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ardupilot/ArduSub/Parameters.cpp

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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
#include "Sub.h"
/*
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/>.
*/
/*
* ArduCopter parameter definitions
*
*/
#define GSCALAR(v, name, def) { sub.g.v.vtype, name, Parameters::k_param_ ## v, &sub.g.v, {def_value : def} }
#define ASCALAR(v, name, def) { sub.aparm.v.vtype, name, Parameters::k_param_ ## v, (const void *)&sub.aparm.v, {def_value : def} }
#define GGROUP(v, name, class) { AP_PARAM_GROUP, name, Parameters::k_param_ ## v, &sub.g.v, {group_info : class::var_info} }
#define GOBJECT(v, name, class) { AP_PARAM_GROUP, name, Parameters::k_param_ ## v, (const void *)&sub.v, {group_info : class::var_info} }
#define GOBJECTN(v, pname, name, class) { AP_PARAM_GROUP, name, Parameters::k_param_ ## pname, (const void *)&sub.v, {group_info : class::var_info} }
const AP_Param::Info Sub::var_info[] = {
// @Param: SURFACE_DEPTH
// @DisplayName: Depth reading at surface
// @Description: The depth the external pressure sensor will read when the vehicle is considered at the surface (in centimeters)
// @Range: -100 0
// @User: Standard
GSCALAR(surface_depth, "SURFACE_DEPTH", SURFACE_DEPTH_DEFAULT),
// @Param: SYSID_SW_MREV
// @DisplayName: Eeprom format version number
// @Description: This value is incremented when changes are made to the eeprom format
// @User: Advanced
// @ReadOnly: True
GSCALAR(format_version, "SYSID_SW_MREV", 0),
// @Param: SYSID_SW_TYPE
// @DisplayName: Software Type
// @Description: This is used by the ground station to recognise the software type (eg ArduPlane vs ArduCopter)
// @Values: 0:ArduPlane,4:AntennaTracker,10:Copter,20:Rover
// @User: Advanced
// @ReadOnly: True
GSCALAR(software_type, "SYSID_SW_TYPE", Parameters::k_software_type),
// @Param: SYSID_THISMAV
// @DisplayName: MAVLink system ID of this vehicle
// @Description: Allows setting an individual MAVLink system id for this vehicle to distinguish it from others on the same network
// @Range: 1 255
// @User: Advanced
GSCALAR(sysid_this_mav, "SYSID_THISMAV", MAV_SYSTEM_ID),
// @Param: SYSID_MYGCS
// @DisplayName: My ground station number
// @Description: Allows restricting radio overrides to only come from my ground station
// @Values: 255:Mission Planner and DroidPlanner, 252: AP Planner 2
// @User: Advanced
GSCALAR(sysid_my_gcs, "SYSID_MYGCS", 255),
#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
// @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),
// @Param: PILOT_THR_BHV
// @DisplayName: Throttle stick behavior
// @Description: Bitmask containing various throttle stick options. Add up the values for options that you want.
// @User: Standard
// @Values: 0:None,1:Feedback from mid stick,2:High throttle cancels landing,4:Disarm on land detection
// @Bitmask: 0:Feedback from mid stick,1:High throttle cancels landing,2:Disarm on land detection
GSCALAR(throttle_behavior, "PILOT_THR_BHV", 0),
// @Group: SERIAL
// @Path: ../libraries/AP_SerialManager/AP_SerialManager.cpp
GOBJECT(serial_manager, "SERIAL", AP_SerialManager),
// @Param: GCS_PID_MASK
// @DisplayName: GCS PID tuning mask
// @Description: bitmask of PIDs to send MAVLink PID_TUNING messages for
// @User: Advanced
// @Values: 0:None,1:Roll,2:Pitch,4:Yaw
// @Bitmask: 0:Roll,1:Pitch,2:Yaw
GSCALAR(gcs_pid_mask, "GCS_PID_MASK", 0),
// @Param: RTL_ALT
// @DisplayName: RTL Altitude
// @Description: The minimum relative altitude the model will move to before Returning to Launch. Set to zero to return at current altitude.
// @Units: Centimeters
// @Range: 0 8000
// @Increment: 1
// @User: Standard
GSCALAR(rtl_altitude, "RTL_ALT", RTL_ALT),
// @Param: RTL_CONE_SLOPE
// @DisplayName: RTL cone slope
// @Description: Defines a cone above home which determines maximum climb
// @Range: 0.5 10.0
// @Increment: .1
// @Values: 0:Disabled,1:Shallow,3:Steep
// @User: Standard
GSCALAR(rtl_cone_slope, "RTL_CONE_SLOPE", RTL_CONE_SLOPE_DEFAULT),
// @Param: RTL_SPEED
// @DisplayName: RTL speed
// @Description: Defines the speed in cm/s which the aircraft will attempt to maintain horizontally while flying home. If this is set to zero, WPNAV_SPEED will be used instead.
// @Units: cm/s
// @Range: 0 2000
// @Increment: 50
// @User: Standard
GSCALAR(rtl_speed_cms, "RTL_SPEED", 0),
// @Param: RNGFND_GAIN
// @DisplayName: Rangefinder gain
// @Description: Used to adjust the speed with which the target altitude is changed when objects are sensed below the copter
// @Range: 0.01 2.0
// @Increment: 0.01
// @User: Standard
GSCALAR(rangefinder_gain, "RNGFND_GAIN", RANGEFINDER_GAIN_DEFAULT),
// @Param: FS_BATT_ENABLE
// @DisplayName: Battery Failsafe Enable
// @Description: Controls whether failsafe will be invoked when battery voltage or current runs low
// @Values: 0:Disabled,1:Land,2:RTL
// @User: Standard
GSCALAR(failsafe_battery_enabled, "FS_BATT_ENABLE", FS_BATT_DISABLED),
// @Param: FS_BATT_VOLTAGE
// @DisplayName: Failsafe battery voltage
// @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
// @Units: Volts
// @Increment: 0.1
// @User: Standard
GSCALAR(fs_batt_voltage, "FS_BATT_VOLTAGE", FS_BATT_VOLTAGE_DEFAULT),
// @Param: FS_BATT_MAH
// @DisplayName: Failsafe battery milliAmpHours
// @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
// @Units: mAh
// @Increment: 50
// @User: Standard
GSCALAR(fs_batt_mah, "FS_BATT_MAH", FS_BATT_MAH_DEFAULT),
// @Param: FS_GCS_ENABLE
// @DisplayName: Ground Station Failsafe Enable
// @Description: Controls what action to take when GCS heartbeat is lost.
// @Values: 0:Disabled,1:Warn only,2:Disarm,3:Enter depth hold mode,4:Enter surface mode
// @User: Standard
GSCALAR(failsafe_gcs, "FS_GCS_ENABLE", FS_GCS_DISABLED),
// @Param: FS_LEAK_ENABLE
// @DisplayName: Leak Failsafe Enable
// @Description: Controls what action to take if a leak is detected.
// @Values: 0:Disabled,1:Warn only,2:Enter surface mode
// @User: Standard
GSCALAR(failsafe_leak, "FS_LEAK_ENABLE", FS_LEAK_DISABLED),
// @Param: FS_PRESS_ENABLE
// @DisplayName: Internal Pressure Failsafe Enable
// @Description: Controls what action to take if internal pressure exceeds FS_PRESS_MAX parameter.
// @Values: 0:Disabled,1:Warn only
// @User: Standard
GSCALAR(failsafe_pressure, "FS_PRESS_ENABLE", FS_PRESS_DISABLED),
// @Param: FS_TEMP_ENABLE
// @DisplayName: Internal Temperature Failsafe Enable
// @Description: Controls what action to take if internal temperature exceeds FS_TEMP_MAX parameter.
// @Values: 0:Disabled,1:Warn only
// @User: Standard
GSCALAR(failsafe_temperature, "FS_TEMP_ENABLE", FS_TEMP_DISABLED),
// @Param: FS_PRESS_MAX
// @DisplayName: Internal Pressure Failsafe Threshold
// @Description: The maximum internal pressure allowed before triggering failsafe. Failsafe action is determined by FS_PRESS_ENABLE parameter
// @Units: Pascal
// @User: Standard
GSCALAR(failsafe_pressure_max, "FS_PRESS_MAX", FS_PRESS_MAX_DEFAULT),
// @Param: FS_TEMP_MAX
// @DisplayName: Internal Temperature Failsafe Threshold
// @Description: The maximum internal temperature allowed before triggering failsafe. Failsafe action is determined by FS_TEMP_ENABLE parameter.
// @Units: Degrees Centigrade
// @User: Standard
GSCALAR(failsafe_temperature_max, "FS_TEMP_MAX", FS_TEMP_MAX_DEFAULT),
// @Param: FS_TERRAIN_ENAB
// @DisplayName: Terrain Failsafe Enable
// @Description: Controls what action to take if terrain information is lost during AUTO mode
// @Values: 0:Disarm, 1:Hold Position, 2:Surface
// @User: Standard
GSCALAR(failsafe_terrain, "FS_TERRAIN_ENAB", FS_TERRAIN_DISARM),
// @Param: XTRACK_ANG_LIM
// @DisplayName: Crosstrack correction angle limit
// @Description: Maximum allowed angle (in degrees) between current track and desired heading during waypoint navigation
// @Range: 10 90
// @User: Standard
GSCALAR(xtrack_angle_limit,"XTRACK_ANG_LIM", 45),
// @Param: GPS_HDOP_GOOD
// @DisplayName: GPS Hdop Good
// @Description: GPS Hdop value at or below this value represent a good position. Used for pre-arm checks
// @Range: 100 900
// @User: Advanced
GSCALAR(gps_hdop_good, "GPS_HDOP_GOOD", GPS_HDOP_GOOD_DEFAULT),
// @Param: MAG_ENABLE
// @DisplayName: Compass enable/disable
// @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: RTL_ALT_FINAL
// @DisplayName: RTL Final Altitude
// @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.
// @Units: Centimeters
// @Range: -1 1000
// @Increment: 1
// @User: Standard
GSCALAR(rtl_alt_final, "RTL_ALT_FINAL", RTL_ALT_FINAL),
// @Param: RTL_CLIMB_MIN
// @DisplayName: RTL minimum climb
// @Description: The vehicle will climb this many cm during the initial climb portion of the RTL
// @Units: Centimeters
// @Range: 0 3000
// @Increment: 10
// @User: Standard
GSCALAR(rtl_climb_min, "RTL_CLIMB_MIN", RTL_CLIMB_MIN_DEFAULT),
// @Param: WP_YAW_BEHAVIOR
// @DisplayName: Yaw behaviour during missions
// @Description: Determines how the autopilot controls the yaw during missions and RTL
// @Values: 0:Never change yaw, 1:Face next waypoint, 2:Face next waypoint except RTL, 3:Face along GPS course
// @User: Standard
GSCALAR(wp_yaw_behavior, "WP_YAW_BEHAVIOR", WP_YAW_BEHAVIOR_DEFAULT),
// @Param: RTL_LOIT_TIME
// @DisplayName: RTL loiter time
// @Description: Time (in milliseconds) to loiter above home before beginning final descent
// @Units: ms
// @Range: 0 60000
// @Increment: 1000
// @User: Standard
GSCALAR(rtl_loiter_time, "RTL_LOIT_TIME", RTL_LOITER_TIME),
// @Param: PILOT_VELZ_MAX
// @DisplayName: Pilot maximum vertical speed
// @Description: The maximum vertical velocity the pilot may request in cm/s
// @Units: Centimeters/Second
// @Range: 50 500
// @Increment: 10
// @User: Standard
GSCALAR(pilot_velocity_z_max, "PILOT_VELZ_MAX", PILOT_VELZ_MAX),
// @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),
// @Param: FS_THR_ENABLE
// @DisplayName: Throttle Failsafe Enable
// @Description: The throttle failsafe allows you to configure a software failsafe activated by a setting on the throttle input channel
// @Values: 0:Disabled,1:Enabled always RTL,2:Enabled Continue with Mission in Auto Mode,3:Enabled always LAND
// @User: Standard
GSCALAR(failsafe_throttle, "FS_THR_ENABLE", FS_THR_DISABLED),
// @Param: FS_THR_VALUE
// @DisplayName: Throttle Failsafe Value
// @Description: The PWM level on channel 3 below which throttle sailsafe triggers
// @Range: 925 1100
// @Units: pwm
// @Increment: 1
// @User: Standard
GSCALAR(failsafe_throttle_value, "FS_THR_VALUE", FS_THR_VALUE_DEFAULT),
// @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),
// @Param: FLTMODE1
// @DisplayName: Flight Mode 1
// @Description: Flight mode when Channel 5 pwm is <= 1230
// @Values: 0:Stabilize,2:DepthHold,19:Manual
// @User: Standard
GSCALAR(flight_mode1, "FLTMODE1", FLIGHT_MODE_1),
// @Param: FLTMODE2
// @DisplayName: Flight Mode 2
// @Description: Flight mode when Channel 5 pwm is >1230, <= 1360
// @Values: 0:Stabilize,2:DepthHold,19:Manual
// @User: Standard
GSCALAR(flight_mode2, "FLTMODE2", FLIGHT_MODE_2),
// @Param: FLTMODE3
// @DisplayName: Flight Mode 3
// @Description: Flight mode when Channel 5 pwm is >1360, <= 1490
// @Values: 0:Stabilize,2:DepthHold,19:Manual
// @User: Standard
GSCALAR(flight_mode3, "FLTMODE3", FLIGHT_MODE_3),
// @Param: FLTMODE4
// @DisplayName: Flight Mode 4
// @Description: Flight mode when Channel 5 pwm is >1490, <= 1620
// @Values: 0:Stabilize,2:DepthHold,19:Manual
// @User: Standard
GSCALAR(flight_mode4, "FLTMODE4", FLIGHT_MODE_4),
// @Param: FLTMODE5
// @DisplayName: Flight Mode 5
// @Description: Flight mode when Channel 5 pwm is >1620, <= 1749
// @Values: 0:Stabilize,2:DepthHold,19:Manual
// @User: Standard
GSCALAR(flight_mode5, "FLTMODE5", FLIGHT_MODE_5),
// @Param: FLTMODE6
// @DisplayName: Flight Mode 6
// @Description: Flight mode when Channel 5 pwm is >=1750
// @Values: 0:Stabilize,2:DepthHold,19:Manual
// @User: Standard
GSCALAR(flight_mode6, "FLTMODE6", FLIGHT_MODE_6),
// @Param: LOG_BITMASK
// @DisplayName: Log bitmask
// @Description: 4 byte bitmap of log types to enable
// @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,397310:All+FastIMU+PID,655358:All+FullIMU,0:Disabled
// @Bitmask: 0:ATTITUDE_FAST,1:ATTITUDE_MED,2:GPS,3:PM,4:CTUN,5:NTUN,6:RCIN,7:IMU,8:CMD,9:CURRENT,10:RCOUT,11:OPTFLOW,12:PID,13:COMPASS,14:INAV,15:CAMERA,16:WHEN_DISARMED,17:MOTBATT,18:IMU_FAST,19:IMU_RAW
// @User: Standard
GSCALAR(log_bitmask, "LOG_BITMASK", DEFAULT_LOG_BITMASK),
// @Param: ESC_CALIBRATION
// @DisplayName: ESC Calibration
// @Description: Controls whether ArduCopter will enter ESC calibration on the next restart. Do not adjust this parameter manually.
// @User: Advanced
// @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, 9:Disabled
GSCALAR(esc_calibrate, "ESC_CALIBRATION", 0),
// @Param: TUNE
// @DisplayName: Channel 6 Tuning
// @Description: Controls which parameters (normally PID gains) are being tuned with transmitter's channel 6 knob
// @User: Standard
// @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
GSCALAR(radio_tuning, "TUNE", 0),
// @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
GSCALAR(radio_tuning_low, "TUNE_LOW", 0),
// @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
GSCALAR(radio_tuning_high, "TUNE_HIGH", 1000),
#if AUXSW_ENABLED == ENABLED
// @Param: CH7_OPT
// @DisplayName: Channel 7 option
// @Description: Select which function if performed when CH7 is above 1800 pwm
// @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:Gripper, 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, 34:Relay2 On/Off, 35:Relay3 On/Off, 36:Relay4 On/Off, 29:Landing Gear, 30:Lost Copter Sound, 31:Motor Emergency Stop, 32:Motor Interlock, 33:Brake, 37:Throw
// @User: Standard
GSCALAR(ch7_option, "CH7_OPT", AUXSW_DO_NOTHING),
// @Param: CH8_OPT
// @DisplayName: Channel 8 option
// @Description: Select which function if performed when CH8 is above 1800 pwm
// @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:Gripper, 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, 34:Relay2 On/Off, 35:Relay3 On/Off, 36:Relay4 On/Off, 29:Landing Gear, 30:Lost Copter Sound, 31:Motor Emergency Stop, 32:Motor Interlock, 33:Brake, 37:Throw
// @User: Standard
GSCALAR(ch8_option, "CH8_OPT", AUXSW_DO_NOTHING),
// @Param: CH9_OPT
// @DisplayName: Channel 9 option
// @Description: Select which function if performed when CH9 is above 1800 pwm
// @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:Gripper, 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, 34:Relay2 On/Off, 35:Relay3 On/Off, 36:Relay4 On/Off, 29:Landing Gear, 30:Lost Copter Sound, 31:Motor Emergency Stop, 32:Motor Interlock, 33:Brake, 37:Throw
// @User: Standard
GSCALAR(ch9_option, "CH9_OPT", AUXSW_DO_NOTHING),
// @Param: CH10_OPT
// @DisplayName: Channel 10 option
// @Description: Select which function if performed when CH10 is above 1800 pwm
// @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:Gripper, 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, 34:Relay2 On/Off, 35:Relay3 On/Off, 36:Relay4 On/Off, 29:Landing Gear, 30:Lost Copter Sound, 31:Motor Emergency Stop, 32:Motor Interlock, 33:Brake, 37:Throw
// @User: Standard
GSCALAR(ch10_option, "CH10_OPT", AUXSW_DO_NOTHING),
// @Param: CH11_OPT
// @DisplayName: Channel 11 option
// @Description: Select which function if performed when CH11 is above 1800 pwm
// @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:Gripper, 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, 34:Relay2 On/Off, 35:Relay3 On/Off, 36:Relay4 On/Off, 29:Landing Gear, 30:Lost Copter Sound, 31:Motor Emergency Stop, 32:Motor Interlock, 33:Brake, 37:Throw
// @User: Standard
GSCALAR(ch11_option, "CH11_OPT", AUXSW_DO_NOTHING),
// @Param: CH12_OPT
// @DisplayName: Channel 12 option
// @Description: Select which function if performed when CH12 is above 1800 pwm
// @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:Gripper, 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, 34:Relay2 On/Off, 35:Relay3 On/Off, 36:Relay4 On/Off, 29:Landing Gear, 30:Lost Copter Sound, 31:Motor Emergency Stop, 32:Motor Interlock, 33:Brake, 37:Throw
// @User: Standard
GSCALAR(ch12_option, "CH12_OPT", AUXSW_DO_NOTHING),
#endif
// @Param: ARMING_CHECK
// @DisplayName: Arming check
// @Description: Allows enabling or disabling of pre-arming checks of receiver, accelerometer, barometer, compass and GPS
// @Values: 0:Disabled, 1:Enabled, -3:Skip Baro, -5:Skip Compass, -9:Skip GPS, -17:Skip INS, -33:Skip Params/Rangefinder, -65:Skip RC, 127:Skip Voltage
// @Bitmask: 0:All,1:Baro,2:Compass,3:GPS,4:INS,5:Parameters+Rangefinder,6:RC,7:Voltage
// @User: Standard
GSCALAR(arming_check, "ARMING_CHECK", ARMING_CHECK_NONE),
// @Param: DISARM_DELAY
// @DisplayName: Disarm delay
// @Description: Delay before automatic disarm in seconds. A value of zero disables auto disarm.
// @Units: Seconds
// @Range: 0 127
// @User: Advanced
GSCALAR(disarm_delay, "DISARM_DELAY", AUTO_DISARMING_DELAY),
// @Param: ANGLE_MAX
// @DisplayName: Angle Max
// @Description: Maximum lean angle in all flight modes
// @Units: Centi-degrees
// @Range: 1000 8000
// @User: Advanced
ASCALAR(angle_max, "ANGLE_MAX", DEFAULT_ANGLE_MAX),
// @Param: RC_FEEL_RP
// @DisplayName: RC Feel Roll/Pitch
// @Description: RC feel for roll/pitch which controls vehicle response to user input with 0 being extremely soft and 100 being crisp
// @Range: 0 100
// @Increment: 10
// @User: Standard
// @Values: 0:Very Soft, 25:Soft, 50:Medium, 75:Crisp, 100:Very Crisp
GSCALAR(rc_feel_rp, "RC_FEEL_RP", RC_FEEL_RP_MEDIUM),
// @Param: FS_EKF_ACTION
// @DisplayName: EKF Failsafe Action
// @Description: Controls the action that will be taken when an EKF failsafe is invoked
// @Values: 1:Land, 2:AltHold, 3:Land even in Stabilize
// @User: Advanced
GSCALAR(fs_ekf_action, "FS_EKF_ACTION", FS_EKF_ACTION_DEFAULT),
// @Param: FS_EKF_THRESH
// @DisplayName: EKF failsafe variance threshold
// @Description: Allows setting the maximum acceptable compass and velocity variance
// @Values: 0.6:Strict, 0.8:Default, 1.0:Relaxed
// @User: Advanced
GSCALAR(fs_ekf_thresh, "FS_EKF_THRESH", FS_EKF_THRESHOLD_DEFAULT),
// @Param: FS_CRASH_CHECK
// @DisplayName: Crash check enable
// @Description: This enables automatic crash checking. When enabled the motors will disarm if a crash is detected.
// @Values: 0:Disabled, 1:Enabled
// @User: Advanced
GSCALAR(fs_crash_check, "FS_CRASH_CHECK", 0),
// 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_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_5, "RC5_", RC_Channel_aux),
// @Group: RC6_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_6, "RC6_", RC_Channel_aux),
// @Group: RC7_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_7, "RC7_", RC_Channel_aux),
// @Group: RC8_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_8, "RC8_", RC_Channel_aux),
// @Group: RC9_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_9, "RC9_", RC_Channel_aux),
// @Group: RC10_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_10, "RC10_", RC_Channel_aux),
// @Group: RC11_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_11, "RC11_", RC_Channel_aux),
// @Group: RC12_
// @Path: ../libraries/RC_Channel/RC_Channel.cpp,../libraries/RC_Channel/RC_Channel_aux.cpp
GGROUP(rc_12, "RC12_", RC_Channel_aux),
// @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),
// @Param: JS_GAIN_DEFAULT
// @DisplayName: Default gain at boot
// @Description: Default gain at boot, must be in range [JS_GAIN_MIN , JS_GAIN_MAX]
// @User: Standard
// @Range: 0.1 1.0
GSCALAR(gain_default, "JS_GAIN_DEFAULT", 0.5),
// @Param: JS_GAIN_MAX
// @DisplayName: Maximum joystick gain
// @Description: Maximum joystick gain
// @User: Standard
// @Range: 0.2 1.0
GSCALAR(maxGain, "JS_GAIN_MAX", 1.0),
// @Param: JS_GAIN_MIN
// @DisplayName: Minimum joystick gain
// @Description: Minimum joystick gain
// @User: Standard
// @Range: 0.1 0.8
GSCALAR(minGain, "JS_GAIN_MIN", 0.25),
// @Param: JS_GAIN_STEPS
// @DisplayName: Gain steps
// @Description: Controls the number of steps between minimum and maximum joystick gain when the gain is adjusted using buttons. Set to 1 to always use JS_GAIN_DEFAULT.
// @User: Standard
// @Range: 1 10
GSCALAR(numGainSettings, "JS_GAIN_STEPS", 4),
// @Param: JS_CAM_TILT_STEP
// @DisplayName: Camera tilt step size
// @Description: Size of PWM increment on camera tilt servo
// @User: Standard
// @Range: 30 400
GSCALAR(cam_tilt_step, "JS_CAM_TILT_STEP", 50),
// @Param: JS_LIGHTS_STEP
// @DisplayName: Lights step size
// @Description: Size of PWM increment on lights servo
// @User: Standard
// @Range: 30 400
GSCALAR(lights_step, "JS_LIGHTS_STEP", 100),
// @Group: BTN0_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_0, "BTN0_", JSButton),
// @Group: BTN1_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_1, "BTN1_", JSButton),
// @Group: BTN2_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_2, "BTN2_", JSButton),
// @Group: BTN3_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_3, "BTN3_", JSButton),
// @Group: BTN4_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_4, "BTN4_", JSButton),
// @Group: BTN5_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_5, "BTN5_", JSButton),
// @Group: BTN6_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_6, "BTN6_", JSButton),
// @Group: BTN7_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_7, "BTN7_", JSButton),
// @Group: BTN8_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_8, "BTN8_", JSButton),
// @Group: BTN9_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_9, "BTN9_", JSButton),
// @Group: BTN10_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_10, "BTN10_", JSButton),
// @Group: BTN11_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_11, "BTN11_", JSButton),
// @Group: BTN12_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_12, "BTN12_", JSButton),
// @Group: BTN13_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_13, "BTN13_", JSButton),
// @Group: BTN14_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_14, "BTN14_", JSButton),
// @Group: BTN15_
// @Path: ../libraries/AP_JSButton/AP_JSButton.cpp
GGROUP(jbtn_15, "BTN15_", JSButton),
// @Param: RC_SPEED
// @DisplayName: ESC Update Speed
// @Description: This is the speed in Hertz that your ESCs will receive updates
// @Units: Hz
// @Range: 50 490
// @Increment: 1
// @User: Advanced
GSCALAR(rc_speed, "RC_SPEED", RC_FAST_SPEED),
// @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.
// @Range: 1 10
// @User: Standard
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),
// @Param: ACRO_BAL_ROLL
// @DisplayName: Acro Balance Roll
// @Description: rate at which roll angle returns to level in acro mode. A higher value causes the vehicle to return to level faster.
// @Range: 0 3
// @Increment: 0.1
// @User: Advanced
GSCALAR(acro_balance_roll, "ACRO_BAL_ROLL", ACRO_BALANCE_ROLL),
// @Param: ACRO_BAL_PITCH
// @DisplayName: Acro Balance Pitch
// @Description: rate at which pitch angle returns to level in acro mode. A higher value causes the vehicle to return to level faster.
// @Range: 0 3
// @Increment: 0.1
// @User: Advanced
GSCALAR(acro_balance_pitch, "ACRO_BAL_PITCH", ACRO_BALANCE_PITCH),
// @Param: ACRO_TRAINER
// @DisplayName: Acro Trainer
// @Description: Type of trainer used in acro mode
// @Values: 0:Disabled,1:Leveling,2:Leveling and Limited
// @User: Advanced
GSCALAR(acro_trainer, "ACRO_TRAINER", ACRO_TRAINER_LIMITED),
// @Param: ACRO_EXPO
// @DisplayName: Acro Expo
// @Description: Acro roll/pitch Expo to allow faster rotation when stick at edges
// @Values: 0:Disabled,0.1:Very Low,0.2:Low,0.3:Medium,0.4:High,0.5:Very High
// @User: Advanced
GSCALAR(acro_expo, "ACRO_EXPO", ACRO_EXPO_DEFAULT),
// @Param: VEL_XY_P
// @DisplayName: Velocity (horizontal) P gain
// @Description: Velocity (horizontal) P gain. Converts the difference between desired velocity to a target acceleration
// @Range: 0.1 6.0
// @Increment: 0.1
// @User: Advanced
// @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
// @Range: 0.02 1.00
// @Increment: 0.01
// @User: Advanced
// @Param: VEL_XY_IMAX
// @DisplayName: Velocity (horizontal) integrator maximum
// @Description: Velocity (horizontal) integrator maximum. Constrains the target acceleration that the I gain will output
// @Range: 0 4500
// @Increment: 10
// @Units: cm/s/s
// @User: Advanced
GGROUP(pi_vel_xy, "VEL_XY_", AC_PI_2D),
// @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
// @Range: 1.000 8.000
// @User: Standard
GGROUP(p_vel_z, "VEL_Z_", AC_P),
// @Param: ACCEL_Z_P
// @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
// @Increment: 0.05
// @User: Standard
// @Param: ACCEL_Z_I
// @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
// @Param: ACCEL_Z_IMAX
// @DisplayName: Throttle acceleration controller I gain maximum
// @Description: Throttle acceleration controller I gain maximum. Constrains the maximum pwm that the I term will generate
// @Range: 0 1000
// @Units: Percent*10
// @User: Standard
// @Param: ACCEL_Z_D
// @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
// @Param: ACCEL_Z_FILT_HZ
// @DisplayName: Throttle acceleration filter
// @Description: Filter applied to acceleration to reduce noise. Lower values reduce noise but add delay.
// @Range: 1.000 100.000
// @Units: Hz
// @User: Standard
GGROUP(pid_accel_z, "ACCEL_Z_", AC_PID),
// @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
// @Range: 1.000 3.000
// @User: Standard
GGROUP(p_alt_hold, "POS_Z_", AC_P),
// @Param: POS_XY_P
// @DisplayName: Position (horizonal) controller P gain
// @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
// @Range: 0.500 2.000
// @User: Standard
GGROUP(p_pos_xy, "POS_XY_", AC_P),
#if TRANSECT_ENABLED == ENABLED
GGROUP(pid_crosstrack_control, "XTRACK_", AC_PID),
GGROUP(pid_heading_control, "HEAD_", AC_PID),
#endif
// variables not in the g class which contain EEPROM saved variables
#if CAMERA == ENABLED
// @Group: CAM_
// @Path: ../libraries/AP_Camera/AP_Camera.cpp
GOBJECT(camera, "CAM_", AP_Camera),
#endif
// @Group: RELAY_
// @Path: ../libraries/AP_Relay/AP_Relay.cpp
GOBJECT(relay, "RELAY_", AP_Relay),
// @Group: COMPASS_
// @Path: ../libraries/AP_Compass/AP_Compass.cpp
GOBJECT(compass, "COMPASS_", Compass),
// @Group: INS_
// @Path: ../libraries/AP_InertialSensor/AP_InertialSensor.cpp
GOBJECT(ins, "INS_", AP_InertialSensor),
// @Group: WPNAV_
// @Path: ../libraries/AC_WPNav/AC_WPNav.cpp
GOBJECT(wp_nav, "WPNAV_", AC_WPNav),
// @Group: CIRCLE_
// @Path: ../libraries/AC_WPNav/AC_Circle.cpp
GOBJECT(circle_nav, "CIRCLE_", AC_Circle),
// @Group: ATC_
// @Path: ../libraries/AC_AttitudeControl/AC_AttitudeControl.cpp,../libraries/AC_AttitudeControl/AC_AttitudeControl_Multi.cpp
GOBJECT(attitude_control, "ATC_", AC_AttitudeControl_Multi),
// @Group: POSCON_
// @Path: ../libraries/AC_AttitudeControl/AC_PosControl.cpp
GOBJECT(pos_control, "PSC", AC_PosControl),
// @Group: SR0_
// @Path: GCS_Mavlink.cpp
GOBJECTN(gcs[0], gcs0, "SR0_", GCS_MAVLINK),
// @Group: SR1_
// @Path: GCS_Mavlink.cpp
GOBJECTN(gcs[1], gcs1, "SR1_", GCS_MAVLINK),
// @Group: SR2_
// @Path: GCS_Mavlink.cpp
GOBJECTN(gcs[2], gcs2, "SR2_", GCS_MAVLINK),
// @Group: SR3_
// @Path: GCS_Mavlink.cpp
GOBJECTN(gcs[3], gcs3, "SR3_", GCS_MAVLINK),
// @Group: AHRS_
// @Path: ../libraries/AP_AHRS/AP_AHRS.cpp
GOBJECT(ahrs, "AHRS_", AP_AHRS),
#if MOUNT == ENABLED
// @Group: MNT
// @Path: ../libraries/AP_Mount/AP_Mount.cpp
GOBJECT(camera_mount, "MNT", AP_Mount),
#endif
// @Group: LOG
// @Path: ../libraries/DataFlash/DataFlash.cpp
GOBJECT(DataFlash, "LOG", DataFlash_Class),
// @Group: BATT
// @Path: ../libraries/AP_BattMonitor/AP_BattMonitor.cpp
GOBJECT(battery, "BATT", AP_BattMonitor),
// @Group: BRD_
// @Path: ../libraries/AP_BoardConfig/AP_BoardConfig.cpp
GOBJECT(BoardConfig, "BRD_", AP_BoardConfig),
#if CONFIG_HAL_BOARD == HAL_BOARD_SITL
GOBJECT(sitl, "SIM_", SITL::SITL),
#endif
// @Group: GND_
// @Path: ../libraries/AP_Baro/AP_Baro.cpp
GOBJECT(barometer, "GND_", AP_Baro),
// GPS driver
// @Group: GPS_
// @Path: ../libraries/AP_GPS/AP_GPS.cpp
GOBJECT(gps, "GPS_", AP_GPS),
// Leak detector
// @Group: LEAK
// @Path: ../libraries/AP_LeakDetector/AP_LeakDetector.cpp
GOBJECT(leak_detector, "LEAK", AP_LeakDetector),
// @Group: SCHED_
// @Path: ../libraries/AP_Scheduler/AP_Scheduler.cpp
GOBJECT(scheduler, "SCHED_", AP_Scheduler),
#if AC_FENCE == ENABLED
// @Group: FENCE_
// @Path: ../libraries/AC_Fence/AC_Fence.cpp
GOBJECT(fence, "FENCE_", AC_Fence),
#endif
// @Group: AVOID_
// @Path: ../libraries/AC_Avoidance/AC_Avoid.cpp
GOBJECT(avoid, "AVOID_", AC_Avoid),
#if AC_RALLY == ENABLED
// @Group: RALLY_
// @Path: ../libraries/AP_Rally/AP_Rally.cpp
GOBJECT(rally, "RALLY_", AP_Rally),
#endif
//#if (FRAME_CONFIG == VECTORED_FRAME || FRAME_CONFIG == BLUEROV_FRAME || FRAME_CONFIG == VECTORED6DOF_FRAME || FRAME_CONFIG == SIMPLEROV || FRAME_CONFIG == VECTORED90_FRAME)
// @Group: MOT_
// @Path: ../libraries/AP_Motors/AP_Motors6DOF.cpp
GOBJECT(motors, "MOT_", AP_Motors6DOF),
//#else
// // @Group: MOT_
// // @Path: ../libraries/AP_Motors/AP_MotorsMulticopter.cpp
// GOBJECT(motors, "MOT_", AP_MotorsMulticopter),
//#endif
#if RCMAP_ENABLED == ENABLED
// @Group: RCMAP_
// @Path: ../libraries/AP_RCMapper/AP_RCMapper.cpp
GOBJECT(rcmap, "RCMAP_", RCMapper),
#endif
// @Group: EKF_
// @Path: ../libraries/AP_NavEKF/AP_NavEKF.cpp
GOBJECTN(EKF, NavEKF, "EKF_", NavEKF),
// @Group: EK2_
// @Path: ../libraries/AP_NavEKF2/AP_NavEKF2.cpp
GOBJECTN(EKF2, NavEKF2, "EK2_", NavEKF2),
// @Group: MIS_
// @Path: ../libraries/AP_Mission/AP_Mission.cpp
GOBJECT(mission, "MIS_", AP_Mission),
#if RANGEFINDER_ENABLED == ENABLED
// @Group: RNGFND
// @Path: ../libraries/AP_RangeFinder/RangeFinder.cpp
GOBJECT(rangefinder, "RNGFND", RangeFinder),
#endif
#if AP_TERRAIN_AVAILABLE && AC_TERRAIN
// @Group: TERRAIN_
// @Path: ../libraries/AP_Terrain/AP_Terrain.cpp
GOBJECT(terrain, "TERRAIN_", AP_Terrain),
#endif
#if OPTFLOW == ENABLED
// @Group: FLOW
// @Path: ../libraries/AP_OpticalFlow/OpticalFlow.cpp
GOBJECT(optflow, "FLOW", OpticalFlow),
#endif
#if RPM_ENABLED == ENABLED
// @Group: RPM
// @Path: ../libraries/AP_RPM/AP_RPM.cpp
GOBJECT(rpm_sensor, "RPM", AP_RPM),
#endif
#if AUTOTUNE_ENABLED == ENABLED
// @Param: AUTOTUNE_AXES
// @DisplayName: Autotune axis bitmask
// @Description: 1-byte bitmap of axes to autotune
// @Values: 7:All,1:Roll Only,2:Pitch Only,4:Yaw Only,3:Roll and Pitch,5:Roll and Yaw,6:Pitch and Yaw
// @Bitmask: 0:Roll,1:Pitch,2:Yaw
// @User: Standard
GSCALAR(autotune_axis_bitmask, "AUTOTUNE_AXES", 7), // AUTOTUNE_AXIS_BITMASK_DEFAULT
// @Param: AUTOTUNE_AGGR
// @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
GSCALAR(autotune_aggressiveness, "AUTOTUNE_AGGR", 0.1f),
// @Param: AUTOTUNE_MIN_D
// @DisplayName: AutoTune minimum D
// @Description: Defines the minimum D gain
// @Range: 0.001 0.006
// @User: Standard
GSCALAR(autotune_min_d, "AUTOTUNE_MIN_D", 0.001f),
#endif
// @Group: NTF_
// @Path: ../libraries/AP_Notify/AP_Notify.cpp
GOBJECT(notify, "NTF_", AP_Notify),
// @Param: TERRAIN_FOLLOW
// @DisplayName: Terrain Following use control
// @Description: This enables terrain following for RTL and LAND flight modes. To use this option TERRAIN_ENABLE must be 1 and the GCS must support sending terrain data to the aircraft. In RTL the RTL_ALT will be considered a height above the terrain. In LAND mode the vehicle will slow to LAND_SPEED 10m above terrain (instead of 10m above home). This parameter does not affect AUTO and Guided which use a per-command flag to determine if the height is above-home, absolute or above-terrain.
// @Values: 0:Do Not Use in RTL and Land,1:Use in RTL and Land
// @User: Standard
GSCALAR(terrain_follow, "TERRAIN_FOLLOW", 0),
// @Group:
// @Path: Parameters.cpp
GOBJECT(g2, "", ParametersG2),
AP_VAREND
};
/*
2nd group of parameters
*/
const AP_Param::GroupInfo ParametersG2::var_info[] = {
// @Param: WP_NAVALT_MIN
// @DisplayName: Minimum navigation altitude
// @Description: This is the altitude in meters above which for navigation can begin. This applies in auto takeoff and auto landing.
// @Range: 0 5
// @User: Standard
AP_GROUPINFO("WP_NAVALT_MIN", 1, ParametersG2, wp_navalt_min, 0),
#if PROXIMITY_ENABLED == ENABLED
// @Group: PRX
// @Path: ../libraries/AP_Proximity/AP_Proximity.cpp
AP_SUBGROUPINFO(proximity, "PRX", 2, ParametersG2, AP_Proximity),
#endif
#if GRIPPER_ENABLED == ENABLED
// @Group: GRIP_
// @Path: ../libraries/AP_Gripper/AP_Gripper.cpp
AP_SUBGROUPINFO(gripper, "GRIP_", 3, ParametersG2, AP_Gripper),
#endif
AP_GROUPEND
};
/*
constructor for g2 object
*/
ParametersG2::ParametersG2(void)
: proximity(sub.serial_manager)
{
AP_Param::setup_object_defaults(this, var_info);
}
void Sub::load_parameters(void)
{
if (!AP_Param::check_var_info()) {
cliSerial->printf("Bad var table\n");
AP_HAL::panic("Bad var table");
}
// disable centrifugal force correction, it will be enabled as part of the arming process
ahrs.set_correct_centrifugal(false);
hal.util->set_soft_armed(false);
if (!g.format_version.load() ||
g.format_version != Parameters::k_format_version) {
// erase all parameters
cliSerial->printf("Firmware change: erasing EEPROM...\n");
AP_Param::erase_all();
// save the current format version
g.format_version.set_and_save(Parameters::k_format_version);
cliSerial->println("done.");
}
uint32_t before = micros();
// Load all auto-loaded EEPROM variables
AP_Param::load_all();
cliSerial->printf("load_all took %uus\n", (unsigned)(micros() - before));
}
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