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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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/*
This program is free software: you can redistribute it and/or modify
it under the terms of the GNU General Public License as published by
the Free Software Foundation, either version 3 of the License, or
(at your option) any later version.
This program is distributed in the hope that it will be useful,
but WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
GNU General Public License for more details.
You should have received a copy of the GNU General Public License
along with this program. If not, see <http://www.gnu.org/licenses/>.
*/
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/*
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* ArduCopter parameter definitions
*
*/
#define GSCALAR(v, name, def) { g.v.vtype, name, Parameters::k_param_ ## v, &g.v, {def_value : def} }
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#define ASCALAR(v, name, def) { aparm.v.vtype, name, Parameters::k_param_ ## v, &aparm.v, {def_value : def} }
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#define GGROUP(v, name, class) { AP_PARAM_GROUP, name, Parameters::k_param_ ## v, &g.v, {group_info : class::var_info} }
#define GOBJECT(v, name, class) { AP_PARAM_GROUP, name, Parameters::k_param_ ## v, &v, {group_info : class::var_info} }
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#define GOBJECTN(v, pname, name, class) { AP_PARAM_GROUP, name, Parameters::k_param_ ## pname, &v, {group_info : class::var_info} }
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const AP_Param::Info var_info[] PROGMEM = {
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// @Param: SYSID_SW_MREV
// @DisplayName: Eeprom format version number
// @Description: This value is incremented when changes are made to the eeprom format
// @User: Advanced
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GSCALAR(format_version, "SYSID_SW_MREV", 0),
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// @Param: SYSID_SW_TYPE
// @DisplayName: Software Type
// @Description: This is used by the ground station to recognise the software type (eg ArduPlane vs ArduCopter)
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// @Values: 0:ArduPlane,4:AntennaTracker,10:Copter,20:Rover
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// @User: Advanced
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GSCALAR(software_type, "SYSID_SW_TYPE", Parameters::k_software_type),
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// @Param: SYSID_THISMAV
// @DisplayName: Mavlink version
// @Description: Allows reconising the mavlink version
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// @Range: 1 255
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// @User: Advanced
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GSCALAR(sysid_this_mav, "SYSID_THISMAV", MAV_SYSTEM_ID),
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// @Param: SYSID_MYGCS
// @DisplayName: My ground station number
// @Description: Allows restricting radio overrides to only come from my ground station
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// @Values: 255:Mission Planner and DroidPlanner, 252: AP Planner 2
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// @User: Advanced
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GSCALAR(sysid_my_gcs, "SYSID_MYGCS", 255),
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#if CLI_ENABLED == ENABLED
// @Param: CLI_ENABLED
// @DisplayName: CLI Enable
// @Description: This enables/disables the checking for three carriage returns on telemetry links on startup to enter the diagnostics command line interface
// @Values: 0:Disabled,1:Enabled
// @User: Advanced
GSCALAR(cli_enabled, "CLI_ENABLED", 0),
#endif
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// @Param: PILOT_THR_FILT
// @DisplayName: Throttle filter cutoff
// @Description: Throttle filter cutoff (Hz) - active whenever altitude control is inactive - 0 to disable
// @User: Advanced
// @Units: Hz
// @Range: 0 10
// @Increment: .5
GSCALAR(throttle_filt, "PILOT_THR_FILT", 0),
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// @Param: PILOT_TKOFF_ALT
// @DisplayName: Pilot takeoff altitude
// @Description: Altitude that altitude control modes will climb to when a takeoff is triggered with the throttle stick.
// @User: Standard
// @Units: Centimeters
// @Range: 0.0 1000.0
// @Increment: 10
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GSCALAR(pilot_takeoff_alt, "PILOT_TKOFF_ALT", PILOT_TKOFF_ALT_DEFAULT),
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// @Param: PILOT_TKOFF_DZ
// @DisplayName: Takeoff trigger deadzone
// @Description: Offset from mid stick at which takeoff is triggered
// @User: Standard
// @Range 0.0 500.0
// @Increment: 10
GSCALAR(takeoff_trigger_dz, "PILOT_TKOFF_DZ", THR_DZ_DEFAULT),
// @Param: PILOT_THR_BHV
// @DisplayName: Throttle stick behavior
// @Description: Bits for: Feedback starts from mid stick
// @User: Standard
// @Values: 0:None,1:FeedbackFromMid
GSCALAR(throttle_behavior, "PILOT_THR_BHV", 0),
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// @Group: SERIAL
// @Path: ../libraries/AP_SerialManager/AP_SerialManager.cpp
GOBJECT(serial_manager, "SERIAL", AP_SerialManager),
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// @Param: TELEM_DELAY
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// @DisplayName: Telemetry startup delay
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// @Description: The amount of time (in seconds) to delay radio telemetry to prevent an Xbee bricking on power up
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// @User: Advanced
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// @Units: seconds
// @Range: 0 10
// @Increment: 1
GSCALAR(telem_delay, "TELEM_DELAY", 0),
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// @Param: RTL_ALT
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// @DisplayName: RTL Altitude
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// @Description: The minimum altitude the model will move to before Returning to Launch. Set to zero to return at current altitude.
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// @Units: Centimeters
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// @Range: 0 8000
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// @Increment: 1
// @User: Standard
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GSCALAR(rtl_altitude, "RTL_ALT", RTL_ALT),
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// @Param: RNGFND_GAIN
// @DisplayName: Rangefinder gain
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// @Description: Used to adjust the speed with which the target altitude is changed when objects are sensed below the copter
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// @Range: 0.01 2.0
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// @Increment: 0.01
// @User: Standard
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GSCALAR(sonar_gain, "RNGFND_GAIN", SONAR_GAIN_DEFAULT),
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// @Param: FS_BATT_ENABLE
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// @DisplayName: Battery Failsafe Enable
// @Description: Controls whether failsafe will be invoked when battery voltage or current runs low
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// @Values: 0:Disabled,1:Land,2:RTL
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// @User: Standard
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GSCALAR(failsafe_battery_enabled, "FS_BATT_ENABLE", FS_BATT_DISABLED),
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// @Param: FS_BATT_VOLTAGE
// @DisplayName: Failsafe battery voltage
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// @Description: Battery voltage to trigger failsafe. Set to 0 to disable battery voltage failsafe. If the battery voltage drops below this voltage then the copter will RTL
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// @Units: Volts
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// @Increment: 0.1
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// @User: Standard
GSCALAR(fs_batt_voltage, "FS_BATT_VOLTAGE", FS_BATT_VOLTAGE_DEFAULT),
// @Param: FS_BATT_MAH
// @DisplayName: Failsafe battery milliAmpHours
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// @Description: Battery capacity remaining to trigger failsafe. Set to 0 to disable battery remaining failsafe. If the battery remaining drops below this level then the copter will RTL
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// @Units: mAh
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// @Increment: 50
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// @User: Standard
GSCALAR(fs_batt_mah, "FS_BATT_MAH", FS_BATT_MAH_DEFAULT),
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// @Param: FS_GCS_ENABLE
// @DisplayName: Ground Station Failsafe Enable
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// @Description: Controls whether failsafe will be invoked (and what action to take) when connection with Ground station is lost for at least 5 seconds. NB. The GCS Failsafe is only active when RC_OVERRIDE is being used to control the vehicle.
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// @Values: 0:Disabled,1:Enabled always RTL,2:Enabled Continue with Mission in Auto Mode
// @User: Standard
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GSCALAR(failsafe_gcs, "FS_GCS_ENABLE", FS_GCS_ENABLED_ALWAYS_RTL),
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// @Param: GPS_HDOP_GOOD
// @DisplayName: GPS Hdop Good
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// @Description: GPS Hdop value at or below this value represent a good position. Used for pre-arm checks
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// @Range: 100 900
// @User: Advanced
GSCALAR(gps_hdop_good, "GPS_HDOP_GOOD", GPS_HDOP_GOOD_DEFAULT),
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// @Param: MAG_ENABLE
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// @DisplayName: Compass enable/disable
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// @Description: Setting this to Enabled(1) will enable the compass. Setting this to Disabled(0) will disable the compass
// @Values: 0:Disabled,1:Enabled
// @User: Standard
GSCALAR(compass_enabled, "MAG_ENABLE", MAGNETOMETER),
// @Param: SUPER_SIMPLE
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// @DisplayName: Super Simple Mode
// @Description: Bitmask to enable Super Simple mode for some flight modes. Setting this to Disabled(0) will disable Super Simple Mode
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// @Values: 0:Disabled,1:Mode1,2:Mode2,3:Mode1+2,4:Mode3,5:Mode1+3,6:Mode2+3,7:Mode1+2+3,8:Mode4,9:Mode1+4,10:Mode2+4,11:Mode1+2+4,12:Mode3+4,13:Mode1+3+4,14:Mode2+3+4,15:Mode1+2+3+4,16:Mode5,17:Mode1+5,18:Mode2+5,19:Mode1+2+5,20:Mode3+5,21:Mode1+3+5,22:Mode2+3+5,23:Mode1+2+3+5,24:Mode4+5,25:Mode1+4+5,26:Mode2+4+5,27:Mode1+2+4+5,28:Mode3+4+5,29:Mode1+3+4+5,30:Mode2+3+4+5,31:Mode1+2+3+4+5,32:Mode6,33:Mode1+6,34:Mode2+6,35:Mode1+2+6,36:Mode3+6,37:Mode1+3+6,38:Mode2+3+6,39:Mode1+2+3+6,40:Mode4+6,41:Mode1+4+6,42:Mode2+4+6,43:Mode1+2+4+6,44:Mode3+4+6,45:Mode1+3+4+6,46:Mode2+3+4+6,47:Mode1+2+3+4+6,48:Mode5+6,49:Mode1+5+6,50:Mode2+5+6,51:Mode1+2+5+6,52:Mode3+5+6,53:Mode1+3+5+6,54:Mode2+3+5+6,55:Mode1+2+3+5+6,56:Mode4+5+6,57:Mode1+4+5+6,58:Mode2+4+5+6,59:Mode1+2+4+5+6,60:Mode3+4+5+6,61:Mode1+3+4+5+6,62:Mode2+3+4+5+6,63:Mode1+2+3+4+5+6
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// @User: Standard
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GSCALAR(super_simple, "SUPER_SIMPLE", 0),
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// @Param: RTL_ALT_FINAL
// @DisplayName: RTL Final Altitude
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// @Description: This is the altitude the vehicle will move to as the final stage of Returning to Launch or after completing a mission. Set to zero to land.
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// @Units: Centimeters
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// @Range: -1 1000
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// @Increment: 1
// @User: Standard
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GSCALAR(rtl_alt_final, "RTL_ALT_FINAL", RTL_ALT_FINAL),
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// @Param: RSSI_PIN
// @DisplayName: Receiver RSSI sensing pin
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// @Description: This selects an analog pin for the receiver RSSI voltage. It assumes the voltage is RSSI_RANGE for max rssi, 0V for minimum
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// @Values: -1:Disabled, 0:APM2 A0, 1:APM2 A1, 2:APM2 A2, 13:APM2 A13, 103:Pixhawk SBUS
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// @User: Standard
GSCALAR(rssi_pin, "RSSI_PIN", -1),
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// @Param: RSSI_RANGE
// @DisplayName: Receiver RSSI voltage range
// @Description: Receiver RSSI voltage range
// @Units: Volt
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// @Values: 3.3:3.3V, 5:5V
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// @User: Standard
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GSCALAR(rssi_range, "RSSI_RANGE", 5.0f),
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// @Param: WP_YAW_BEHAVIOR
// @DisplayName: Yaw behaviour during missions
// @Description: Determines how the autopilot controls the yaw during missions and RTL
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// @Values: 0:Never change yaw, 1:Face next waypoint, 2:Face next waypoint except RTL, 3:Face along GPS course
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// @User: Standard
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GSCALAR(wp_yaw_behavior, "WP_YAW_BEHAVIOR", WP_YAW_BEHAVIOR_DEFAULT),
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// @Param: RTL_LOIT_TIME
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// @DisplayName: RTL loiter time
// @Description: Time (in milliseconds) to loiter above home before begining final descent
// @Units: ms
// @Range: 0 60000
// @Increment: 1000
// @User: Standard
GSCALAR(rtl_loiter_time, "RTL_LOIT_TIME", RTL_LOITER_TIME),
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// @Param: LAND_SPEED
// @DisplayName: Land speed
// @Description: The descent speed for the final stage of landing in cm/s
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// @Units: cm/s
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// @Range: 30 200
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// @Increment: 10
// @User: Standard
GSCALAR(land_speed, "LAND_SPEED", LAND_SPEED),
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// @Param: PILOT_VELZ_MAX
// @DisplayName: Pilot maximum vertical speed
// @Description: The maximum vertical velocity the pilot may request in cm/s
// @Units: Centimeters/Second
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// @Range: 50 500
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// @Increment: 10
// @User: Standard
GSCALAR(pilot_velocity_z_max, "PILOT_VELZ_MAX", PILOT_VELZ_MAX),
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// @Param: PILOT_ACCEL_Z
// @DisplayName: Pilot vertical acceleration
// @Description: The vertical acceleration used when pilot is controlling the altitude
// @Units: cm/s/s
// @Range: 50 500
// @Increment: 10
// @User: Standard
GSCALAR(pilot_accel_z, "PILOT_ACCEL_Z", PILOT_ACCEL_Z_DEFAULT),
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// @Param: THR_MIN
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// @DisplayName: Throttle Minimum
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// @Description: The minimum throttle that will be sent to the motors to keep them spinning
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// @Units: Percent*10
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// @Range: 0 300
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// @Increment: 1
// @User: Standard
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GSCALAR(throttle_min, "THR_MIN", THR_MIN_DEFAULT),
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// @Param: FS_THR_ENABLE
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// @DisplayName: Throttle Failsafe Enable
// @Description: The throttle failsafe allows you to configure a software failsafe activated by a setting on the throttle input channel
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// @Values: 0:Disabled,1:Enabled always RTL,2:Enabled Continue with Mission in Auto Mode,3:Enabled always LAND
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// @User: Standard
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GSCALAR(failsafe_throttle, "FS_THR_ENABLE", FS_THR_DISABLED),
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// @Param: FS_THR_VALUE
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// @DisplayName: Throttle Failsafe Value
// @Description: The PWM level on channel 3 below which throttle sailsafe triggers
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// @Range: 925 1100
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// @Units: pwm
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// @Increment: 1
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// @User: Standard
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GSCALAR(failsafe_throttle_value, "FS_THR_VALUE", FS_THR_VALUE_DEFAULT),
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// @Param: THR_MID
// @DisplayName: Throttle Mid Position
// @Description: The throttle output (0 ~ 1000) when throttle stick is in mid position. Used to scale the manual throttle so that the mid throttle stick position is close to the throttle required to hover
// @User: Standard
// @Range: 300 700
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// @Units: Percent*10
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// @Increment: 1
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GSCALAR(throttle_mid, "THR_MID", THR_MID_DEFAULT),
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// @Param: THR_DZ
// @DisplayName: Throttle deadzone
// @Description: The deadzone above and below mid throttle. Used in AltHold, Loiter, PosHold flight modes
// @User: Standard
// @Range: 0 300
// @Units: pwm
// @Increment: 1
GSCALAR(throttle_deadzone, "THR_DZ", THR_DZ_DEFAULT),
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// @Param: FLTMODE1
// @DisplayName: Flight Mode 1
// @Description: Flight mode when Channel 5 pwm is <= 1230
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// @Values: 0:Stabilize,1:Acro,2:AltHold,3:Auto,4:Guided,5:Loiter,6:RTL,7:Circle,9:Land,11:Drift,13:Sport,16:PosHold
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// @User: Standard
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GSCALAR(flight_mode1, "FLTMODE1", FLIGHT_MODE_1),
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// @Param: FLTMODE2
// @DisplayName: Flight Mode 2
// @Description: Flight mode when Channel 5 pwm is >1230, <= 1360
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// @Values: 0:Stabilize,1:Acro,2:AltHold,3:Auto,4:Guided,5:Loiter,6:RTL,7:Circle,9:Land,11:Drift,13:Sport,16:PosHold
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// @User: Standard
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GSCALAR(flight_mode2, "FLTMODE2", FLIGHT_MODE_2),
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// @Param: FLTMODE3
// @DisplayName: Flight Mode 3
// @Description: Flight mode when Channel 5 pwm is >1360, <= 1490
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// @Values: 0:Stabilize,1:Acro,2:AltHold,3:Auto,4:Guided,5:Loiter,6:RTL,7:Circle,9:Land,11:Drift,13:Sport,16:PosHold
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// @User: Standard
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GSCALAR(flight_mode3, "FLTMODE3", FLIGHT_MODE_3),
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// @Param: FLTMODE4
// @DisplayName: Flight Mode 4
// @Description: Flight mode when Channel 5 pwm is >1490, <= 1620
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// @Values: 0:Stabilize,1:Acro,2:AltHold,3:Auto,4:Guided,5:Loiter,6:RTL,7:Circle,9:Land,11:Drift,13:Sport,16:PosHold
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// @User: Standard
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GSCALAR(flight_mode4, "FLTMODE4", FLIGHT_MODE_4),
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// @Param: FLTMODE5
// @DisplayName: Flight Mode 5
// @Description: Flight mode when Channel 5 pwm is >1620, <= 1749
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// @Values: 0:Stabilize,1:Acro,2:AltHold,3:Auto,4:Guided,5:Loiter,6:RTL,7:Circle,9:Land,11:Drift,13:Sport,16:PosHold
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// @User: Standard
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GSCALAR(flight_mode5, "FLTMODE5", FLIGHT_MODE_5),
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// @Param: FLTMODE6
// @DisplayName: Flight Mode 6
// @Description: Flight mode when Channel 5 pwm is >=1750
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// @Values: 0:Stabilize,1:Acro,2:AltHold,3:Auto,4:Guided,5:Loiter,6:RTL,7:Circle,9:Land,11:Drift,13:Sport,16:PosHold
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// @User: Standard
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GSCALAR(flight_mode6, "FLTMODE6", FLIGHT_MODE_6),
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// @Param: SIMPLE
// @DisplayName: Simple mode bitmask
// @Description: Bitmask which holds which flight modes use simple heading mode (eg bit 0 = 1 means Flight Mode 0 uses simple mode)
// @User: Advanced
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GSCALAR(simple_modes, "SIMPLE", 0),
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// @Param: LOG_BITMASK
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// @DisplayName: Log bitmask
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// @Description: 4 byte bitmap of log types to enable
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// @Values: 830:Default,894:Default+RCIN,958:Default+IMU,1854:Default+Motors,-6146:NearlyAll-AC315,45054:NearlyAll,131070:All+DisarmedLogging,131071:All+FastATT,262142:All+MotBatt,393214:All+FastIMU,0:Disabled
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// @User: Standard
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GSCALAR(log_bitmask, "LOG_BITMASK", DEFAULT_LOG_BITMASK),
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// @Param: ESC
// @DisplayName: ESC Calibration
// @Description: Controls whether ArduCopter will enter ESC calibration on the next restart. Do not adjust this parameter manually.
// @User: Advanced
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// @Values: 0:Normal Start-up, 1:Start-up in ESC Calibration mode if throttle high, 2:Start-up in ESC Calibration mode regardless of throttle
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GSCALAR(esc_calibrate, "ESC", 0),
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// @Param: TUNE
// @DisplayName: Channel 6 Tuning
// @Description: Controls which parameters (normally PID gains) are being tuned with transmitter's channel 6 knob
// @User: Standard
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// @Values: 0:None,1:Stab Roll/Pitch kP,4:Rate Roll/Pitch kP,5:Rate Roll/Pitch kI,21:Rate Roll/Pitch kD,3:Stab Yaw kP,6:Rate Yaw kP,26:Rate Yaw kD,14:Altitude Hold kP,7:Throttle Rate kP,34:Throttle Accel kP,35:Throttle Accel kI,36:Throttle Accel kD,42:Loiter Speed,12:Loiter Pos kP,22:Velocity XY kP,28:Velocity XY kI,10:WP Speed,25:Acro RollPitch kP,40:Acro Yaw kP,13:Heli Ext Gyro,17:OF Loiter kP,18:OF Loiter kI,19:OF Loiter kD,38:Declination,39:Circle Rate,41:RangeFinder Gain,46:Rate Pitch kP,47:Rate Pitch kI,48:Rate Pitch kD,49:Rate Roll kP,50:Rate Roll kI,51:Rate Roll kD,52:Rate Pitch FF,53:Rate Roll FF,54:Rate Yaw FF
2012-08-21 23:19:50 -03:00
GSCALAR(radio_tuning, "TUNE", 0),
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// @Param: TUNE_LOW
// @DisplayName: Tuning minimum
// @Description: The minimum value that will be applied to the parameter currently being tuned with the transmitter's channel 6 knob
// @User: Standard
// @Range: 0 32767
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GSCALAR(radio_tuning_low, "TUNE_LOW", 0),
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// @Param: TUNE_HIGH
// @DisplayName: Tuning maximum
// @Description: The maximum value that will be applied to the parameter currently being tuned with the transmitter's channel 6 knob
// @User: Standard
// @Range: 0 32767
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GSCALAR(radio_tuning_high, "TUNE_HIGH", 1000),
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// @Param: FRAME
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// @DisplayName: Frame Orientation (+, X or V)
// @Description: Controls motor mixing for multicopters. Not used for Tri or Traditional Helicopters.
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// @Values: 0:Plus, 1:X, 2:V, 3:H, 4:V-Tail, 5:A-Tail, 10:Y6B (New)
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// @User: Standard
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GSCALAR(frame_orientation, "FRAME", AP_MOTORS_X_FRAME),
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// @Param: CH7_OPT
// @DisplayName: Channel 7 option
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// @Description: Select which function if performed when CH7 is above 1800 pwm
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// @Values: 0:Do Nothing, 2:Flip, 3:Simple Mode, 4:RTL, 5:Save Trim, 7:Save WP, 9:Camera Trigger, 10:RangeFinder, 11:Fence, 12:ResetToArmedYaw, 13:Super Simple Mode, 14:Acro Trainer, 16:Auto, 17:AutoTune, 18:Land, 19:EPM, 21:Parachute Enable, 22:Parachute Release, 23:Parachute 3pos, 24:Auto Mission Reset, 25:AttCon Feed Forward, 26:AttCon Accel Limits, 27:Retract Mount, 28:Relay On/Off, 29:Landing Gear, 30:Lost Copter Sound, 31:Motor Emergency Stop, 32:Motor Interlock
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// @User: Standard
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GSCALAR(ch7_option, "CH7_OPT", AUXSW_DO_NOTHING),
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// @Param: CH8_OPT
// @DisplayName: Channel 8 option
// @Description: Select which function if performed when CH8 is above 1800 pwm
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// @Values: 0:Do Nothing, 2:Flip, 3:Simple Mode, 4:RTL, 5:Save Trim, 7:Save WP, 9:Camera Trigger, 10:RangeFinder, 11:Fence, 12:ResetToArmedYaw, 13:Super Simple Mode, 14:Acro Trainer, 16:Auto, 17:AutoTune, 18:Land, 19:EPM, 21:Parachute Enable, 22:Parachute Release, 23:Parachute 3pos, 24:Auto Mission Reset, 25:AttCon Feed Forward, 26:AttCon Accel Limits, 27:Retract Mount, 28:Relay On/Off, 29:Landing Gear, 30:Lost Copter Sound, 31:Motor Emergency Stop, 32:Motor Interlock
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// @User: Standard
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GSCALAR(ch8_option, "CH8_OPT", AUXSW_DO_NOTHING),
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// @Param: CH9_OPT
// @DisplayName: Channel 9 option
// @Description: Select which function if performed when CH9 is above 1800 pwm
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// @Values: 0:Do Nothing, 2:Flip, 3:Simple Mode, 4:RTL, 5:Save Trim, 7:Save WP, 9:Camera Trigger, 10:RangeFinder, 11:Fence, 12:ResetToArmedYaw, 13:Super Simple Mode, 14:Acro Trainer, 16:Auto, 17:AutoTune, 18:Land, 19:EPM, 21:Parachute Enable, 22:Parachute Release, 23:Parachute 3pos, 24:Auto Mission Reset, 25:AttCon Feed Forward, 26:AttCon Accel Limits, 27:Retract Mount, 28:Relay On/Off, 29:Landing Gear, 30:Lost Copter Sound, 31:Motor Emergency Stop, 32:Motor Interlock
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// @User: Standard
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GSCALAR(ch9_option, "CH9_OPT", AUXSW_DO_NOTHING),
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// @Param: CH10_OPT
// @DisplayName: Channel 10 option
// @Description: Select which function if performed when CH10 is above 1800 pwm
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// @Values: 0:Do Nothing, 2:Flip, 3:Simple Mode, 4:RTL, 5:Save Trim, 7:Save WP, 9:Camera Trigger, 10:RangeFinder, 11:Fence, 12:ResetToArmedYaw, 13:Super Simple Mode, 14:Acro Trainer, 16:Auto, 17:AutoTune, 18:Land, 19:EPM, 21:Parachute Enable, 22:Parachute Release, 23:Parachute 3pos, 24:Auto Mission Reset, 25:AttCon Feed Forward, 26:AttCon Accel Limits, 27:Retract Mount, 28:Relay On/Off, 29:Landing Gear, 30:Lost Copter Sound, 31:Motor Emergency Stop, 32:Motor Interlock
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// @User: Standard
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GSCALAR(ch10_option, "CH10_OPT", AUXSW_DO_NOTHING),
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// @Param: CH11_OPT
// @DisplayName: Channel 11 option
// @Description: Select which function if performed when CH11 is above 1800 pwm
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// @Values: 0:Do Nothing, 2:Flip, 3:Simple Mode, 4:RTL, 5:Save Trim, 7:Save WP, 9:Camera Trigger, 10:RangeFinder, 11:Fence, 12:ResetToArmedYaw, 13:Super Simple Mode, 14:Acro Trainer, 16:Auto, 17:AutoTune, 18:Land, 19:EPM, 21:Parachute Enable, 22:Parachute Release, 23:Parachute 3pos, 24:Auto Mission Reset, 25:AttCon Feed Forward, 26:AttCon Accel Limits, 27:Retract Mount, 28:Relay On/Off, 29:Landing Gear, 30:Lost Copter Sound, 31:Motor Emergency Stop, 32:Motor Interlock
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// @User: Standard
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GSCALAR(ch11_option, "CH11_OPT", AUXSW_DO_NOTHING),
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// @Param: CH12_OPT
// @DisplayName: Channel 12 option
// @Description: Select which function if performed when CH12 is above 1800 pwm
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// @Values: 0:Do Nothing, 2:Flip, 3:Simple Mode, 4:RTL, 5:Save Trim, 7:Save WP, 9:Camera Trigger, 10:RangeFinder, 11:Fence, 12:ResetToArmedYaw, 13:Super Simple Mode, 14:Acro Trainer, 16:Auto, 17:AutoTune, 18:Land, 19:EPM, 21:Parachute Enable, 22:Parachute Release, 23:Parachute 3pos, 24:Auto Mission Reset, 25:AttCon Feed Forward, 26:AttCon Accel Limits, 27:Retract Mount, 28:Relay On/Off, 29:Landing Gear, 30:Lost Copter Sound, 31:Motor Emergency Stop, 32:Motor Interlock
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// @User: Standard
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GSCALAR(ch12_option, "CH12_OPT", AUXSW_DO_NOTHING),
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// @Param: ARMING_CHECK
// @DisplayName: Arming check
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// @Description: Allows enabling or disabling of pre-arming checks of receiver, accelerometer, barometer, compass and GPS
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// @Values: 0:Disabled, 1:Enabled, -3:Skip Baro, -5:Skip Compass, -9:Skip GPS, -17:Skip INS, -33:Skip Params/Sonar, -65:Skip RC, 127:Skip Voltage
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// @User: Standard
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GSCALAR(arming_check, "ARMING_CHECK", ARMING_CHECK_ALL),
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// @Param: ANGLE_MAX
// @DisplayName: Angle Max
// @Description: Maximum lean angle in all flight modes
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// @Units: Centi-degrees
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// @Range 1000 8000
// @User: Advanced
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ASCALAR(angle_max, "ANGLE_MAX", DEFAULT_ANGLE_MAX),
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// @Param: RC_FEEL_RP
// @DisplayName: RC Feel Roll/Pitch
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// @Description: RC feel for roll/pitch which controls vehicle response to user input with 0 being extremely soft and 100 being crisp
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// @Range: 0 100
// @Increment: 1
// @User: Standard
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// @Values: 0:Very Soft, 25:Soft, 50:Medium, 75:Crisp, 100:Very Crisp
GSCALAR(rc_feel_rp, "RC_FEEL_RP", RC_FEEL_RP_VERY_CRISP),
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#if POSHOLD_ENABLED == ENABLED
// @Param: PHLD_BRAKE_RATE
// @DisplayName: PosHold braking rate
// @Description: PosHold flight mode's rotation rate during braking in deg/sec
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// @Units: deg/sec
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// @Range: 4 12
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// @User: Advanced
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GSCALAR(poshold_brake_rate, "PHLD_BRAKE_RATE", POSHOLD_BRAKE_RATE_DEFAULT),
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2014-07-11 02:08:09 -03:00
// @Param: PHLD_BRAKE_ANGLE
// @DisplayName: PosHold braking angle max
// @Description: PosHold flight mode's max lean angle during braking in centi-degrees
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// @Units: Centi-degrees
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// @Range: 2000 4500
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// @User: Advanced
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GSCALAR(poshold_brake_angle_max, "PHLD_BRAKE_ANGLE", POSHOLD_BRAKE_ANGLE_DEFAULT),
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#endif
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// @Param: LAND_REPOSITION
// @DisplayName: Land repositioning
// @Description: Enables user input during LAND mode, the landing phase of RTL, and auto mode landings.
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// @Values: 0:No repositioning, 1:Repositioning
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// @User: Advanced
GSCALAR(land_repositioning, "LAND_REPOSITION", LAND_REPOSITION_DEFAULT),
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// @Param: EKF_CHECK_THRESH
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// @DisplayName: EKF check compass and velocity variance threshold
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// @Description: Allows setting the maximum acceptable compass and velocity variance (0 to disable check)
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// @Values: 0:Disabled, 0.6:Strict, 0.8:Default, 1.0:Relaxed
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// @User: Advanced
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GSCALAR(ekfcheck_thresh, "EKF_CHECK_THRESH", EKFCHECK_THRESHOLD_DEFAULT),
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#if FRAME_CONFIG == HELI_FRAME
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// @Group: HS1_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
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GGROUP(heli_servo_1, "HS1_", RC_Channel),
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// @Group: HS2_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
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GGROUP(heli_servo_2, "HS2_", RC_Channel),
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// @Group: HS3_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
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GGROUP(heli_servo_3, "HS3_", RC_Channel),
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// @Group: HS4_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
2012-08-21 23:19:50 -03:00
GGROUP(heli_servo_4, "HS4_", RC_Channel),
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// @Param: H_STAB_COL_MIN
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// @DisplayName: Heli Stabilize Throttle Collective Minimum
// @Description: Helicopter's minimum collective position while pilot directly controls collective in stabilize mode
// @Range: 0 500
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// @Units: Percent*10
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// @Increment: 1
// @User: Standard
2014-01-09 18:02:08 -04:00
GSCALAR(heli_stab_col_min, "H_STAB_COL_MIN", HELI_STAB_COLLECTIVE_MIN_DEFAULT),
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// @Param: H_STAB_COL_MAX
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// @DisplayName: Stabilize Throttle Maximum
// @Description: Helicopter's maximum collective position while pilot directly controls collective in stabilize mode
// @Range: 500 1000
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// @Units: Percent*10
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// @Increment: 1
// @User: Standard
2014-01-09 18:02:08 -04:00
GSCALAR(heli_stab_col_max, "H_STAB_COL_MAX", HELI_STAB_COLLECTIVE_MAX_DEFAULT),
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#endif
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// RC channel
//-----------
// @Group: RC1_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(rc_1, "RC1_", RC_Channel),
// @Group: RC2_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(rc_2, "RC2_", RC_Channel),
// @Group: RC3_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(rc_3, "RC3_", RC_Channel),
// @Group: RC4_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(rc_4, "RC4_", RC_Channel),
// @Group: RC5_
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// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
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GGROUP(rc_5, "RC5_", RC_Channel_aux),
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// @Group: RC6_
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// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
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GGROUP(rc_6, "RC6_", RC_Channel_aux),
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// @Group: RC7_
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// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
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GGROUP(rc_7, "RC7_", RC_Channel_aux),
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// @Group: RC8_
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// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
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GGROUP(rc_8, "RC8_", RC_Channel_aux),
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#if CONFIG_HAL_BOARD == HAL_BOARD_PX4 || CONFIG_HAL_BOARD == HAL_BOARD_VRBRAIN
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// @Group: RC9_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_9, "RC9_", RC_Channel_aux),
#endif
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// @Group: RC10_
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// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
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GGROUP(rc_10, "RC10_", RC_Channel_aux),
// @Group: RC11_
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// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
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GGROUP(rc_11, "RC11_", RC_Channel_aux),
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#if CONFIG_HAL_BOARD == HAL_BOARD_PX4 || CONFIG_HAL_BOARD == HAL_BOARD_VRBRAIN
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// @Group: RC12_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_12, "RC12_", RC_Channel_aux),
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// @Group: RC13_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_13, "RC13_", RC_Channel_aux),
// @Group: RC14_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_14, "RC14_", RC_Channel_aux),
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#endif
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// @Param: RC_SPEED
// @DisplayName: ESC Update Speed
// @Description: This is the speed in Hertz that your ESCs will receive updates
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// @Units: Hz
// @Range: 50 490
// @Increment: 1
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// @User: Advanced
GSCALAR(rc_speed, "RC_SPEED", RC_FAST_SPEED),
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// @Param: ACRO_RP_P
// @DisplayName: Acro Roll and Pitch P gain
// @Description: Converts pilot roll and pitch into a desired rate of rotation in ACRO and SPORT mode. Higher values mean faster rate of rotation.
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// @Range: 1 10
// @User: Standard
2013-08-04 08:22:12 -03:00
GSCALAR(acro_rp_p, "ACRO_RP_P", ACRO_RP_P),
// @Param: ACRO_YAW_P
// @DisplayName: Acro Yaw P gain
// @Description: Converts pilot yaw input into a desired rate of rotation in ACRO, Stabilize and SPORT modes. Higher values mean faster rate of rotation.
// @Range: 1 10
// @User: Standard
GSCALAR(acro_yaw_p, "ACRO_YAW_P", ACRO_YAW_P),
2012-12-10 08:45:57 -04:00
2012-10-23 09:30:50 -03:00
// @Param: ACRO_BAL_ROLL
// @DisplayName: Acro Balance Roll
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// @Description: rate at which roll angle returns to level in acro mode. A higher value causes the vehicle to return to level faster.
2013-08-04 06:14:07 -03:00
// @Range: 0 3
// @Increment: 0.1
2012-10-23 09:30:50 -03:00
// @User: Advanced
GSCALAR(acro_balance_roll, "ACRO_BAL_ROLL", ACRO_BALANCE_ROLL),
// @Param: ACRO_BAL_PITCH
// @DisplayName: Acro Balance Pitch
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// @Description: rate at which pitch angle returns to level in acro mode. A higher value causes the vehicle to return to level faster.
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// @Range: 0 3
// @Increment: 0.1
2012-10-23 09:30:50 -03:00
// @User: Advanced
GSCALAR(acro_balance_pitch, "ACRO_BAL_PITCH", ACRO_BALANCE_PITCH),
2012-12-10 09:27:46 -04:00
// @Param: ACRO_TRAINER
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// @DisplayName: Acro Trainer
// @Description: Type of trainer used in acro mode
// @Values: 0:Disabled,1:Leveling,2:Leveling and Limited
2012-12-10 09:27:46 -04:00
// @User: Advanced
2013-08-04 06:14:07 -03:00
GSCALAR(acro_trainer, "ACRO_TRAINER", ACRO_TRAINER_LIMITED),
2012-12-10 09:27:46 -04:00
2014-08-12 23:25:59 -03:00
// @Param: ACRO_EXPO
// @DisplayName: Acro Expo
// @Description: Acro roll/pitch Expo to allow faster rotation when stick at edges
2014-08-19 00:51:27 -03:00
// @Values: 0:Disabled,0.1:Very Low,0.2:Low,0.3:Medium,0.4:High,0.5:Very High
2014-08-12 23:25:59 -03:00
// @User: Advanced
GSCALAR(acro_expo, "ACRO_EXPO", ACRO_EXPO_DEFAULT),
2012-08-21 23:19:50 -03:00
// PID controller
//---------------
2014-05-02 18:44:09 -03:00
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// @Param: RATE_RLL_P
// @DisplayName: Roll axis rate controller P gain
// @Description: Roll axis rate controller P gain. Converts the difference between desired roll rate and actual roll rate into a motor speed output
2015-04-09 08:09:03 -03:00
// @Range: 0.08 0.30
2013-06-16 09:53:50 -03:00
// @Increment: 0.005
2013-01-02 04:05:57 -04:00
// @User: Standard
// @Param: RATE_RLL_I
// @DisplayName: Roll axis rate controller I gain
// @Description: Roll axis rate controller I gain. Corrects long-term difference in desired roll rate vs actual roll rate
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// @Range: 0.01 0.5
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// @Increment: 0.01
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// @User: Standard
// @Param: RATE_RLL_IMAX
// @DisplayName: Roll axis rate controller I gain maximum
// @Description: Roll axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output
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// @Range: 0 4500
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// @Increment: 10
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// @Units: Percent*10
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// @User: Standard
// @Param: RATE_RLL_D
// @DisplayName: Roll axis rate controller D gain
// @Description: Roll axis rate controller D gain. Compensates for short-term change in desired roll rate vs actual roll rate
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// @Range: 0.001 0.02
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// @Increment: 0.001
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// @User: Standard
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#if FRAME_CONFIG == HELI_FRAME
GGROUP(pid_rate_roll, "RATE_RLL_", AC_HELI_PID),
#else
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GGROUP(pid_rate_roll, "RATE_RLL_", AC_PID),
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#endif
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// @Param: RATE_PIT_P
// @DisplayName: Pitch axis rate controller P gain
// @Description: Pitch axis rate controller P gain. Converts the difference between desired pitch rate and actual pitch rate into a motor speed output
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// @Range: 0.08 0.30
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// @Increment: 0.005
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// @User: Standard
// @Param: RATE_PIT_I
// @DisplayName: Pitch axis rate controller I gain
// @Description: Pitch axis rate controller I gain. Corrects long-term difference in desired pitch rate vs actual pitch rate
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// @Range: 0.01 0.5
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// @Increment: 0.01
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// @User: Standard
// @Param: RATE_PIT_IMAX
// @DisplayName: Pitch axis rate controller I gain maximum
// @Description: Pitch axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output
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// @Range: 0 4500
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// @Increment: 10
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// @Units: Percent*10
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// @User: Standard
// @Param: RATE_PIT_D
// @DisplayName: Pitch axis rate controller D gain
// @Description: Pitch axis rate controller D gain. Compensates for short-term change in desired pitch rate vs actual pitch rate
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// @Range: 0.001 0.02
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// @Increment: 0.001
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// @User: Standard
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#if FRAME_CONFIG == HELI_FRAME
GGROUP(pid_rate_pitch, "RATE_PIT_", AC_HELI_PID),
#else
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GGROUP(pid_rate_pitch, "RATE_PIT_", AC_PID),
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#endif
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// @Param: RATE_YAW_P
// @DisplayName: Yaw axis rate controller P gain
// @Description: Yaw axis rate controller P gain. Converts the difference between desired yaw rate and actual yaw rate into a motor speed output
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// @Range: 0.150 0.50
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// @Increment: 0.005
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// @User: Standard
// @Param: RATE_YAW_I
// @DisplayName: Yaw axis rate controller I gain
// @Description: Yaw axis rate controller I gain. Corrects long-term difference in desired yaw rate vs actual yaw rate
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// @Range: 0.010 0.05
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// @Increment: 0.01
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// @User: Standard
// @Param: RATE_YAW_IMAX
// @DisplayName: Yaw axis rate controller I gain maximum
// @Description: Yaw axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output
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// @Range: 0 4500
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// @Increment: 10
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// @Units: Percent*10
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// @User: Standard
// @Param: RATE_YAW_D
// @DisplayName: Yaw axis rate controller D gain
// @Description: Yaw axis rate controller D gain. Compensates for short-term change in desired yaw rate vs actual yaw rate
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// @Range: 0.000 0.02
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// @Increment: 0.001
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// @User: Standard
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#if FRAME_CONFIG == HELI_FRAME
GGROUP(pid_rate_yaw, "RATE_YAW_", AC_HELI_PID),
#else
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GGROUP(pid_rate_yaw, "RATE_YAW_", AC_PID),
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#endif
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// @Param: VEL_XY_P
// @DisplayName: Velocity (horizontal) P gain
// @Description: Velocity (horizontal) P gain. Converts the difference between desired velocity to a target acceleration
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// @Range: 0.1 6.0
// @Increment: 0.1
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// @User: Advanced
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// @Param: VEL_XY_I
// @DisplayName: Velocity (horizontal) I gain
// @Description: Velocity (horizontal) I gain. Corrects long-term difference in desired velocity to a target acceleration
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// @Range: 0.02 1.00
// @Increment: 0.01
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// @User: Advanced
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// @Param: VEL_XY_IMAX
// @DisplayName: Velocity (horizontal) integrator maximum
// @Description: Velocity (horizontal) integrator maximum. Constrains the target acceleration that the I gain will output
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// @Range: 0 4500
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// @Increment: 10
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// @Units: cm/s/s
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// @User: Advanced
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GGROUP(pi_vel_xy, "VEL_XY_", AC_PI_2D),
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// @Param: VEL_Z_P
// @DisplayName: Velocity (vertical) P gain
// @Description: Velocity (vertical) P gain. Converts the difference between desired vertical speed and actual speed into a desired acceleration that is passed to the throttle acceleration controller
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// @Range: 1.000 8.000
// @User: Standard
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GGROUP(p_vel_z, "VEL_Z_", AC_P),
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// @Param: ACCEL_Z_P
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// @DisplayName: Throttle acceleration controller P gain
// @Description: Throttle acceleration controller P gain. Converts the difference between desired vertical acceleration and actual acceleration into a motor output
// @Range: 0.500 1.500
// @User: Standard
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// @Param: ACCEL_Z_I
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// @DisplayName: Throttle acceleration controller I gain
// @Description: Throttle acceleration controller I gain. Corrects long-term difference in desired vertical acceleration and actual acceleration
// @Range: 0.000 3.000
// @User: Standard
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// @Param: ACCEL_Z_IMAX
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// @DisplayName: Throttle acceleration controller I gain maximum
// @Description: Throttle acceleration controller I gain maximum. Constrains the maximum pwm that the I term will generate
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// @Range: 0 1000
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// @Units: Percent*10
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// @User: Standard
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// @Param: ACCEL_Z_D
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// @DisplayName: Throttle acceleration controller D gain
// @Description: Throttle acceleration controller D gain. Compensates for short-term change in desired vertical acceleration vs actual acceleration
// @Range: 0.000 0.400
// @User: Standard
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GGROUP(pid_accel_z, "ACCEL_Z_", AC_PID),
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// P controllers
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//--------------
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// @Param: STB_RLL_P
// @DisplayName: Roll axis stabilize controller P gain
// @Description: Roll axis stabilize (i.e. angle) controller P gain. Converts the error between the desired roll angle and actual angle to a desired roll rate
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// @Range: 3.000 12.000
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// @User: Standard
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GGROUP(p_stabilize_roll, "STB_RLL_", AC_P),
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// @Param: STB_PIT_P
// @DisplayName: Pitch axis stabilize controller P gain
// @Description: Pitch axis stabilize (i.e. angle) controller P gain. Converts the error between the desired pitch angle and actual angle to a desired pitch rate
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// @Range: 3.000 12.000
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// @User: Standard
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GGROUP(p_stabilize_pitch, "STB_PIT_", AC_P),
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// @Param: STB_YAW_P
// @DisplayName: Yaw axis stabilize controller P gain
// @Description: Yaw axis stabilize (i.e. angle) controller P gain. Converts the error between the desired yaw angle and actual angle to a desired yaw rate
// @Range: 3.000 6.000
// @User: Standard
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GGROUP(p_stabilize_yaw, "STB_YAW_", AC_P),
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// @Param: POS_Z_P
// @DisplayName: Position (vertical) controller P gain
// @Description: Position (vertical) controller P gain. Converts the difference between the desired altitude and actual altitude into a climb or descent rate which is passed to the throttle rate controller
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// @Range: 1.000 3.000
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// @User: Standard
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GGROUP(p_alt_hold, "POS_Z_", AC_P),
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// @Param: POS_XY_P
// @DisplayName: Position (horizonal) controller P gain
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// @Description: Loiter position controller P gain. Converts the distance (in the latitude direction) to the target location into a desired speed which is then passed to the loiter latitude rate controller
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// @Range: 0.500 2.000
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// @User: Standard
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GGROUP(p_pos_xy, "POS_XY_", AC_P),
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// variables not in the g class which contain EEPROM saved variables
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#if CAMERA == ENABLED
// @Group: CAM_
// @Path: ../libraries/AP_Camera/AP_Camera.cpp
GOBJECT(camera, "CAM_", AP_Camera),
#endif
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// @Group: RELAY_
// @Path: ../libraries/AP_Relay/AP_Relay.cpp
GOBJECT(relay, "RELAY_", AP_Relay),
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#if EPM_ENABLED == ENABLED
// @Group: EPM_
// @Path: ../libraries/AP_EPM/AP_EPM.cpp
GOBJECT(epm, "EPM_", AP_EPM),
#endif
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#if PARACHUTE == ENABLED
// @Group: CHUTE_
// @Path: ../libraries/AP_Parachute/AP_Parachute.cpp
GOBJECT(parachute, "CHUTE_", AP_Parachute),
#endif
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// @Group: LGR_
// @Path: ../libraries/AP_LandingGear/AP_LandingGear.cpp
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GOBJECT(landinggear, "LGR_", AP_LandingGear),
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// @Group: COMPASS_
// @Path: ../libraries/AP_Compass/Compass.cpp
GOBJECT(compass, "COMPASS_", Compass),
// @Group: INS_
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// @Path: ../libraries/AP_InertialSensor/AP_InertialSensor.cpp
GOBJECT(ins, "INS_", AP_InertialSensor),
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// @Group: WPNAV_
// @Path: ../libraries/AC_WPNav/AC_WPNav.cpp
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GOBJECT(wp_nav, "WPNAV_", AC_WPNav),
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// @Group: CIRCLE_
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// @Path: ../libraries/AC_WPNav/AC_Circle.cpp
GOBJECT(circle_nav, "CIRCLE_", AC_Circle),
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#if FRAME_CONFIG == HELI_FRAME
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// @Group: ATC_
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// @Path: ../libraries/AC_AttitudeControl/AC_AttitudeControl_Heli.cpp
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GOBJECT(attitude_control, "ATC_", AC_AttitudeControl_Heli),
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#else
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// @Group: ATC_
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// @Path: ../libraries/AC_AttitudeControl/AC_AttitudeControl.cpp
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GOBJECT(attitude_control, "ATC_", AC_AttitudeControl),
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#endif
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// @Group: POSCON_
// @Path: ../libraries/AC_AttitudeControl/AC_PosControl.cpp
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GOBJECT(pos_control, "PSC", AC_PosControl),
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// @Group: SR0_
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// @Path: GCS_Mavlink.pde
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GOBJECTN(gcs[0], gcs0, "SR0_", GCS_MAVLINK),
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// @Group: SR1_
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// @Path: GCS_Mavlink.pde
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GOBJECTN(gcs[1], gcs1, "SR1_", GCS_MAVLINK),
#if MAVLINK_COMM_NUM_BUFFERS > 2
// @Group: SR2_
// @Path: GCS_Mavlink.pde
GOBJECTN(gcs[2], gcs2, "SR2_", GCS_MAVLINK),
#endif
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// @Group: AHRS_
// @Path: ../libraries/AP_AHRS/AP_AHRS.cpp
GOBJECT(ahrs, "AHRS_", AP_AHRS),
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#if MOUNT == ENABLED
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// @Group: MNT
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// @Path: ../libraries/AP_Mount/AP_Mount.cpp
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GOBJECT(camera_mount, "MNT", AP_Mount),
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#endif
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// @Group: BATT_
// @Path: ../libraries/AP_BattMonitor/AP_BattMonitor.cpp
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GOBJECT(battery, "BATT", AP_BattMonitor),
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// @Group: BRD_
// @Path: ../libraries/AP_BoardConfig/AP_BoardConfig.cpp
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GOBJECT(BoardConfig, "BRD_", AP_BoardConfig),
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#if SPRAYER == ENABLED
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// @Group: SPRAY_
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// @Path: ../libraries/AC_Sprayer/AC_Sprayer.cpp
GOBJECT(sprayer, "SPRAY_", AC_Sprayer),
#endif
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#if CONFIG_HAL_BOARD == HAL_BOARD_SITL
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GOBJECT(sitl, "SIM_", SITL),
#endif
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// @Group: GND_
// @Path: ../libraries/AP_Baro/AP_Baro.cpp
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GOBJECT(barometer, "GND_", AP_Baro),
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// GPS driver
// @Group: GPS_
// @Path: ../libraries/AP_GPS/AP_GPS.cpp
GOBJECT(gps, "GPS_", AP_GPS),
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// @Group: SCHED_
// @Path: ../libraries/AP_Scheduler/AP_Scheduler.cpp
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GOBJECT(scheduler, "SCHED_", AP_Scheduler),
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#if AC_FENCE == ENABLED
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// @Group: FENCE_
// @Path: ../libraries/AC_Fence/AC_Fence.cpp
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GOBJECT(fence, "FENCE_", AC_Fence),
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#endif
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#if AC_RALLY == ENABLED
// @Group: RALLY_
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// @Path: ../libraries/AP_Rally/AP_Rally.cpp
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GOBJECT(rally, "RALLY_", AP_Rally),
#endif
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#if FRAME_CONFIG == HELI_FRAME
// @Group: H_
// @Path: ../libraries/AP_Motors/AP_MotorsHeli.cpp
GOBJECT(motors, "H_", AP_MotorsHeli),
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#elif FRAME_CONFIG == SINGLE_FRAME
// @Group: SS1_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(single_servo_1, "SS1_", RC_Channel),
// @Group: SS2_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(single_servo_2, "SS2_", RC_Channel),
// @Group: SS3_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(single_servo_3, "SS3_", RC_Channel),
// @Group: SS4_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(single_servo_4, "SS4_", RC_Channel),
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// @Group: MOT_
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// @Path: ../libraries/AP_Motors/AP_MotorsSingle.cpp
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GOBJECT(motors, "MOT_", AP_MotorsSingle),
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#elif FRAME_CONFIG == COAX_FRAME
// @Group: SS1_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(single_servo_1, "SS1_", RC_Channel),
// @Group: SS2_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp
GGROUP(single_servo_2, "SS2_", RC_Channel),
// @Group: MOT_
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// @Path: ../libraries/AP_Motors/AP_MotorsCoax.cpp
GOBJECT(motors, "MOT_", AP_MotorsCoax),
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#else
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// @Group: MOT_
// @Path: ../libraries/AP_Motors/AP_Motors_Class.cpp
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GOBJECT(motors, "MOT_", AP_Motors),
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#endif
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// @Group: RCMAP_
// @Path: ../libraries/AP_RCMapper/AP_RCMapper.cpp
GOBJECT(rcmap, "RCMAP_", RCMapper),
2014-02-21 00:51:22 -04:00
#if AP_AHRS_NAVEKF_AVAILABLE
// @Group: EKF_
// @Path: ../libraries/AP_NavEKF/AP_NavEKF.cpp
GOBJECTN(ahrs.get_NavEKF(), NavEKF, "EKF_", NavEKF),
#endif
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// @Group: MIS_
// @Path: ../libraries/AP_Mission/AP_Mission.cpp
GOBJECT(mission, "MIS_", AP_Mission),
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#if CONFIG_SONAR == ENABLED
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// @Group: RNGFND
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// @Path: ../libraries/AP_RangeFinder/RangeFinder.cpp
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GOBJECT(sonar, "RNGFND", RangeFinder),
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#endif
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#if AP_TERRAIN_AVAILABLE
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// @Group: TERRAIN_
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// @Path: ../libraries/AP_Terrain/AP_Terrain.cpp
GOBJECT(terrain, "TERRAIN_", AP_Terrain),
#endif
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#if OPTFLOW == ENABLED
// @Group: FLOW
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// @Path: ../libraries/AP_OpticalFlow/OpticalFlow.cpp
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GOBJECT(optflow, "FLOW", OpticalFlow),
#endif
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// @Param: AUTOTUNE_AXIS_BITMASK
// @DisplayName: Autotune axis bitmask
// @Description: 1-byte bitmap of axes to autotune
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// @Values: 7:All,1:Roll Only,2:Pitch Only,4:Yaw Only,3:Roll and Pitch,5:Roll and Yaw,6:Pitch and Yaw
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// @User: Standard
GSCALAR(autotune_axis_bitmask, "AUTOTUNE_AXES", 7), // AUTOTUNE_AXIS_BITMASK_DEFAULT
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// @Param: AUTOTUNE_AGGRESSIVENESS
// @DisplayName: autotune_aggressiveness
// @Description: autotune_aggressiveness. Defines the bounce back used to detect size of the D term.
// @Range: 0.05 0.10
// @User: Standard
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GSCALAR(autotune_aggressiveness, "AUTOTUNE_AGGR", 0.1f),
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AP_VAREND
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};
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/*
This is a conversion table from old parameter values to new
parameter names. The startup code looks for saved values of the old
parameters and will copy them across to the new parameters if the
new parameter does not yet have a saved value. It then saves the new
value.
Note that this works even if the old parameter has been removed. It
relies on the old k_param index not being removed
The second column below is the index in the var_info[] table for the
old object. This should be zero for top level parameters.
*/
const AP_Param::ConversionInfo conversion_table[] PROGMEM = {
{ Parameters::k_param_battery_monitoring, 0, AP_PARAM_INT8, "BATT_MONITOR" },
{ Parameters::k_param_battery_volt_pin, 0, AP_PARAM_INT8, "BATT_VOLT_PIN" },
{ Parameters::k_param_battery_curr_pin, 0, AP_PARAM_INT8, "BATT_CURR_PIN" },
{ Parameters::k_param_volt_div_ratio, 0, AP_PARAM_FLOAT, "BATT_VOLT_MULT" },
{ Parameters::k_param_curr_amp_per_volt, 0, AP_PARAM_FLOAT, "BATT_AMP_PERVOLT" },
{ Parameters::k_param_pack_capacity, 0, AP_PARAM_INT32, "BATT_CAPACITY" },
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{ Parameters::k_param_log_bitmask_old, 0, AP_PARAM_INT16, "LOG_BITMASK" },
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{ Parameters::k_param_serial0_baud, 0, AP_PARAM_INT16, "SERIAL0_BAUD" },
{ Parameters::k_param_serial1_baud, 0, AP_PARAM_INT16, "SERIAL1_BAUD" },
{ Parameters::k_param_serial2_baud, 0, AP_PARAM_INT16, "SERIAL2_BAUD" },
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};
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static void load_parameters(void)
{
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if (!AP_Param::check_var_info()) {
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cliSerial->printf_P(PSTR("Bad var table\n"));
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hal.scheduler->panic(PSTR("Bad var table"));
}
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// disable centrifugal force correction, it will be enabled as part of the arming process
ahrs.set_correct_centrifugal(false);
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hal.util->set_soft_armed(false);
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if (!g.format_version.load() ||
g.format_version != Parameters::k_format_version) {
// erase all parameters
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cliSerial->printf_P(PSTR("Firmware change: erasing EEPROM...\n"));
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AP_Param::erase_all();
// save the current format version
g.format_version.set_and_save(Parameters::k_format_version);
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cliSerial->println_P(PSTR("done."));
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} else {
uint32_t before = micros();
// Load all auto-loaded EEPROM variables
AP_Param::load_all();
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AP_Param::convert_old_parameters(&conversion_table[0], sizeof(conversion_table)/sizeof(conversion_table[0]));
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cliSerial->printf_P(PSTR("load_all took %luus\n"), micros() - before);
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}
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}
