
|
|
|
|
satellite_azimuth : Direction of satellite, 0: 0 deg, 255: 360 deg. (int8_t)
|
|
|
|
satellite_snr : Signal to noise ratio of satellite (int8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_gps_status_message(satellites_visible, satellite_prn, satellite_used, satellite_elevation, satellite_azimuth, satellite_snr)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def gps_status_send(self, satellites_visible, satellite_prn, satellite_used, satellite_elevation, satellite_azimuth, satellite_snr):
|
|
|
|
'''
|
|
|
|
The positioning status, as reported by GPS. This message is intended
|
|
|
|
to display status information about each satellite
|
|
|
|
visible to the receiver. See message GLOBAL_POSITION
|
|
|
|
for the global position estimate. This message can
|
|
|
|
contain information for up to 20 satellites.
|
|
|
|
|
|
|
|
satellites_visible : Number of satellites visible (uint8_t)
|
|
|
|
satellite_prn : Global satellite ID (int8_t)
|
|
|
|
satellite_used : 0: Satellite not used, 1: used for localization (int8_t)
|
|
|
|
satellite_elevation : Elevation (0: right on top of receiver, 90: on the horizon) of satellite (int8_t)
|
|
|
|
satellite_azimuth : Direction of satellite, 0: 0 deg, 255: 360 deg. (int8_t)
|
|
|
|
satellite_snr : Signal to noise ratio of satellite (int8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.gps_status_encode(satellites_visible, satellite_prn, satellite_used, satellite_elevation, satellite_azimuth, satellite_snr))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def raw_imu_encode(self, usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
|
|
|
|
'''
|
|
|
|
The RAW IMU readings for the usual 9DOF sensor setup. This message
|
|
|
|
should always contain the true raw values without any
|
|
|
|
scaling to allow data capture and system debugging.
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
xacc : X acceleration (raw) (int16_t)
|
|
|
|
yacc : Y acceleration (raw) (int16_t)
|
|
|
|
zacc : Z acceleration (raw) (int16_t)
|
|
|
|
xgyro : Angular speed around X axis (raw) (int16_t)
|
|
|
|
ygyro : Angular speed around Y axis (raw) (int16_t)
|
|
|
|
zgyro : Angular speed around Z axis (raw) (int16_t)
|
|
|
|
xmag : X Magnetic field (raw) (int16_t)
|
|
|
|
ymag : Y Magnetic field (raw) (int16_t)
|
|
|
|
zmag : Z Magnetic field (raw) (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_raw_imu_message(usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def raw_imu_send(self, usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag):
|
|
|
|
'''
|
|
|
|
The RAW IMU readings for the usual 9DOF sensor setup. This message
|
|
|
|
should always contain the true raw values without any
|
|
|
|
scaling to allow data capture and system debugging.
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
xacc : X acceleration (raw) (int16_t)
|
|
|
|
yacc : Y acceleration (raw) (int16_t)
|
|
|
|
zacc : Z acceleration (raw) (int16_t)
|
|
|
|
xgyro : Angular speed around X axis (raw) (int16_t)
|
|
|
|
ygyro : Angular speed around Y axis (raw) (int16_t)
|
|
|
|
zgyro : Angular speed around Z axis (raw) (int16_t)
|
|
|
|
xmag : X Magnetic field (raw) (int16_t)
|
|
|
|
ymag : Y Magnetic field (raw) (int16_t)
|
|
|
|
zmag : Z Magnetic field (raw) (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.raw_imu_encode(usec, xacc, yacc, zacc, xgyro, ygyro, zgyro, xmag, ymag, zmag))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def raw_pressure_encode(self, usec, press_abs, press_diff1, press_diff2, temperature):
|
|
|
|
'''
|
|
|
|
The RAW pressure readings for the typical setup of one absolute
|
|
|
|
pressure and one differential pressure sensor. The
|
|
|
|
sensor values should be the raw, UNSCALED ADC values.
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
press_abs : Absolute pressure (raw) (int16_t)
|
|
|
|
press_diff1 : Differential pressure 1 (raw) (int16_t)
|
|
|
|
press_diff2 : Differential pressure 2 (raw) (int16_t)
|
|
|
|
temperature : Raw Temperature measurement (raw) (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_raw_pressure_message(usec, press_abs, press_diff1, press_diff2, temperature)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def raw_pressure_send(self, usec, press_abs, press_diff1, press_diff2, temperature):
|
|
|
|
'''
|
|
|
|
The RAW pressure readings for the typical setup of one absolute
|
|
|
|
pressure and one differential pressure sensor. The
|
|
|
|
sensor values should be the raw, UNSCALED ADC values.
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
press_abs : Absolute pressure (raw) (int16_t)
|
|
|
|
press_diff1 : Differential pressure 1 (raw) (int16_t)
|
|
|
|
press_diff2 : Differential pressure 2 (raw) (int16_t)
|
|
|
|
temperature : Raw Temperature measurement (raw) (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.raw_pressure_encode(usec, press_abs, press_diff1, press_diff2, temperature))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def scaled_pressure_encode(self, usec, press_abs, press_diff, temperature):
|
|
|
|
'''
|
|
|
|
The pressure readings for the typical setup of one absolute and
|
|
|
|
differential pressure sensor. The units are as
|
|
|
|
specified in each field.
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
press_abs : Absolute pressure (hectopascal) (float)
|
|
|
|
press_diff : Differential pressure 1 (hectopascal) (float)
|
|
|
|
temperature : Temperature measurement (0.01 degrees celsius) (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_scaled_pressure_message(usec, press_abs, press_diff, temperature)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def scaled_pressure_send(self, usec, press_abs, press_diff, temperature):
|
|
|
|
'''
|
|
|
|
The pressure readings for the typical setup of one absolute and
|
|
|
|
differential pressure sensor. The units are as
|
|
|
|
specified in each field.
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
press_abs : Absolute pressure (hectopascal) (float)
|
|
|
|
press_diff : Differential pressure 1 (hectopascal) (float)
|
|
|
|
temperature : Temperature measurement (0.01 degrees celsius) (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.scaled_pressure_encode(usec, press_abs, press_diff, temperature))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def attitude_encode(self, usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed):
|
|
|
|
'''
|
|
|
|
The attitude in the aeronautical frame (right-handed, Z-down, X-front,
|
|
|
|
Y-right).
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
roll : Roll angle (rad) (float)
|
|
|
|
pitch : Pitch angle (rad) (float)
|
|
|
|
yaw : Yaw angle (rad) (float)
|
|
|
|
rollspeed : Roll angular speed (rad/s) (float)
|
|
|
|
pitchspeed : Pitch angular speed (rad/s) (float)
|
|
|
|
yawspeed : Yaw angular speed (rad/s) (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_attitude_message(usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def attitude_send(self, usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed):
|
|
|
|
'''
|
|
|
|
The attitude in the aeronautical frame (right-handed, Z-down, X-front,
|
|
|
|
Y-right).
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
roll : Roll angle (rad) (float)
|
|
|
|
pitch : Pitch angle (rad) (float)
|
|
|
|
yaw : Yaw angle (rad) (float)
|
|
|
|
rollspeed : Roll angular speed (rad/s) (float)
|
|
|
|
pitchspeed : Pitch angular speed (rad/s) (float)
|
|
|
|
yawspeed : Yaw angular speed (rad/s) (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.attitude_encode(usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def local_position_encode(self, usec, x, y, z, vx, vy, vz):
|
|
|
|
'''
|
|
|
|
The filtered local position (e.g. fused computer vision and
|
|
|
|
accelerometers). Coordinate frame is right-handed,
|
|
|
|
Z-axis down (aeronautical frame)
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
x : X Position (float)
|
|
|
|
y : Y Position (float)
|
|
|
|
z : Z Position (float)
|
|
|
|
vx : X Speed (float)
|
|
|
|
vy : Y Speed (float)
|
|
|
|
vz : Z Speed (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_local_position_message(usec, x, y, z, vx, vy, vz)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def local_position_send(self, usec, x, y, z, vx, vy, vz):
|
|
|
|
'''
|
|
|
|
The filtered local position (e.g. fused computer vision and
|
|
|
|
accelerometers). Coordinate frame is right-handed,
|
|
|
|
Z-axis down (aeronautical frame)
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
x : X Position (float)
|
|
|
|
y : Y Position (float)
|
|
|
|
z : Z Position (float)
|
|
|
|
vx : X Speed (float)
|
|
|
|
vy : Y Speed (float)
|
|
|
|
vz : Z Speed (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.local_position_encode(usec, x, y, z, vx, vy, vz))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def global_position_encode(self, usec, lat, lon, alt, vx, vy, vz):
|
|
|
|
'''
|
|
|
|
The filtered global position (e.g. fused GPS and accelerometers).
|
|
|
|
Coordinate frame is right-handed, Z-axis up (GPS
|
|
|
|
frame)
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since unix epoch) (uint64_t)
|
|
|
|
lat : Latitude, in degrees (float)
|
|
|
|
lon : Longitude, in degrees (float)
|
|
|
|
alt : Absolute altitude, in meters (float)
|
|
|
|
vx : X Speed (in Latitude direction, positive: going north) (float)
|
|
|
|
vy : Y Speed (in Longitude direction, positive: going east) (float)
|
|
|
|
vz : Z Speed (in Altitude direction, positive: going up) (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_global_position_message(usec, lat, lon, alt, vx, vy, vz)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def global_position_send(self, usec, lat, lon, alt, vx, vy, vz):
|
|
|
|
'''
|
|
|
|
The filtered global position (e.g. fused GPS and accelerometers).
|
|
|
|
Coordinate frame is right-handed, Z-axis up (GPS
|
|
|
|
frame)
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since unix epoch) (uint64_t)
|
|
|
|
lat : Latitude, in degrees (float)
|
|
|
|
lon : Longitude, in degrees (float)
|
|
|
|
alt : Absolute altitude, in meters (float)
|
|
|
|
vx : X Speed (in Latitude direction, positive: going north) (float)
|
|
|
|
vy : Y Speed (in Longitude direction, positive: going east) (float)
|
|
|
|
vz : Z Speed (in Altitude direction, positive: going up) (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.global_position_encode(usec, lat, lon, alt, vx, vy, vz))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def gps_raw_encode(self, usec, fix_type, lat, lon, alt, eph, epv, v, hdg):
|
|
|
|
'''
|
|
|
|
The global position, as returned by the Global Positioning System
|
|
|
|
(GPS). This is NOT the global position estimate of the
|
|
|
|
sytem, but rather a RAW sensor value. See message
|
|
|
|
GLOBAL_POSITION for the global position estimate.
|
|
|
|
Coordinate frame is right-handed, Z-axis up (GPS
|
|
|
|
frame)
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
fix_type : 0-1: no fix, 2: 2D fix, 3: 3D fix. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. (uint8_t)
|
|
|
|
lat : Latitude in degrees (float)
|
|
|
|
lon : Longitude in degrees (float)
|
|
|
|
alt : Altitude in meters (float)
|
|
|
|
eph : GPS HDOP (float)
|
|
|
|
epv : GPS VDOP (float)
|
|
|
|
v : GPS ground speed (float)
|
|
|
|
hdg : Compass heading in degrees, 0..360 degrees (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_gps_raw_message(usec, fix_type, lat, lon, alt, eph, epv, v, hdg)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def gps_raw_send(self, usec, fix_type, lat, lon, alt, eph, epv, v, hdg):
|
|
|
|
'''
|
|
|
|
The global position, as returned by the Global Positioning System
|
|
|
|
(GPS). This is NOT the global position estimate of the
|
|
|
|
sytem, but rather a RAW sensor value. See message
|
|
|
|
GLOBAL_POSITION for the global position estimate.
|
|
|
|
Coordinate frame is right-handed, Z-axis up (GPS
|
|
|
|
frame)
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
fix_type : 0-1: no fix, 2: 2D fix, 3: 3D fix. Some applications will not use the value of this field unless it is at least two, so always correctly fill in the fix. (uint8_t)
|
|
|
|
lat : Latitude in degrees (float)
|
|
|
|
lon : Longitude in degrees (float)
|
|
|
|
alt : Altitude in meters (float)
|
|
|
|
eph : GPS HDOP (float)
|
|
|
|
epv : GPS VDOP (float)
|
|
|
|
v : GPS ground speed (float)
|
|
|
|
hdg : Compass heading in degrees, 0..360 degrees (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.gps_raw_encode(usec, fix_type, lat, lon, alt, eph, epv, v, hdg))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def sys_status_encode(self, mode, nav_mode, status, load, vbat, battery_remaining, packet_drop):
|
|
|
|
'''
|
|
|
|
The general system state. If the system is following the MAVLink
|
|
|
|
standard, the system state is mainly defined by three
|
|
|
|
orthogonal states/modes: The system mode, which is
|
|
|
|
either LOCKED (motors shut down and locked), MANUAL
|
|
|
|
(system under RC control), GUIDED (system with
|
|
|
|
autonomous position control, position setpoint
|
|
|
|
controlled manually) or AUTO (system guided by
|
|
|
|
path/waypoint planner). The NAV_MODE defined the
|
|
|
|
current flight state: LIFTOFF (often an open-loop
|
|
|
|
maneuver), LANDING, WAYPOINTS or VECTOR. This
|
|
|
|
represents the internal navigation state machine. The
|
|
|
|
system status shows wether the system is currently
|
|
|
|
active or not and if an emergency occured. During the
|
|
|
|
CRITICAL and EMERGENCY states the MAV is still
|
|
|
|
considered to be active, but should start emergency
|
|
|
|
procedures autonomously. After a failure occured it
|
|
|
|
should first move from active to critical to allow
|
|
|
|
manual intervention and then move to emergency after a
|
|
|
|
certain timeout.
|
|
|
|
|
|
|
|
mode : System mode, see MAV_MODE ENUM in mavlink/include/mavlink_types.h (uint8_t)
|
|
|
|
nav_mode : Navigation mode, see MAV_NAV_MODE ENUM (uint8_t)
|
|
|
|
status : System status flag, see MAV_STATUS ENUM (uint8_t)
|
|
|
|
load : Maximum usage in percent of the mainloop time, (0%: 0, 100%: 1000) should be always below 1000 (uint16_t)
|
|
|
|
vbat : Battery voltage, in millivolts (1 = 1 millivolt) (uint16_t)
|
|
|
|
battery_remaining : Remaining battery energy: (0%: 0, 100%: 1000) (uint16_t)
|
|
|
|
packet_drop : Dropped packets (packets that were corrupted on reception on the MAV) (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_sys_status_message(mode, nav_mode, status, load, vbat, battery_remaining, packet_drop)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def sys_status_send(self, mode, nav_mode, status, load, vbat, battery_remaining, packet_drop):
|
|
|
|
'''
|
|
|
|
The general system state. If the system is following the MAVLink
|
|
|
|
standard, the system state is mainly defined by three
|
|
|
|
orthogonal states/modes: The system mode, which is
|
|
|
|
either LOCKED (motors shut down and locked), MANUAL
|
|
|
|
(system under RC control), GUIDED (system with
|
|
|
|
autonomous position control, position setpoint
|
|
|
|
controlled manually) or AUTO (system guided by
|
|
|
|
path/waypoint planner). The NAV_MODE defined the
|
|
|
|
current flight state: LIFTOFF (often an open-loop
|
|
|
|
maneuver), LANDING, WAYPOINTS or VECTOR. This
|
|
|
|
represents the internal navigation state machine. The
|
|
|
|
system status shows wether the system is currently
|
|
|
|
active or not and if an emergency occured. During the
|
|
|
|
CRITICAL and EMERGENCY states the MAV is still
|
|
|
|
considered to be active, but should start emergency
|
|
|
|
procedures autonomously. After a failure occured it
|
|
|
|
should first move from active to critical to allow
|
|
|
|
manual intervention and then move to emergency after a
|
|
|
|
certain timeout.
|
|
|
|
|
|
|
|
mode : System mode, see MAV_MODE ENUM in mavlink/include/mavlink_types.h (uint8_t)
|
|
|
|
nav_mode : Navigation mode, see MAV_NAV_MODE ENUM (uint8_t)
|
|
|
|
status : System status flag, see MAV_STATUS ENUM (uint8_t)
|
|
|
|
load : Maximum usage in percent of the mainloop time, (0%: 0, 100%: 1000) should be always below 1000 (uint16_t)
|
|
|
|
vbat : Battery voltage, in millivolts (1 = 1 millivolt) (uint16_t)
|
|
|
|
battery_remaining : Remaining battery energy: (0%: 0, 100%: 1000) (uint16_t)
|
|
|
|
packet_drop : Dropped packets (packets that were corrupted on reception on the MAV) (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.sys_status_encode(mode, nav_mode, status, load, vbat, battery_remaining, packet_drop))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def rc_channels_raw_encode(self, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, rssi):
|
|
|
|
'''
|
|
|
|
The RAW values of the RC channels received. The standard PPM
|
|
|
|
modulation is as follows: 1000 microseconds: 0%, 2000
|
|
|
|
microseconds: 100%. Individual receivers/transmitters
|
|
|
|
might violate this specification.
|
|
|
|
|
|
|
|
chan1_raw : RC channel 1 value, in microseconds (uint16_t)
|
|
|
|
chan2_raw : RC channel 2 value, in microseconds (uint16_t)
|
|
|
|
chan3_raw : RC channel 3 value, in microseconds (uint16_t)
|
|
|
|
chan4_raw : RC channel 4 value, in microseconds (uint16_t)
|
|
|
|
chan5_raw : RC channel 5 value, in microseconds (uint16_t)
|
|
|
|
chan6_raw : RC channel 6 value, in microseconds (uint16_t)
|
|
|
|
chan7_raw : RC channel 7 value, in microseconds (uint16_t)
|
|
|
|
chan8_raw : RC channel 8 value, in microseconds (uint16_t)
|
|
|
|
rssi : Receive signal strength indicator, 0: 0%, 255: 100% (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_rc_channels_raw_message(chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, rssi)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def rc_channels_raw_send(self, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, rssi):
|
|
|
|
'''
|
|
|
|
The RAW values of the RC channels received. The standard PPM
|
|
|
|
modulation is as follows: 1000 microseconds: 0%, 2000
|
|
|
|
microseconds: 100%. Individual receivers/transmitters
|
|
|
|
might violate this specification.
|
|
|
|
|
|
|
|
chan1_raw : RC channel 1 value, in microseconds (uint16_t)
|
|
|
|
chan2_raw : RC channel 2 value, in microseconds (uint16_t)
|
|
|
|
chan3_raw : RC channel 3 value, in microseconds (uint16_t)
|
|
|
|
chan4_raw : RC channel 4 value, in microseconds (uint16_t)
|
|
|
|
chan5_raw : RC channel 5 value, in microseconds (uint16_t)
|
|
|
|
chan6_raw : RC channel 6 value, in microseconds (uint16_t)
|
|
|
|
chan7_raw : RC channel 7 value, in microseconds (uint16_t)
|
|
|
|
chan8_raw : RC channel 8 value, in microseconds (uint16_t)
|
|
|
|
rssi : Receive signal strength indicator, 0: 0%, 255: 100% (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.rc_channels_raw_encode(chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw, rssi))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def rc_channels_scaled_encode(self, chan1_scaled, chan2_scaled, chan3_scaled, chan4_scaled, chan5_scaled, chan6_scaled, chan7_scaled, chan8_scaled, rssi):
|
|
|
|
'''
|
|
|
|
The scaled values of the RC channels received. (-100%) -10000, (0%) 0,
|
|
|
|
(100%) 10000
|
|
|
|
|
|
|
|
chan1_scaled : RC channel 1 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan2_scaled : RC channel 2 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan3_scaled : RC channel 3 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan4_scaled : RC channel 4 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan5_scaled : RC channel 5 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan6_scaled : RC channel 6 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan7_scaled : RC channel 7 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan8_scaled : RC channel 8 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
rssi : Receive signal strength indicator, 0: 0%, 255: 100% (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_rc_channels_scaled_message(chan1_scaled, chan2_scaled, chan3_scaled, chan4_scaled, chan5_scaled, chan6_scaled, chan7_scaled, chan8_scaled, rssi)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def rc_channels_scaled_send(self, chan1_scaled, chan2_scaled, chan3_scaled, chan4_scaled, chan5_scaled, chan6_scaled, chan7_scaled, chan8_scaled, rssi):
|
|
|
|
'''
|
|
|
|
The scaled values of the RC channels received. (-100%) -10000, (0%) 0,
|
|
|
|
(100%) 10000
|
|
|
|
|
|
|
|
chan1_scaled : RC channel 1 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan2_scaled : RC channel 2 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan3_scaled : RC channel 3 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan4_scaled : RC channel 4 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan5_scaled : RC channel 5 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan6_scaled : RC channel 6 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan7_scaled : RC channel 7 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
chan8_scaled : RC channel 8 value scaled, (-100%) -10000, (0%) 0, (100%) 10000 (int16_t)
|
|
|
|
rssi : Receive signal strength indicator, 0: 0%, 255: 100% (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.rc_channels_scaled_encode(chan1_scaled, chan2_scaled, chan3_scaled, chan4_scaled, chan5_scaled, chan6_scaled, chan7_scaled, chan8_scaled, rssi))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def servo_output_raw_encode(self, servo1_raw, servo2_raw, servo3_raw, servo4_raw, servo5_raw, servo6_raw, servo7_raw, servo8_raw):
|
|
|
|
'''
|
|
|
|
The RAW values of the servo outputs (for RC input from the remote, use
|
|
|
|
the RC_CHANNELS messages). The standard PPM modulation
|
|
|
|
is as follows: 1000 microseconds: 0%, 2000
|
|
|
|
microseconds: 100%.
|
|
|
|
|
|
|
|
servo1_raw : Servo output 1 value, in microseconds (uint16_t)
|
|
|
|
servo2_raw : Servo output 2 value, in microseconds (uint16_t)
|
|
|
|
servo3_raw : Servo output 3 value, in microseconds (uint16_t)
|
|
|
|
servo4_raw : Servo output 4 value, in microseconds (uint16_t)
|
|
|
|
servo5_raw : Servo output 5 value, in microseconds (uint16_t)
|
|
|
|
servo6_raw : Servo output 6 value, in microseconds (uint16_t)
|
|
|
|
servo7_raw : Servo output 7 value, in microseconds (uint16_t)
|
|
|
|
servo8_raw : Servo output 8 value, in microseconds (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_servo_output_raw_message(servo1_raw, servo2_raw, servo3_raw, servo4_raw, servo5_raw, servo6_raw, servo7_raw, servo8_raw)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def servo_output_raw_send(self, servo1_raw, servo2_raw, servo3_raw, servo4_raw, servo5_raw, servo6_raw, servo7_raw, servo8_raw):
|
|
|
|
'''
|
|
|
|
The RAW values of the servo outputs (for RC input from the remote, use
|
|
|
|
the RC_CHANNELS messages). The standard PPM modulation
|
|
|
|
is as follows: 1000 microseconds: 0%, 2000
|
|
|
|
microseconds: 100%.
|
|
|
|
|
|
|
|
servo1_raw : Servo output 1 value, in microseconds (uint16_t)
|
|
|
|
servo2_raw : Servo output 2 value, in microseconds (uint16_t)
|
|
|
|
servo3_raw : Servo output 3 value, in microseconds (uint16_t)
|
|
|
|
servo4_raw : Servo output 4 value, in microseconds (uint16_t)
|
|
|
|
servo5_raw : Servo output 5 value, in microseconds (uint16_t)
|
|
|
|
servo6_raw : Servo output 6 value, in microseconds (uint16_t)
|
|
|
|
servo7_raw : Servo output 7 value, in microseconds (uint16_t)
|
|
|
|
servo8_raw : Servo output 8 value, in microseconds (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.servo_output_raw_encode(servo1_raw, servo2_raw, servo3_raw, servo4_raw, servo5_raw, servo6_raw, servo7_raw, servo8_raw))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_encode(self, target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
|
|
|
|
'''
|
|
|
|
Message encoding a waypoint. This message is emitted to announce
|
|
|
|
the presence of a waypoint and to set a waypoint on
|
|
|
|
the system. The waypoint can be either in x, y, z
|
|
|
|
meters (type: LOCAL) or x:lat, y:lon, z:altitude.
|
|
|
|
Local frame is Z-down, right handed, global frame is
|
|
|
|
Z-up, right handed
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
seq : Sequence (uint16_t)
|
|
|
|
frame : The coordinate system of the waypoint. see MAV_FRAME in mavlink_types.h (uint8_t)
|
|
|
|
command : The scheduled action for the waypoint. see MAV_COMMAND in common.xml MAVLink specs (uint8_t)
|
|
|
|
current : false:0, true:1 (uint8_t)
|
|
|
|
autocontinue : autocontinue to next wp (uint8_t)
|
|
|
|
param1 : PARAM1 / For NAV command waypoints: Radius in which the waypoint is accepted as reached, in meters (float)
|
|
|
|
param2 : PARAM2 / For NAV command waypoints: Time that the MAV should stay inside the PARAM1 radius before advancing, in milliseconds (float)
|
|
|
|
param3 : PARAM3 / For LOITER command waypoints: Orbit to circle around the waypoint, in meters. If positive the orbit direction should be clockwise, if negative the orbit direction should be counter-clockwise. (float)
|
|
|
|
param4 : PARAM4 / For NAV and LOITER command waypoints: Yaw orientation in degrees, [0..360] 0 = NORTH (float)
|
|
|
|
x : PARAM5 / local: x position, global: latitude (float)
|
|
|
|
y : PARAM6 / y position: global: longitude (float)
|
|
|
|
z : PARAM7 / z position: global: altitude (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_waypoint_message(target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_send(self, target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z):
|
|
|
|
'''
|
|
|
|
Message encoding a waypoint. This message is emitted to announce
|
|
|
|
the presence of a waypoint and to set a waypoint on
|
|
|
|
the system. The waypoint can be either in x, y, z
|
|
|
|
meters (type: LOCAL) or x:lat, y:lon, z:altitude.
|
|
|
|
Local frame is Z-down, right handed, global frame is
|
|
|
|
Z-up, right handed
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
seq : Sequence (uint16_t)
|
|
|
|
frame : The coordinate system of the waypoint. see MAV_FRAME in mavlink_types.h (uint8_t)
|
|
|
|
command : The scheduled action for the waypoint. see MAV_COMMAND in common.xml MAVLink specs (uint8_t)
|
|
|
|
current : false:0, true:1 (uint8_t)
|
|
|
|
autocontinue : autocontinue to next wp (uint8_t)
|
|
|
|
param1 : PARAM1 / For NAV command waypoints: Radius in which the waypoint is accepted as reached, in meters (float)
|
|
|
|
param2 : PARAM2 / For NAV command waypoints: Time that the MAV should stay inside the PARAM1 radius before advancing, in milliseconds (float)
|
|
|
|
param3 : PARAM3 / For LOITER command waypoints: Orbit to circle around the waypoint, in meters. If positive the orbit direction should be clockwise, if negative the orbit direction should be counter-clockwise. (float)
|
|
|
|
param4 : PARAM4 / For NAV and LOITER command waypoints: Yaw orientation in degrees, [0..360] 0 = NORTH (float)
|
|
|
|
x : PARAM5 / local: x position, global: latitude (float)
|
|
|
|
y : PARAM6 / y position: global: longitude (float)
|
|
|
|
z : PARAM7 / z position: global: altitude (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.waypoint_encode(target_system, target_component, seq, frame, command, current, autocontinue, param1, param2, param3, param4, x, y, z))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_request_encode(self, target_system, target_component, seq):
|
|
|
|
'''
|
|
|
|
Request the information of the waypoint with the sequence number seq.
|
|
|
|
The response of the system to this message should be a
|
|
|
|
WAYPOINT message.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
seq : Sequence (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_waypoint_request_message(target_system, target_component, seq)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_request_send(self, target_system, target_component, seq):
|
|
|
|
'''
|
|
|
|
Request the information of the waypoint with the sequence number seq.
|
|
|
|
The response of the system to this message should be a
|
|
|
|
WAYPOINT message.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
seq : Sequence (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.waypoint_request_encode(target_system, target_component, seq))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_set_current_encode(self, target_system, target_component, seq):
|
|
|
|
'''
|
|
|
|
Set the waypoint with sequence number seq as current waypoint. This
|
|
|
|
means that the MAV will continue to this waypoint on
|
|
|
|
the shortest path (not following the waypoints in-
|
|
|
|
between).
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
seq : Sequence (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_waypoint_set_current_message(target_system, target_component, seq)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_set_current_send(self, target_system, target_component, seq):
|
|
|
|
'''
|
|
|
|
Set the waypoint with sequence number seq as current waypoint. This
|
|
|
|
means that the MAV will continue to this waypoint on
|
|
|
|
the shortest path (not following the waypoints in-
|
|
|
|
between).
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
seq : Sequence (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.waypoint_set_current_encode(target_system, target_component, seq))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_current_encode(self, seq):
|
|
|
|
'''
|
|
|
|
Message that announces the sequence number of the current active
|
|
|
|
waypoint. The MAV will fly towards this waypoint.
|
|
|
|
|
|
|
|
seq : Sequence (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_waypoint_current_message(seq)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_current_send(self, seq):
|
|
|
|
'''
|
|
|
|
Message that announces the sequence number of the current active
|
|
|
|
waypoint. The MAV will fly towards this waypoint.
|
|
|
|
|
|
|
|
seq : Sequence (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.waypoint_current_encode(seq))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_request_list_encode(self, target_system, target_component):
|
|
|
|
'''
|
|
|
|
Request the overall list of waypoints from the system/component.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_waypoint_request_list_message(target_system, target_component)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_request_list_send(self, target_system, target_component):
|
|
|
|
'''
|
|
|
|
Request the overall list of waypoints from the system/component.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.waypoint_request_list_encode(target_system, target_component))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_count_encode(self, target_system, target_component, count):
|
|
|
|
'''
|
|
|
|
This message is emitted as response to WAYPOINT_REQUEST_LIST by the
|
|
|
|
MAV. The GCS can then request the individual waypoints
|
|
|
|
based on the knowledge of the total number of
|
|
|
|
waypoints.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
count : Number of Waypoints in the Sequence (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_waypoint_count_message(target_system, target_component, count)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_count_send(self, target_system, target_component, count):
|
|
|
|
'''
|
|
|
|
This message is emitted as response to WAYPOINT_REQUEST_LIST by the
|
|
|
|
MAV. The GCS can then request the individual waypoints
|
|
|
|
based on the knowledge of the total number of
|
|
|
|
waypoints.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
count : Number of Waypoints in the Sequence (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.waypoint_count_encode(target_system, target_component, count))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_clear_all_encode(self, target_system, target_component):
|
|
|
|
'''
|
|
|
|
Delete all waypoints at once.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_waypoint_clear_all_message(target_system, target_component)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_clear_all_send(self, target_system, target_component):
|
|
|
|
'''
|
|
|
|
Delete all waypoints at once.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.waypoint_clear_all_encode(target_system, target_component))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_reached_encode(self, seq):
|
|
|
|
'''
|
|
|
|
A certain waypoint has been reached. The system will either hold this
|
|
|
|
position (or circle on the orbit) or (if the
|
|
|
|
autocontinue on the WP was set) continue to the next
|
|
|
|
waypoint.
|
|
|
|
|
|
|
|
seq : Sequence (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_waypoint_reached_message(seq)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_reached_send(self, seq):
|
|
|
|
'''
|
|
|
|
A certain waypoint has been reached. The system will either hold this
|
|
|
|
position (or circle on the orbit) or (if the
|
|
|
|
autocontinue on the WP was set) continue to the next
|
|
|
|
waypoint.
|
|
|
|
|
|
|
|
seq : Sequence (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.waypoint_reached_encode(seq))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_ack_encode(self, target_system, target_component, type):
|
|
|
|
'''
|
|
|
|
Ack message during waypoint handling. The type field states if this
|
|
|
|
message is a positive ack (type=0) or if an error
|
|
|
|
happened (type=non-zero).
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
type : 0: OK, 1: Error (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_waypoint_ack_message(target_system, target_component, type)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def waypoint_ack_send(self, target_system, target_component, type):
|
|
|
|
'''
|
|
|
|
Ack message during waypoint handling. The type field states if this
|
|
|
|
message is a positive ack (type=0) or if an error
|
|
|
|
happened (type=non-zero).
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
type : 0: OK, 1: Error (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.waypoint_ack_encode(target_system, target_component, type))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def gps_set_global_origin_encode(self, target_system, target_component, latitude, longitude, altitude):
|
|
|
|
'''
|
|
|
|
As local waypoints exist, the global waypoint reference allows to
|
|
|
|
transform between the local coordinate frame and the
|
|
|
|
global (GPS) coordinate frame. This can be necessary
|
|
|
|
when e.g. in- and outdoor settings are connected and
|
|
|
|
the MAV should move from in- to outdoor.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
latitude : global position * 1E7 (int32_t)
|
|
|
|
longitude : global position * 1E7 (int32_t)
|
|
|
|
altitude : global position * 1000 (int32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_gps_set_global_origin_message(target_system, target_component, latitude, longitude, altitude)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def gps_set_global_origin_send(self, target_system, target_component, latitude, longitude, altitude):
|
|
|
|
'''
|
|
|
|
As local waypoints exist, the global waypoint reference allows to
|
|
|
|
transform between the local coordinate frame and the
|
|
|
|
global (GPS) coordinate frame. This can be necessary
|
|
|
|
when e.g. in- and outdoor settings are connected and
|
|
|
|
the MAV should move from in- to outdoor.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
latitude : global position * 1E7 (int32_t)
|
|
|
|
longitude : global position * 1E7 (int32_t)
|
|
|
|
altitude : global position * 1000 (int32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.gps_set_global_origin_encode(target_system, target_component, latitude, longitude, altitude))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def gps_local_origin_set_encode(self, latitude, longitude, altitude):
|
|
|
|
'''
|
|
|
|
Once the MAV sets a new GPS-Local correspondence, this message
|
|
|
|
announces the origin (0,0,0) position
|
|
|
|
|
|
|
|
latitude : Latitude (WGS84), expressed as * 1E7 (int32_t)
|
|
|
|
longitude : Longitude (WGS84), expressed as * 1E7 (int32_t)
|
|
|
|
altitude : Altitude(WGS84), expressed as * 1000 (int32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_gps_local_origin_set_message(latitude, longitude, altitude)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def gps_local_origin_set_send(self, latitude, longitude, altitude):
|
|
|
|
'''
|
|
|
|
Once the MAV sets a new GPS-Local correspondence, this message
|
|
|
|
announces the origin (0,0,0) position
|
|
|
|
|
|
|
|
latitude : Latitude (WGS84), expressed as * 1E7 (int32_t)
|
|
|
|
longitude : Longitude (WGS84), expressed as * 1E7 (int32_t)
|
|
|
|
altitude : Altitude(WGS84), expressed as * 1000 (int32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.gps_local_origin_set_encode(latitude, longitude, altitude))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def local_position_setpoint_set_encode(self, target_system, target_component, x, y, z, yaw):
|
|
|
|
'''
|
|
|
|
Set the setpoint for a local position controller. This is the position
|
|
|
|
in local coordinates the MAV should fly to. This
|
|
|
|
message is sent by the path/waypoint planner to the
|
|
|
|
onboard position controller. As some MAVs have a
|
|
|
|
degree of freedom in yaw (e.g. all
|
|
|
|
helicopters/quadrotors), the desired yaw angle is part
|
|
|
|
of the message.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
x : x position (float)
|
|
|
|
y : y position (float)
|
|
|
|
z : z position (float)
|
|
|
|
yaw : Desired yaw angle (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_local_position_setpoint_set_message(target_system, target_component, x, y, z, yaw)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def local_position_setpoint_set_send(self, target_system, target_component, x, y, z, yaw):
|
|
|
|
'''
|
|
|
|
Set the setpoint for a local position controller. This is the position
|
|
|
|
in local coordinates the MAV should fly to. This
|
|
|
|
message is sent by the path/waypoint planner to the
|
|
|
|
onboard position controller. As some MAVs have a
|
|
|
|
degree of freedom in yaw (e.g. all
|
|
|
|
helicopters/quadrotors), the desired yaw angle is part
|
|
|
|
of the message.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
x : x position (float)
|
|
|
|
y : y position (float)
|
|
|
|
z : z position (float)
|
|
|
|
yaw : Desired yaw angle (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.local_position_setpoint_set_encode(target_system, target_component, x, y, z, yaw))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def local_position_setpoint_encode(self, x, y, z, yaw):
|
|
|
|
'''
|
|
|
|
Transmit the current local setpoint of the controller to other MAVs
|
|
|
|
(collision avoidance) and to the GCS.
|
|
|
|
|
|
|
|
x : x position (float)
|
|
|
|
y : y position (float)
|
|
|
|
z : z position (float)
|
|
|
|
yaw : Desired yaw angle (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_local_position_setpoint_message(x, y, z, yaw)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def local_position_setpoint_send(self, x, y, z, yaw):
|
|
|
|
'''
|
|
|
|
Transmit the current local setpoint of the controller to other MAVs
|
|
|
|
(collision avoidance) and to the GCS.
|
|
|
|
|
|
|
|
x : x position (float)
|
|
|
|
y : y position (float)
|
|
|
|
z : z position (float)
|
|
|
|
yaw : Desired yaw angle (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.local_position_setpoint_encode(x, y, z, yaw))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def control_status_encode(self, position_fix, vision_fix, gps_fix, ahrs_health, control_att, control_pos_xy, control_pos_z, control_pos_yaw):
|
|
|
|
'''
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
|
|
|
|
position_fix : Position fix: 0: lost, 2: 2D position fix, 3: 3D position fix (uint8_t)
|
|
|
|
vision_fix : Vision position fix: 0: lost, 1: 2D local position hold, 2: 2D global position fix, 3: 3D global position fix (uint8_t)
|
|
|
|
gps_fix : GPS position fix: 0: no reception, 1: Minimum 1 satellite, but no position fix, 2: 2D position fix, 3: 3D position fix (uint8_t)
|
|
|
|
ahrs_health : Attitude estimation health: 0: poor, 255: excellent (uint8_t)
|
|
|
|
control_att : 0: Attitude control disabled, 1: enabled (uint8_t)
|
|
|
|
control_pos_xy : 0: X, Y position control disabled, 1: enabled (uint8_t)
|
|
|
|
control_pos_z : 0: Z position control disabled, 1: enabled (uint8_t)
|
|
|
|
control_pos_yaw : 0: Yaw angle control disabled, 1: enabled (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_control_status_message(position_fix, vision_fix, gps_fix, ahrs_health, control_att, control_pos_xy, control_pos_z, control_pos_yaw)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def control_status_send(self, position_fix, vision_fix, gps_fix, ahrs_health, control_att, control_pos_xy, control_pos_z, control_pos_yaw):
|
|
|
|
'''
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
|
|
|
|
position_fix : Position fix: 0: lost, 2: 2D position fix, 3: 3D position fix (uint8_t)
|
|
|
|
vision_fix : Vision position fix: 0: lost, 1: 2D local position hold, 2: 2D global position fix, 3: 3D global position fix (uint8_t)
|
|
|
|
gps_fix : GPS position fix: 0: no reception, 1: Minimum 1 satellite, but no position fix, 2: 2D position fix, 3: 3D position fix (uint8_t)
|
|
|
|
ahrs_health : Attitude estimation health: 0: poor, 255: excellent (uint8_t)
|
|
|
|
control_att : 0: Attitude control disabled, 1: enabled (uint8_t)
|
|
|
|
control_pos_xy : 0: X, Y position control disabled, 1: enabled (uint8_t)
|
|
|
|
control_pos_z : 0: Z position control disabled, 1: enabled (uint8_t)
|
|
|
|
control_pos_yaw : 0: Yaw angle control disabled, 1: enabled (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.control_status_encode(position_fix, vision_fix, gps_fix, ahrs_health, control_att, control_pos_xy, control_pos_z, control_pos_yaw))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def safety_set_allowed_area_encode(self, target_system, target_component, frame, p1x, p1y, p1z, p2x, p2y, p2z):
|
|
|
|
'''
|
|
|
|
Set a safety zone (volume), which is defined by two corners of a cube.
|
|
|
|
This message can be used to tell the MAV which
|
|
|
|
setpoints/waypoints to accept and which to reject.
|
|
|
|
Safety areas are often enforced by national or
|
|
|
|
competition regulations.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
frame : Coordinate frame, as defined by MAV_FRAME enum in mavlink_types.h. Can be either global, GPS, right-handed with Z axis up or local, right handed, Z axis down. (uint8_t)
|
|
|
|
p1x : x position 1 / Latitude 1 (float)
|
|
|
|
p1y : y position 1 / Longitude 1 (float)
|
|
|
|
p1z : z position 1 / Altitude 1 (float)
|
|
|
|
p2x : x position 2 / Latitude 2 (float)
|
|
|
|
p2y : y position 2 / Longitude 2 (float)
|
|
|
|
p2z : z position 2 / Altitude 2 (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_safety_set_allowed_area_message(target_system, target_component, frame, p1x, p1y, p1z, p2x, p2y, p2z)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def safety_set_allowed_area_send(self, target_system, target_component, frame, p1x, p1y, p1z, p2x, p2y, p2z):
|
|
|
|
'''
|
|
|
|
Set a safety zone (volume), which is defined by two corners of a cube.
|
|
|
|
This message can be used to tell the MAV which
|
|
|
|
setpoints/waypoints to accept and which to reject.
|
|
|
|
Safety areas are often enforced by national or
|
|
|
|
competition regulations.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
frame : Coordinate frame, as defined by MAV_FRAME enum in mavlink_types.h. Can be either global, GPS, right-handed with Z axis up or local, right handed, Z axis down. (uint8_t)
|
|
|
|
p1x : x position 1 / Latitude 1 (float)
|
|
|
|
p1y : y position 1 / Longitude 1 (float)
|
|
|
|
p1z : z position 1 / Altitude 1 (float)
|
|
|
|
p2x : x position 2 / Latitude 2 (float)
|
|
|
|
p2y : y position 2 / Longitude 2 (float)
|
|
|
|
p2z : z position 2 / Altitude 2 (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.safety_set_allowed_area_encode(target_system, target_component, frame, p1x, p1y, p1z, p2x, p2y, p2z))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def safety_allowed_area_encode(self, frame, p1x, p1y, p1z, p2x, p2y, p2z):
|
|
|
|
'''
|
|
|
|
Read out the safety zone the MAV currently assumes.
|
|
|
|
|
|
|
|
frame : Coordinate frame, as defined by MAV_FRAME enum in mavlink_types.h. Can be either global, GPS, right-handed with Z axis up or local, right handed, Z axis down. (uint8_t)
|
|
|
|
p1x : x position 1 / Latitude 1 (float)
|
|
|
|
p1y : y position 1 / Longitude 1 (float)
|
|
|
|
p1z : z position 1 / Altitude 1 (float)
|
|
|
|
p2x : x position 2 / Latitude 2 (float)
|
|
|
|
p2y : y position 2 / Longitude 2 (float)
|
|
|
|
p2z : z position 2 / Altitude 2 (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_safety_allowed_area_message(frame, p1x, p1y, p1z, p2x, p2y, p2z)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def safety_allowed_area_send(self, frame, p1x, p1y, p1z, p2x, p2y, p2z):
|
|
|
|
'''
|
|
|
|
Read out the safety zone the MAV currently assumes.
|
|
|
|
|
|
|
|
frame : Coordinate frame, as defined by MAV_FRAME enum in mavlink_types.h. Can be either global, GPS, right-handed with Z axis up or local, right handed, Z axis down. (uint8_t)
|
|
|
|
p1x : x position 1 / Latitude 1 (float)
|
|
|
|
p1y : y position 1 / Longitude 1 (float)
|
|
|
|
p1z : z position 1 / Altitude 1 (float)
|
|
|
|
p2x : x position 2 / Latitude 2 (float)
|
|
|
|
p2y : y position 2 / Longitude 2 (float)
|
|
|
|
p2z : z position 2 / Altitude 2 (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.safety_allowed_area_encode(frame, p1x, p1y, p1z, p2x, p2y, p2z))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def set_roll_pitch_yaw_thrust_encode(self, target_system, target_component, roll, pitch, yaw, thrust):
|
|
|
|
'''
|
|
|
|
Set roll, pitch and yaw.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
roll : Desired roll angle in radians (float)
|
|
|
|
pitch : Desired pitch angle in radians (float)
|
|
|
|
yaw : Desired yaw angle in radians (float)
|
|
|
|
thrust : Collective thrust, normalized to 0 .. 1 (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_set_roll_pitch_yaw_thrust_message(target_system, target_component, roll, pitch, yaw, thrust)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def set_roll_pitch_yaw_thrust_send(self, target_system, target_component, roll, pitch, yaw, thrust):
|
|
|
|
'''
|
|
|
|
Set roll, pitch and yaw.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
roll : Desired roll angle in radians (float)
|
|
|
|
pitch : Desired pitch angle in radians (float)
|
|
|
|
yaw : Desired yaw angle in radians (float)
|
|
|
|
thrust : Collective thrust, normalized to 0 .. 1 (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.set_roll_pitch_yaw_thrust_encode(target_system, target_component, roll, pitch, yaw, thrust))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def set_roll_pitch_yaw_speed_thrust_encode(self, target_system, target_component, roll_speed, pitch_speed, yaw_speed, thrust):
|
|
|
|
'''
|
|
|
|
Set roll, pitch and yaw.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
roll_speed : Desired roll angular speed in rad/s (float)
|
|
|
|
pitch_speed : Desired pitch angular speed in rad/s (float)
|
|
|
|
yaw_speed : Desired yaw angular speed in rad/s (float)
|
|
|
|
thrust : Collective thrust, normalized to 0 .. 1 (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_set_roll_pitch_yaw_speed_thrust_message(target_system, target_component, roll_speed, pitch_speed, yaw_speed, thrust)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def set_roll_pitch_yaw_speed_thrust_send(self, target_system, target_component, roll_speed, pitch_speed, yaw_speed, thrust):
|
|
|
|
'''
|
|
|
|
Set roll, pitch and yaw.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
roll_speed : Desired roll angular speed in rad/s (float)
|
|
|
|
pitch_speed : Desired pitch angular speed in rad/s (float)
|
|
|
|
yaw_speed : Desired yaw angular speed in rad/s (float)
|
|
|
|
thrust : Collective thrust, normalized to 0 .. 1 (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.set_roll_pitch_yaw_speed_thrust_encode(target_system, target_component, roll_speed, pitch_speed, yaw_speed, thrust))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def roll_pitch_yaw_thrust_setpoint_encode(self, time_us, roll, pitch, yaw, thrust):
|
|
|
|
'''
|
|
|
|
Setpoint in roll, pitch, yaw currently active on the system.
|
|
|
|
|
|
|
|
time_us : Timestamp in micro seconds since unix epoch (uint64_t)
|
|
|
|
roll : Desired roll angle in radians (float)
|
|
|
|
pitch : Desired pitch angle in radians (float)
|
|
|
|
yaw : Desired yaw angle in radians (float)
|
|
|
|
thrust : Collective thrust, normalized to 0 .. 1 (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_roll_pitch_yaw_thrust_setpoint_message(time_us, roll, pitch, yaw, thrust)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def roll_pitch_yaw_thrust_setpoint_send(self, time_us, roll, pitch, yaw, thrust):
|
|
|
|
'''
|
|
|
|
Setpoint in roll, pitch, yaw currently active on the system.
|
|
|
|
|
|
|
|
time_us : Timestamp in micro seconds since unix epoch (uint64_t)
|
|
|
|
roll : Desired roll angle in radians (float)
|
|
|
|
pitch : Desired pitch angle in radians (float)
|
|
|
|
yaw : Desired yaw angle in radians (float)
|
|
|
|
thrust : Collective thrust, normalized to 0 .. 1 (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.roll_pitch_yaw_thrust_setpoint_encode(time_us, roll, pitch, yaw, thrust))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def roll_pitch_yaw_speed_thrust_setpoint_encode(self, time_us, roll_speed, pitch_speed, yaw_speed, thrust):
|
|
|
|
'''
|
|
|
|
Setpoint in rollspeed, pitchspeed, yawspeed currently active on the
|
|
|
|
system.
|
|
|
|
|
|
|
|
time_us : Timestamp in micro seconds since unix epoch (uint64_t)
|
|
|
|
roll_speed : Desired roll angular speed in rad/s (float)
|
|
|
|
pitch_speed : Desired pitch angular speed in rad/s (float)
|
|
|
|
yaw_speed : Desired yaw angular speed in rad/s (float)
|
|
|
|
thrust : Collective thrust, normalized to 0 .. 1 (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_roll_pitch_yaw_speed_thrust_setpoint_message(time_us, roll_speed, pitch_speed, yaw_speed, thrust)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def roll_pitch_yaw_speed_thrust_setpoint_send(self, time_us, roll_speed, pitch_speed, yaw_speed, thrust):
|
|
|
|
'''
|
|
|
|
Setpoint in rollspeed, pitchspeed, yawspeed currently active on the
|
|
|
|
system.
|
|
|
|
|
|
|
|
time_us : Timestamp in micro seconds since unix epoch (uint64_t)
|
|
|
|
roll_speed : Desired roll angular speed in rad/s (float)
|
|
|
|
pitch_speed : Desired pitch angular speed in rad/s (float)
|
|
|
|
yaw_speed : Desired yaw angular speed in rad/s (float)
|
|
|
|
thrust : Collective thrust, normalized to 0 .. 1 (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.roll_pitch_yaw_speed_thrust_setpoint_encode(time_us, roll_speed, pitch_speed, yaw_speed, thrust))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def nav_controller_output_encode(self, nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error):
|
|
|
|
'''
|
|
|
|
Outputs of the APM navigation controller. The primary use of this
|
|
|
|
message is to check the response and signs of the
|
|
|
|
controller before actual flight and to assist with
|
|
|
|
tuning controller parameters
|
|
|
|
|
|
|
|
nav_roll : Current desired roll in degrees (float)
|
|
|
|
nav_pitch : Current desired pitch in degrees (float)
|
|
|
|
nav_bearing : Current desired heading in degrees (int16_t)
|
|
|
|
target_bearing : Bearing to current waypoint/target in degrees (int16_t)
|
|
|
|
wp_dist : Distance to active waypoint in meters (uint16_t)
|
|
|
|
alt_error : Current altitude error in meters (float)
|
|
|
|
aspd_error : Current airspeed error in meters/second (float)
|
|
|
|
xtrack_error : Current crosstrack error on x-y plane in meters (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_nav_controller_output_message(nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def nav_controller_output_send(self, nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error):
|
|
|
|
'''
|
|
|
|
Outputs of the APM navigation controller. The primary use of this
|
|
|
|
message is to check the response and signs of the
|
|
|
|
controller before actual flight and to assist with
|
|
|
|
tuning controller parameters
|
|
|
|
|
|
|
|
nav_roll : Current desired roll in degrees (float)
|
|
|
|
nav_pitch : Current desired pitch in degrees (float)
|
|
|
|
nav_bearing : Current desired heading in degrees (int16_t)
|
|
|
|
target_bearing : Bearing to current waypoint/target in degrees (int16_t)
|
|
|
|
wp_dist : Distance to active waypoint in meters (uint16_t)
|
|
|
|
alt_error : Current altitude error in meters (float)
|
|
|
|
aspd_error : Current airspeed error in meters/second (float)
|
|
|
|
xtrack_error : Current crosstrack error on x-y plane in meters (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.nav_controller_output_encode(nav_roll, nav_pitch, nav_bearing, target_bearing, wp_dist, alt_error, aspd_error, xtrack_error))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def position_target_encode(self, x, y, z, yaw):
|
|
|
|
'''
|
|
|
|
The goal position of the system. This position is the input to any
|
|
|
|
navigation or path planning algorithm and does NOT
|
|
|
|
represent the current controller setpoint.
|
|
|
|
|
|
|
|
x : x position (float)
|
|
|
|
y : y position (float)
|
|
|
|
z : z position (float)
|
|
|
|
yaw : yaw orientation in radians, 0 = NORTH (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_position_target_message(x, y, z, yaw)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def position_target_send(self, x, y, z, yaw):
|
|
|
|
'''
|
|
|
|
The goal position of the system. This position is the input to any
|
|
|
|
navigation or path planning algorithm and does NOT
|
|
|
|
represent the current controller setpoint.
|
|
|
|
|
|
|
|
x : x position (float)
|
|
|
|
y : y position (float)
|
|
|
|
z : z position (float)
|
|
|
|
yaw : yaw orientation in radians, 0 = NORTH (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.position_target_encode(x, y, z, yaw))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def state_correction_encode(self, xErr, yErr, zErr, rollErr, pitchErr, yawErr, vxErr, vyErr, vzErr):
|
|
|
|
'''
|
|
|
|
Corrects the systems state by adding an error correction term to the
|
|
|
|
position and velocity, and by rotating the attitude by
|
|
|
|
a correction angle.
|
|
|
|
|
|
|
|
xErr : x position error (float)
|
|
|
|
yErr : y position error (float)
|
|
|
|
zErr : z position error (float)
|
|
|
|
rollErr : roll error (radians) (float)
|
|
|
|
pitchErr : pitch error (radians) (float)
|
|
|
|
yawErr : yaw error (radians) (float)
|
|
|
|
vxErr : x velocity (float)
|
|
|
|
vyErr : y velocity (float)
|
|
|
|
vzErr : z velocity (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_state_correction_message(xErr, yErr, zErr, rollErr, pitchErr, yawErr, vxErr, vyErr, vzErr)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def state_correction_send(self, xErr, yErr, zErr, rollErr, pitchErr, yawErr, vxErr, vyErr, vzErr):
|
|
|
|
'''
|
|
|
|
Corrects the systems state by adding an error correction term to the
|
|
|
|
position and velocity, and by rotating the attitude by
|
|
|
|
a correction angle.
|
|
|
|
|
|
|
|
xErr : x position error (float)
|
|
|
|
yErr : y position error (float)
|
|
|
|
zErr : z position error (float)
|
|
|
|
rollErr : roll error (radians) (float)
|
|
|
|
pitchErr : pitch error (radians) (float)
|
|
|
|
yawErr : yaw error (radians) (float)
|
|
|
|
vxErr : x velocity (float)
|
|
|
|
vyErr : y velocity (float)
|
|
|
|
vzErr : z velocity (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.state_correction_encode(xErr, yErr, zErr, rollErr, pitchErr, yawErr, vxErr, vyErr, vzErr))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def set_altitude_encode(self, target, mode):
|
|
|
|
'''
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
|
|
|
|
target : The system setting the altitude (uint8_t)
|
|
|
|
mode : The new altitude in meters (uint32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_set_altitude_message(target, mode)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def set_altitude_send(self, target, mode):
|
|
|
|
'''
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
|
|
|
|
target : The system setting the altitude (uint8_t)
|
|
|
|
mode : The new altitude in meters (uint32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.set_altitude_encode(target, mode))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def request_data_stream_encode(self, target_system, target_component, req_stream_id, req_message_rate, start_stop):
|
|
|
|
'''
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
|
|
|
|
target_system : The target requested to send the message stream. (uint8_t)
|
|
|
|
target_component : The target requested to send the message stream. (uint8_t)
|
|
|
|
req_stream_id : The ID of the requested message type (uint8_t)
|
|
|
|
req_message_rate : Update rate in Hertz (uint16_t)
|
|
|
|
start_stop : 1 to start sending, 0 to stop sending. (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_request_data_stream_message(target_system, target_component, req_stream_id, req_message_rate, start_stop)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def request_data_stream_send(self, target_system, target_component, req_stream_id, req_message_rate, start_stop):
|
|
|
|
'''
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
|
|
|
|
target_system : The target requested to send the message stream. (uint8_t)
|
|
|
|
target_component : The target requested to send the message stream. (uint8_t)
|
|
|
|
req_stream_id : The ID of the requested message type (uint8_t)
|
|
|
|
req_message_rate : Update rate in Hertz (uint16_t)
|
|
|
|
start_stop : 1 to start sending, 0 to stop sending. (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.request_data_stream_encode(target_system, target_component, req_stream_id, req_message_rate, start_stop))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def hil_state_encode(self, usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, xacc, yacc, zacc):
|
|
|
|
'''
|
|
|
|
This packet is useful for high throughput applications
|
|
|
|
such as hardware in the loop simulations.
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
roll : Roll angle (rad) (float)
|
|
|
|
pitch : Pitch angle (rad) (float)
|
|
|
|
yaw : Yaw angle (rad) (float)
|
|
|
|
rollspeed : Roll angular speed (rad/s) (float)
|
|
|
|
pitchspeed : Pitch angular speed (rad/s) (float)
|
|
|
|
yawspeed : Yaw angular speed (rad/s) (float)
|
|
|
|
lat : Latitude, expressed as * 1E7 (int32_t)
|
|
|
|
lon : Longitude, expressed as * 1E7 (int32_t)
|
|
|
|
alt : Altitude in meters, expressed as * 1000 (millimeters) (int32_t)
|
|
|
|
vx : Ground X Speed (Latitude), expressed as m/s * 100 (int16_t)
|
|
|
|
vy : Ground Y Speed (Longitude), expressed as m/s * 100 (int16_t)
|
|
|
|
vz : Ground Z Speed (Altitude), expressed as m/s * 100 (int16_t)
|
|
|
|
xacc : X acceleration (mg) (int16_t)
|
|
|
|
yacc : Y acceleration (mg) (int16_t)
|
|
|
|
zacc : Z acceleration (mg) (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_hil_state_message(usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, xacc, yacc, zacc)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def hil_state_send(self, usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, xacc, yacc, zacc):
|
|
|
|
'''
|
|
|
|
This packet is useful for high throughput applications
|
|
|
|
such as hardware in the loop simulations.
|
|
|
|
|
|
|
|
usec : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
roll : Roll angle (rad) (float)
|
|
|
|
pitch : Pitch angle (rad) (float)
|
|
|
|
yaw : Yaw angle (rad) (float)
|
|
|
|
rollspeed : Roll angular speed (rad/s) (float)
|
|
|
|
pitchspeed : Pitch angular speed (rad/s) (float)
|
|
|
|
yawspeed : Yaw angular speed (rad/s) (float)
|
|
|
|
lat : Latitude, expressed as * 1E7 (int32_t)
|
|
|
|
lon : Longitude, expressed as * 1E7 (int32_t)
|
|
|
|
alt : Altitude in meters, expressed as * 1000 (millimeters) (int32_t)
|
|
|
|
vx : Ground X Speed (Latitude), expressed as m/s * 100 (int16_t)
|
|
|
|
vy : Ground Y Speed (Longitude), expressed as m/s * 100 (int16_t)
|
|
|
|
vz : Ground Z Speed (Altitude), expressed as m/s * 100 (int16_t)
|
|
|
|
xacc : X acceleration (mg) (int16_t)
|
|
|
|
yacc : Y acceleration (mg) (int16_t)
|
|
|
|
zacc : Z acceleration (mg) (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.hil_state_encode(usec, roll, pitch, yaw, rollspeed, pitchspeed, yawspeed, lat, lon, alt, vx, vy, vz, xacc, yacc, zacc))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def hil_controls_encode(self, time_us, roll_ailerons, pitch_elevator, yaw_rudder, throttle, mode, nav_mode):
|
|
|
|
'''
|
|
|
|
Hardware in the loop control outputs
|
|
|
|
|
|
|
|
time_us : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
roll_ailerons : Control output -3 .. 1 (float)
|
|
|
|
pitch_elevator : Control output -1 .. 1 (float)
|
|
|
|
yaw_rudder : Control output -1 .. 1 (float)
|
|
|
|
throttle : Throttle 0 .. 1 (float)
|
|
|
|
mode : System mode (MAV_MODE) (uint8_t)
|
|
|
|
nav_mode : Navigation mode (MAV_NAV_MODE) (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_hil_controls_message(time_us, roll_ailerons, pitch_elevator, yaw_rudder, throttle, mode, nav_mode)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def hil_controls_send(self, time_us, roll_ailerons, pitch_elevator, yaw_rudder, throttle, mode, nav_mode):
|
|
|
|
'''
|
|
|
|
Hardware in the loop control outputs
|
|
|
|
|
|
|
|
time_us : Timestamp (microseconds since UNIX epoch or microseconds since system boot) (uint64_t)
|
|
|
|
roll_ailerons : Control output -3 .. 1 (float)
|
|
|
|
pitch_elevator : Control output -1 .. 1 (float)
|
|
|
|
yaw_rudder : Control output -1 .. 1 (float)
|
|
|
|
throttle : Throttle 0 .. 1 (float)
|
|
|
|
mode : System mode (MAV_MODE) (uint8_t)
|
|
|
|
nav_mode : Navigation mode (MAV_NAV_MODE) (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.hil_controls_encode(time_us, roll_ailerons, pitch_elevator, yaw_rudder, throttle, mode, nav_mode))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def manual_control_encode(self, target, roll, pitch, yaw, thrust, roll_manual, pitch_manual, yaw_manual, thrust_manual):
|
|
|
|
'''
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
|
|
|
|
target : The system to be controlled (uint8_t)
|
|
|
|
roll : roll (float)
|
|
|
|
pitch : pitch (float)
|
|
|
|
yaw : yaw (float)
|
|
|
|
thrust : thrust (float)
|
|
|
|
roll_manual : roll control enabled auto:0, manual:1 (uint8_t)
|
|
|
|
pitch_manual : pitch auto:0, manual:1 (uint8_t)
|
|
|
|
yaw_manual : yaw auto:0, manual:1 (uint8_t)
|
|
|
|
thrust_manual : thrust auto:0, manual:1 (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_manual_control_message(target, roll, pitch, yaw, thrust, roll_manual, pitch_manual, yaw_manual, thrust_manual)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def manual_control_send(self, target, roll, pitch, yaw, thrust, roll_manual, pitch_manual, yaw_manual, thrust_manual):
|
|
|
|
'''
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
|
|
|
|
target : The system to be controlled (uint8_t)
|
|
|
|
roll : roll (float)
|
|
|
|
pitch : pitch (float)
|
|
|
|
yaw : yaw (float)
|
|
|
|
thrust : thrust (float)
|
|
|
|
roll_manual : roll control enabled auto:0, manual:1 (uint8_t)
|
|
|
|
pitch_manual : pitch auto:0, manual:1 (uint8_t)
|
|
|
|
yaw_manual : yaw auto:0, manual:1 (uint8_t)
|
|
|
|
thrust_manual : thrust auto:0, manual:1 (uint8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.manual_control_encode(target, roll, pitch, yaw, thrust, roll_manual, pitch_manual, yaw_manual, thrust_manual))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def rc_channels_override_encode(self, target_system, target_component, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw):
|
|
|
|
'''
|
|
|
|
The RAW values of the RC channels sent to the MAV to override info
|
|
|
|
received from the RC radio. A value of -1 means no
|
|
|
|
change to that channel. A value of 0 means control of
|
|
|
|
that channel should be released back to the RC radio.
|
|
|
|
The standard PPM modulation is as follows: 1000
|
|
|
|
microseconds: 0%, 2000 microseconds: 100%. Individual
|
|
|
|
receivers/transmitters might violate this
|
|
|
|
specification.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
chan1_raw : RC channel 1 value, in microseconds (uint16_t)
|
|
|
|
chan2_raw : RC channel 2 value, in microseconds (uint16_t)
|
|
|
|
chan3_raw : RC channel 3 value, in microseconds (uint16_t)
|
|
|
|
chan4_raw : RC channel 4 value, in microseconds (uint16_t)
|
|
|
|
chan5_raw : RC channel 5 value, in microseconds (uint16_t)
|
|
|
|
chan6_raw : RC channel 6 value, in microseconds (uint16_t)
|
|
|
|
chan7_raw : RC channel 7 value, in microseconds (uint16_t)
|
|
|
|
chan8_raw : RC channel 8 value, in microseconds (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_rc_channels_override_message(target_system, target_component, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def rc_channels_override_send(self, target_system, target_component, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw):
|
|
|
|
'''
|
|
|
|
The RAW values of the RC channels sent to the MAV to override info
|
|
|
|
received from the RC radio. A value of -1 means no
|
|
|
|
change to that channel. A value of 0 means control of
|
|
|
|
that channel should be released back to the RC radio.
|
|
|
|
The standard PPM modulation is as follows: 1000
|
|
|
|
microseconds: 0%, 2000 microseconds: 100%. Individual
|
|
|
|
receivers/transmitters might violate this
|
|
|
|
specification.
|
|
|
|
|
|
|
|
target_system : System ID (uint8_t)
|
|
|
|
target_component : Component ID (uint8_t)
|
|
|
|
chan1_raw : RC channel 1 value, in microseconds (uint16_t)
|
|
|
|
chan2_raw : RC channel 2 value, in microseconds (uint16_t)
|
|
|
|
chan3_raw : RC channel 3 value, in microseconds (uint16_t)
|
|
|
|
chan4_raw : RC channel 4 value, in microseconds (uint16_t)
|
|
|
|
chan5_raw : RC channel 5 value, in microseconds (uint16_t)
|
|
|
|
chan6_raw : RC channel 6 value, in microseconds (uint16_t)
|
|
|
|
chan7_raw : RC channel 7 value, in microseconds (uint16_t)
|
|
|
|
chan8_raw : RC channel 8 value, in microseconds (uint16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.rc_channels_override_encode(target_system, target_component, chan1_raw, chan2_raw, chan3_raw, chan4_raw, chan5_raw, chan6_raw, chan7_raw, chan8_raw))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def global_position_int_encode(self, lat, lon, alt, vx, vy, vz):
|
|
|
|
'''
|
|
|
|
The filtered global position (e.g. fused GPS and accelerometers). The
|
|
|
|
position is in GPS-frame (right-handed, Z-up)
|
|
|
|
|
|
|
|
lat : Latitude, expressed as * 1E7 (int32_t)
|
|
|
|
lon : Longitude, expressed as * 1E7 (int32_t)
|
|
|
|
alt : Altitude in meters, expressed as * 1000 (millimeters) (int32_t)
|
|
|
|
vx : Ground X Speed (Latitude), expressed as m/s * 100 (int16_t)
|
|
|
|
vy : Ground Y Speed (Longitude), expressed as m/s * 100 (int16_t)
|
|
|
|
vz : Ground Z Speed (Altitude), expressed as m/s * 100 (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_global_position_int_message(lat, lon, alt, vx, vy, vz)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def global_position_int_send(self, lat, lon, alt, vx, vy, vz):
|
|
|
|
'''
|
|
|
|
The filtered global position (e.g. fused GPS and accelerometers). The
|
|
|
|
position is in GPS-frame (right-handed, Z-up)
|
|
|
|
|
|
|
|
lat : Latitude, expressed as * 1E7 (int32_t)
|
|
|
|
lon : Longitude, expressed as * 1E7 (int32_t)
|
|
|
|
alt : Altitude in meters, expressed as * 1000 (millimeters) (int32_t)
|
|
|
|
vx : Ground X Speed (Latitude), expressed as m/s * 100 (int16_t)
|
|
|
|
vy : Ground Y Speed (Longitude), expressed as m/s * 100 (int16_t)
|
|
|
|
vz : Ground Z Speed (Altitude), expressed as m/s * 100 (int16_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.global_position_int_encode(lat, lon, alt, vx, vy, vz))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def vfr_hud_encode(self, airspeed, groundspeed, heading, throttle, alt, climb):
|
|
|
|
'''
|
|
|
|
Metrics typically displayed on a HUD for fixed wing aircraft
|
|
|
|
|
|
|
|
airspeed : Current airspeed in m/s (float)
|
|
|
|
groundspeed : Current ground speed in m/s (float)
|
|
|
|
heading : Current heading in degrees, in compass units (0..360, 0=north) (int16_t)
|
|
|
|
throttle : Current throttle setting in integer percent, 0 to 100 (uint16_t)
|
|
|
|
alt : Current altitude (MSL), in meters (float)
|
|
|
|
climb : Current climb rate in meters/second (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_vfr_hud_message(airspeed, groundspeed, heading, throttle, alt, climb)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def vfr_hud_send(self, airspeed, groundspeed, heading, throttle, alt, climb):
|
|
|
|
'''
|
|
|
|
Metrics typically displayed on a HUD for fixed wing aircraft
|
|
|
|
|
|
|
|
airspeed : Current airspeed in m/s (float)
|
|
|
|
groundspeed : Current ground speed in m/s (float)
|
|
|
|
heading : Current heading in degrees, in compass units (0..360, 0=north) (int16_t)
|
|
|
|
throttle : Current throttle setting in integer percent, 0 to 100 (uint16_t)
|
|
|
|
alt : Current altitude (MSL), in meters (float)
|
|
|
|
climb : Current climb rate in meters/second (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.vfr_hud_encode(airspeed, groundspeed, heading, throttle, alt, climb))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def command_encode(self, target_system, target_component, command, confirmation, param1, param2, param3, param4):
|
|
|
|
'''
|
|
|
|
Send a command with up to four parameters to the MAV
|
|
|
|
|
|
|
|
target_system : System which should execute the command (uint8_t)
|
|
|
|
target_component : Component which should execute the command, 0 for all components (uint8_t)
|
|
|
|
command : Command ID, as defined by MAV_CMD enum. (uint8_t)
|
|
|
|
confirmation : 0: First transmission of this command. 1-255: Confirmation transmissions (e.g. for kill command) (uint8_t)
|
|
|
|
param1 : Parameter 1, as defined by MAV_CMD enum. (float)
|
|
|
|
param2 : Parameter 2, as defined by MAV_CMD enum. (float)
|
|
|
|
param3 : Parameter 3, as defined by MAV_CMD enum. (float)
|
|
|
|
param4 : Parameter 4, as defined by MAV_CMD enum. (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_command_message(target_system, target_component, command, confirmation, param1, param2, param3, param4)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def command_send(self, target_system, target_component, command, confirmation, param1, param2, param3, param4):
|
|
|
|
'''
|
|
|
|
Send a command with up to four parameters to the MAV
|
|
|
|
|
|
|
|
target_system : System which should execute the command (uint8_t)
|
|
|
|
target_component : Component which should execute the command, 0 for all components (uint8_t)
|
|
|
|
command : Command ID, as defined by MAV_CMD enum. (uint8_t)
|
|
|
|
confirmation : 0: First transmission of this command. 1-255: Confirmation transmissions (e.g. for kill command) (uint8_t)
|
|
|
|
param1 : Parameter 1, as defined by MAV_CMD enum. (float)
|
|
|
|
param2 : Parameter 2, as defined by MAV_CMD enum. (float)
|
|
|
|
param3 : Parameter 3, as defined by MAV_CMD enum. (float)
|
|
|
|
param4 : Parameter 4, as defined by MAV_CMD enum. (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.command_encode(target_system, target_component, command, confirmation, param1, param2, param3, param4))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def command_ack_encode(self, command, result):
|
|
|
|
'''
|
|
|
|
Report status of a command. Includes feedback wether the command was
|
|
|
|
executed
|
|
|
|
|
|
|
|
command : Current airspeed in m/s (float)
|
|
|
|
result : 1: Action ACCEPTED and EXECUTED, 1: Action TEMPORARY REJECTED/DENIED, 2: Action PERMANENTLY DENIED, 3: Action UNKNOWN/UNSUPPORTED, 4: Requesting CONFIRMATION (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_command_ack_message(command, result)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def command_ack_send(self, command, result):
|
|
|
|
'''
|
|
|
|
Report status of a command. Includes feedback wether the command was
|
|
|
|
executed
|
|
|
|
|
|
|
|
command : Current airspeed in m/s (float)
|
|
|
|
result : 1: Action ACCEPTED and EXECUTED, 1: Action TEMPORARY REJECTED/DENIED, 2: Action PERMANENTLY DENIED, 3: Action UNKNOWN/UNSUPPORTED, 4: Requesting CONFIRMATION (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.command_ack_encode(command, result))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def optical_flow_encode(self, time, sensor_id, flow_x, flow_y, quality, ground_distance):
|
|
|
|
'''
|
|
|
|
Optical flow from a flow sensor (e.g. optical mouse sensor)
|
|
|
|
|
|
|
|
time : Timestamp (UNIX) (uint64_t)
|
|
|
|
sensor_id : Sensor ID (uint8_t)
|
|
|
|
flow_x : Flow in pixels in x-sensor direction (int16_t)
|
|
|
|
flow_y : Flow in pixels in y-sensor direction (int16_t)
|
|
|
|
quality : Optical flow quality / confidence. 0: bad, 255: maximum quality (uint8_t)
|
|
|
|
ground_distance : Ground distance in meters (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_optical_flow_message(time, sensor_id, flow_x, flow_y, quality, ground_distance)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def optical_flow_send(self, time, sensor_id, flow_x, flow_y, quality, ground_distance):
|
|
|
|
'''
|
|
|
|
Optical flow from a flow sensor (e.g. optical mouse sensor)
|
|
|
|
|
|
|
|
time : Timestamp (UNIX) (uint64_t)
|
|
|
|
sensor_id : Sensor ID (uint8_t)
|
|
|
|
flow_x : Flow in pixels in x-sensor direction (int16_t)
|
|
|
|
flow_y : Flow in pixels in y-sensor direction (int16_t)
|
|
|
|
quality : Optical flow quality / confidence. 0: bad, 255: maximum quality (uint8_t)
|
|
|
|
ground_distance : Ground distance in meters (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.optical_flow_encode(time, sensor_id, flow_x, flow_y, quality, ground_distance))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def object_detection_event_encode(self, time, object_id, type, name, quality, bearing, distance):
|
|
|
|
'''
|
|
|
|
Object has been detected
|
|
|
|
|
|
|
|
time : Timestamp in milliseconds since system boot (uint32_t)
|
|
|
|
object_id : Object ID (uint16_t)
|
|
|
|
type : Object type: 0: image, 1: letter, 2: ground vehicle, 3: air vehicle, 4: surface vehicle, 5: sub-surface vehicle, 6: human, 7: animal (uint8_t)
|
|
|
|
name : Name of the object as defined by the detector (char)
|
|
|
|
quality : Detection quality / confidence. 0: bad, 255: maximum confidence (uint8_t)
|
|
|
|
bearing : Angle of the object with respect to the body frame in NED coordinates in radians. 0: front (float)
|
|
|
|
distance : Ground distance in meters (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_object_detection_event_message(time, object_id, type, name, quality, bearing, distance)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def object_detection_event_send(self, time, object_id, type, name, quality, bearing, distance):
|
|
|
|
'''
|
|
|
|
Object has been detected
|
|
|
|
|
|
|
|
time : Timestamp in milliseconds since system boot (uint32_t)
|
|
|
|
object_id : Object ID (uint16_t)
|
|
|
|
type : Object type: 0: image, 1: letter, 2: ground vehicle, 3: air vehicle, 4: surface vehicle, 5: sub-surface vehicle, 6: human, 7: animal (uint8_t)
|
|
|
|
name : Name of the object as defined by the detector (char)
|
|
|
|
quality : Detection quality / confidence. 0: bad, 255: maximum confidence (uint8_t)
|
|
|
|
bearing : Angle of the object with respect to the body frame in NED coordinates in radians. 0: front (float)
|
|
|
|
distance : Ground distance in meters (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.object_detection_event_encode(time, object_id, type, name, quality, bearing, distance))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def debug_vect_encode(self, name, usec, x, y, z):
|
|
|
|
'''
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
|
|
|
|
name : Name (char)
|
|
|
|
usec : Timestamp (uint64_t)
|
|
|
|
x : x (float)
|
|
|
|
y : y (float)
|
|
|
|
z : z (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_debug_vect_message(name, usec, x, y, z)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def debug_vect_send(self, name, usec, x, y, z):
|
|
|
|
'''
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
|
|
|
|
name : Name (char)
|
|
|
|
usec : Timestamp (uint64_t)
|
|
|
|
x : x (float)
|
|
|
|
y : y (float)
|
|
|
|
z : z (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.debug_vect_encode(name, usec, x, y, z))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def named_value_float_encode(self, name, value):
|
|
|
|
'''
|
|
|
|
Send a key-value pair as float. The use of this message is discouraged
|
|
|
|
for normal packets, but a quite efficient way for
|
|
|
|
testing new messages and getting experimental debug
|
|
|
|
output.
|
|
|
|
|
|
|
|
name : Name of the debug variable (char)
|
|
|
|
value : Floating point value (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_named_value_float_message(name, value)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def named_value_float_send(self, name, value):
|
|
|
|
'''
|
|
|
|
Send a key-value pair as float. The use of this message is discouraged
|
|
|
|
for normal packets, but a quite efficient way for
|
|
|
|
testing new messages and getting experimental debug
|
|
|
|
output.
|
|
|
|
|
|
|
|
name : Name of the debug variable (char)
|
|
|
|
value : Floating point value (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.named_value_float_encode(name, value))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def named_value_int_encode(self, name, value):
|
|
|
|
'''
|
|
|
|
Send a key-value pair as integer. The use of this message is
|
|
|
|
discouraged for normal packets, but a quite efficient
|
|
|
|
way for testing new messages and getting experimental
|
|
|
|
debug output.
|
|
|
|
|
|
|
|
name : Name of the debug variable (char)
|
|
|
|
value : Signed integer value (int32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_named_value_int_message(name, value)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def named_value_int_send(self, name, value):
|
|
|
|
'''
|
|
|
|
Send a key-value pair as integer. The use of this message is
|
|
|
|
discouraged for normal packets, but a quite efficient
|
|
|
|
way for testing new messages and getting experimental
|
|
|
|
debug output.
|
|
|
|
|
|
|
|
name : Name of the debug variable (char)
|
|
|
|
value : Signed integer value (int32_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.named_value_int_encode(name, value))
|
2011-12-28 17:29:37 -04:00
|
|
|
|
2011-12-02 00:20:02 -04:00
|
|
|
def statustext_encode(self, severity, text):
|
|
|
|
'''
|
|
|
|
Status text message. These messages are printed in yellow in the COMM
|
|
|
|
console of QGroundControl. WARNING: They consume quite
|
|
|
|
some bandwidth, so use only for important status and
|
|
|
|
error messages. If implemented wisely, these messages
|
|
|
|
are buffered on the MCU and sent only at a limited
|
|
|
|
rate (e.g. 10 Hz).
|
|
|
|
|
|
|
|
severity : Severity of status, 0 = info message, 255 = critical fault (uint8_t)
|
|
|
|
text : Status text message, without null termination character (int8_t)
|
|
|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_statustext_message(severity, text)
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msg.pack(self)
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return msg
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2011-12-28 17:29:37 -04:00
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2011-12-02 00:20:02 -04:00
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def statustext_send(self, severity, text):
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|
'''
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|
Status text message. These messages are printed in yellow in the COMM
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|
console of QGroundControl. WARNING: They consume quite
|
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|
|
some bandwidth, so use only for important status and
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|
error messages. If implemented wisely, these messages
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|
are buffered on the MCU and sent only at a limited
|
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|
|
rate (e.g. 10 Hz).
|
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|
|
|
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|
|
severity : Severity of status, 0 = info message, 255 = critical fault (uint8_t)
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|
text : Status text message, without null termination character (int8_t)
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'''
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|
|
return self.send(self.statustext_encode(severity, text))
|
2011-12-28 17:29:37 -04:00
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|
2011-12-02 00:20:02 -04:00
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|
def debug_encode(self, ind, value):
|
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|
|
'''
|
|
|
|
Send a debug value. The index is used to discriminate between values.
|
|
|
|
These values show up in the plot of QGroundControl as
|
|
|
|
DEBUG N.
|
|
|
|
|
|
|
|
ind : index of debug variable (uint8_t)
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|
|
value : DEBUG value (float)
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|
|
|
|
|
|
'''
|
|
|
|
msg = MAVLink_debug_message(ind, value)
|
|
|
|
msg.pack(self)
|
|
|
|
return msg
|
2011-12-28 17:29:37 -04:00
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|
2011-12-02 00:20:02 -04:00
|
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|
def debug_send(self, ind, value):
|
|
|
|
'''
|
|
|
|
Send a debug value. The index is used to discriminate between values.
|
|
|
|
These values show up in the plot of QGroundControl as
|
|
|
|
DEBUG N.
|
|
|
|
|
|
|
|
ind : index of debug variable (uint8_t)
|
|
|
|
value : DEBUG value (float)
|
|
|
|
|
|
|
|
'''
|
|
|
|
return self.send(self.debug_encode(ind, value))
|
2011-12-28 17:29:37 -04:00
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|