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434 lines
19 KiB
434 lines
19 KiB
#pragma once |
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#include <AP_HAL/AP_HAL_Boards.h> |
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// Just so that it's completely clear... |
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#define ENABLED 1 |
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#define DISABLED 0 |
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// this avoids a very common config error |
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#define ENABLE ENABLED |
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#define DISABLE DISABLED |
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// Autopilot Yaw Mode enumeration |
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enum autopilot_yaw_mode { |
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AUTO_YAW_HOLD = 0, // pilot controls the heading |
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AUTO_YAW_LOOK_AT_NEXT_WP = 1, // point towards next waypoint (no pilot input accepted) |
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AUTO_YAW_ROI = 2, // point towards a location held in roi (no pilot input accepted) |
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AUTO_YAW_FIXED = 3, // point towards a particular angle (no pilot input accepted) |
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AUTO_YAW_LOOK_AHEAD = 4, // point in the direction the copter is moving |
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AUTO_YAW_RESETTOARMEDYAW = 5, // point towards heading at time motors were armed |
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AUTO_YAW_RATE = 6, // turn at a specified rate (held in auto_yaw_rate) |
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}; |
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// Frame types |
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#define UNDEFINED_FRAME 0 |
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#define MULTICOPTER_FRAME 1 |
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#define HELI_FRAME 2 |
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// HIL enumerations |
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#define HIL_MODE_DISABLED 0 |
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#define HIL_MODE_SENSORS 1 |
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// Auto Pilot Modes enumeration |
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enum control_mode_t { |
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STABILIZE = 0, // manual airframe angle with manual throttle |
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ACRO = 1, // manual body-frame angular rate with manual throttle |
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ALT_HOLD = 2, // manual airframe angle with automatic throttle |
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AUTO = 3, // fully automatic waypoint control using mission commands |
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GUIDED = 4, // fully automatic fly to coordinate or fly at velocity/direction using GCS immediate commands |
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LOITER = 5, // automatic horizontal acceleration with automatic throttle |
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RTL = 6, // automatic return to launching point |
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CIRCLE = 7, // automatic circular flight with automatic throttle |
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LAND = 9, // automatic landing with horizontal position control |
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DRIFT = 11, // semi-automous position, yaw and throttle control |
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SPORT = 13, // manual earth-frame angular rate control with manual throttle |
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FLIP = 14, // automatically flip the vehicle on the roll axis |
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AUTOTUNE = 15, // automatically tune the vehicle's roll and pitch gains |
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POSHOLD = 16, // automatic position hold with manual override, with automatic throttle |
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BRAKE = 17, // full-brake using inertial/GPS system, no pilot input |
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THROW = 18, // throw to launch mode using inertial/GPS system, no pilot input |
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AVOID_ADSB = 19, // automatic avoidance of obstacles in the macro scale - e.g. full-sized aircraft |
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GUIDED_NOGPS = 20, // guided mode but only accepts attitude and altitude |
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SMART_RTL = 21, // SMART_RTL returns to home by retracing its steps |
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FLOWHOLD = 22, // FLOWHOLD holds position with optical flow without rangefinder |
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FOLLOW = 23, // follow attempts to follow another vehicle or ground station |
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ZIGZAG = 24, // ZIGZAG mode is able to fly in a zigzag manner with predefined point A and point B |
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}; |
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enum mode_reason_t { |
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MODE_REASON_UNKNOWN=0, |
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MODE_REASON_TX_COMMAND, |
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MODE_REASON_GCS_COMMAND, |
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MODE_REASON_RADIO_FAILSAFE, |
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MODE_REASON_BATTERY_FAILSAFE, |
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MODE_REASON_GCS_FAILSAFE, |
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MODE_REASON_EKF_FAILSAFE, |
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MODE_REASON_GPS_GLITCH, |
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MODE_REASON_MISSION_END, |
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MODE_REASON_THROTTLE_LAND_ESCAPE, |
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MODE_REASON_FENCE_BREACH, |
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MODE_REASON_TERRAIN_FAILSAFE, |
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MODE_REASON_BRAKE_TIMEOUT, |
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MODE_REASON_FLIP_COMPLETE, |
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MODE_REASON_AVOIDANCE, |
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MODE_REASON_AVOIDANCE_RECOVERY, |
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MODE_REASON_THROW_COMPLETE, |
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MODE_REASON_TERMINATE, |
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MODE_REASON_TMODE, |
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}; |
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// Tuning enumeration |
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enum tuning_func { |
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TUNING_NONE = 0, // |
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TUNING_STABILIZE_ROLL_PITCH_KP = 1, // stabilize roll/pitch angle controller's P term |
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TUNING_STABILIZE_YAW_KP = 3, // stabilize yaw heading controller's P term |
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TUNING_RATE_ROLL_PITCH_KP = 4, // body frame roll/pitch rate controller's P term |
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TUNING_RATE_ROLL_PITCH_KI = 5, // body frame roll/pitch rate controller's I term |
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TUNING_YAW_RATE_KP = 6, // body frame yaw rate controller's P term |
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TUNING_THROTTLE_RATE_KP = 7, // throttle rate controller's P term (desired rate to acceleration or motor output) |
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TUNING_WP_SPEED = 10, // maximum speed to next way point (0 to 10m/s) |
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TUNING_LOITER_POSITION_KP = 12, // loiter distance controller's P term (position error to speed) |
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TUNING_HELI_EXTERNAL_GYRO = 13, // TradHeli specific external tail gyro gain |
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TUNING_ALTITUDE_HOLD_KP = 14, // altitude hold controller's P term (alt error to desired rate) |
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TUNING_RATE_ROLL_PITCH_KD = 21, // body frame roll/pitch rate controller's D term |
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TUNING_VEL_XY_KP = 22, // loiter rate controller's P term (speed error to tilt angle) |
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TUNING_ACRO_RP_KP = 25, // acro controller's P term. converts pilot input to a desired roll, pitch or yaw rate |
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TUNING_YAW_RATE_KD = 26, // body frame yaw rate controller's D term |
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TUNING_VEL_XY_KI = 28, // loiter rate controller's I term (speed error to tilt angle) |
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TUNING_AHRS_YAW_KP = 30, // ahrs's compass effect on yaw angle (0 = very low, 1 = very high) |
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TUNING_AHRS_KP = 31, // accelerometer effect on roll/pitch angle (0=low) |
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TUNING_ACCEL_Z_KP = 34, // accel based throttle controller's P term |
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TUNING_ACCEL_Z_KI = 35, // accel based throttle controller's I term |
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TUNING_ACCEL_Z_KD = 36, // accel based throttle controller's D term |
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TUNING_DECLINATION = 38, // compass declination in radians |
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TUNING_CIRCLE_RATE = 39, // circle turn rate in degrees (hard coded to about 45 degrees in either direction) |
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TUNING_ACRO_YAW_KP = 40, // acro controller's P term. converts pilot input to a desired roll, pitch or yaw rate |
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TUNING_RANGEFINDER_GAIN = 41, // rangefinder gain |
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TUNING_EKF_VERTICAL_POS = 42, // EKF's baro vs accel (higher rely on accels more, baro impact is reduced). Range should be 0.2 ~ 4.0? 2.0 is default |
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TUNING_EKF_HORIZONTAL_POS = 43, // EKF's gps vs accel (higher rely on accels more, gps impact is reduced). Range should be 1.0 ~ 3.0? 1.5 is default |
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TUNING_EKF_ACCEL_NOISE = 44, // EKF's accel noise (lower means trust accels more, gps & baro less). Range should be 0.02 ~ 0.5 0.5 is default (but very robust at that level) |
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TUNING_RC_FEEL_RP = 45, // roll-pitch input smoothing |
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TUNING_RATE_PITCH_KP = 46, // body frame pitch rate controller's P term |
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TUNING_RATE_PITCH_KI = 47, // body frame pitch rate controller's I term |
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TUNING_RATE_PITCH_KD = 48, // body frame pitch rate controller's D term |
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TUNING_RATE_ROLL_KP = 49, // body frame roll rate controller's P term |
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TUNING_RATE_ROLL_KI = 50, // body frame roll rate controller's I term |
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TUNING_RATE_ROLL_KD = 51, // body frame roll rate controller's D term |
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TUNING_RATE_PITCH_FF = 52, // body frame pitch rate controller FF term |
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TUNING_RATE_ROLL_FF = 53, // body frame roll rate controller FF term |
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TUNING_RATE_YAW_FF = 54, // body frame yaw rate controller FF term |
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TUNING_RATE_MOT_YAW_HEADROOM = 55, // motors yaw headroom minimum |
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TUNING_RATE_YAW_FILT = 56, // yaw rate input filter |
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TUNING_WINCH = 57 // winch control (not actually a value to be tuned) |
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}; |
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// Acro Trainer types |
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#define ACRO_TRAINER_DISABLED 0 |
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#define ACRO_TRAINER_LEVELING 1 |
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#define ACRO_TRAINER_LIMITED 2 |
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// Yaw behaviours during missions - possible values for WP_YAW_BEHAVIOR parameter |
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#define WP_YAW_BEHAVIOR_NONE 0 // auto pilot will never control yaw during missions or rtl (except for DO_CONDITIONAL_YAW command received) |
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#define WP_YAW_BEHAVIOR_LOOK_AT_NEXT_WP 1 // auto pilot will face next waypoint or home during rtl |
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#define WP_YAW_BEHAVIOR_LOOK_AT_NEXT_WP_EXCEPT_RTL 2 // auto pilot will face next waypoint except when doing RTL at which time it will stay in it's last |
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#define WP_YAW_BEHAVIOR_LOOK_AHEAD 3 // auto pilot will look ahead during missions and rtl (primarily meant for traditional helicopters) |
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// Auto modes |
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enum AutoMode { |
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Auto_TakeOff, |
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Auto_WP, |
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Auto_Land, |
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Auto_RTL, |
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Auto_CircleMoveToEdge, |
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Auto_Circle, |
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Auto_Spline, |
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Auto_NavGuided, |
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Auto_Loiter, |
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Auto_LoiterToAlt, |
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Auto_NavPayloadPlace, |
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}; |
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// Guided modes |
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enum GuidedMode { |
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Guided_TakeOff, |
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Guided_WP, |
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Guided_Velocity, |
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Guided_PosVel, |
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Guided_Angle, |
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}; |
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// RTL states |
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enum RTLState { |
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RTL_InitialClimb, |
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RTL_ReturnHome, |
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RTL_LoiterAtHome, |
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RTL_FinalDescent, |
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RTL_Land |
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}; |
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// Safe RTL states |
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enum SmartRTLState { |
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SmartRTL_WaitForPathCleanup, |
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SmartRTL_PathFollow, |
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SmartRTL_PreLandPosition, |
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SmartRTL_Descend, |
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SmartRTL_Land |
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}; |
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// Alt_Hold states |
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enum AltHoldModeState { |
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AltHold_MotorStopped, |
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AltHold_Takeoff, |
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AltHold_Flying, |
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AltHold_Landed |
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}; |
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// Loiter states |
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enum LoiterModeState { |
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Loiter_MotorStopped, |
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Loiter_Takeoff, |
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Loiter_Flying, |
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Loiter_Landed |
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}; |
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// Sport states |
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enum SportModeState { |
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Sport_MotorStopped, |
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Sport_Takeoff, |
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Sport_Flying, |
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Sport_Landed |
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}; |
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// Flip states |
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enum FlipState { |
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Flip_Start, |
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Flip_Roll, |
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Flip_Pitch_A, |
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Flip_Pitch_B, |
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Flip_Recover, |
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Flip_Abandon |
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}; |
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enum LandStateType { |
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LandStateType_FlyToLocation = 0, |
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LandStateType_Descending = 1 |
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}; |
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enum PayloadPlaceStateType { |
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PayloadPlaceStateType_FlyToLocation, |
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PayloadPlaceStateType_Calibrating_Hover_Start, |
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PayloadPlaceStateType_Calibrating_Hover, |
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PayloadPlaceStateType_Descending_Start, |
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PayloadPlaceStateType_Descending, |
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PayloadPlaceStateType_Releasing_Start, |
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PayloadPlaceStateType_Releasing, |
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PayloadPlaceStateType_Released, |
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PayloadPlaceStateType_Ascending_Start, |
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PayloadPlaceStateType_Ascending, |
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PayloadPlaceStateType_Done, |
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}; |
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// bit options for DEV_OPTIONS parameter |
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enum DevOptions { |
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DevOptionADSBMAVLink = 1, |
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DevOptionVFR_HUDRelativeAlt = 2, |
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}; |
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// Logging parameters |
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enum LoggingParameters { |
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TYPE_AIRSTART_MSG, |
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TYPE_GROUNDSTART_MSG, |
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LOG_CONTROL_TUNING_MSG, |
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LOG_EVENT_MSG, |
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LOG_ERROR_MSG, |
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LOG_DATA_INT16_MSG, |
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LOG_DATA_UINT16_MSG, |
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LOG_DATA_INT32_MSG, |
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LOG_DATA_UINT32_MSG, |
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LOG_DATA_FLOAT_MSG, |
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LOG_AUTOTUNE_MSG, |
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LOG_AUTOTUNEDETAILS_MSG, |
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LOG_MOTBATT_MSG, |
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LOG_PARAMTUNE_MSG, |
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LOG_HELI_MSG, |
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LOG_PRECLAND_MSG, |
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LOG_GUIDEDTARGET_MSG, |
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}; |
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#define MASK_LOG_ATTITUDE_FAST (1<<0) |
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#define MASK_LOG_ATTITUDE_MED (1<<1) |
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#define MASK_LOG_GPS (1<<2) |
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#define MASK_LOG_PM (1<<3) |
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#define MASK_LOG_CTUN (1<<4) |
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#define MASK_LOG_NTUN (1<<5) |
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#define MASK_LOG_RCIN (1<<6) |
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#define MASK_LOG_IMU (1<<7) |
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#define MASK_LOG_CMD (1<<8) |
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#define MASK_LOG_CURRENT (1<<9) |
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#define MASK_LOG_RCOUT (1<<10) |
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#define MASK_LOG_OPTFLOW (1<<11) |
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#define MASK_LOG_PID (1<<12) |
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#define MASK_LOG_COMPASS (1<<13) |
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#define MASK_LOG_INAV (1<<14) // deprecated |
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#define MASK_LOG_CAMERA (1<<15) |
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#define MASK_LOG_MOTBATT (1UL<<17) |
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#define MASK_LOG_IMU_FAST (1UL<<18) |
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#define MASK_LOG_IMU_RAW (1UL<<19) |
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#define MASK_LOG_ANY 0xFFFF |
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// DATA - event logging |
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#define DATA_AP_STATE 7 |
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// 8 was DATA_SYSTEM_TIME_SET |
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#define DATA_INIT_SIMPLE_BEARING 9 |
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#define DATA_ARMED 10 |
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#define DATA_DISARMED 11 |
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#define DATA_AUTO_ARMED 15 |
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#define DATA_LAND_COMPLETE_MAYBE 17 |
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#define DATA_LAND_COMPLETE 18 |
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#define DATA_NOT_LANDED 28 |
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#define DATA_LOST_GPS 19 |
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#define DATA_FLIP_START 21 |
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#define DATA_FLIP_END 22 |
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#define DATA_SET_HOME 25 |
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#define DATA_SET_SIMPLE_ON 26 |
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#define DATA_SET_SIMPLE_OFF 27 |
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#define DATA_SET_SUPERSIMPLE_ON 29 |
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#define DATA_AUTOTUNE_INITIALISED 30 |
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#define DATA_AUTOTUNE_OFF 31 |
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#define DATA_AUTOTUNE_RESTART 32 |
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#define DATA_AUTOTUNE_SUCCESS 33 |
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#define DATA_AUTOTUNE_FAILED 34 |
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#define DATA_AUTOTUNE_REACHED_LIMIT 35 |
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#define DATA_AUTOTUNE_PILOT_TESTING 36 |
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#define DATA_AUTOTUNE_SAVEDGAINS 37 |
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#define DATA_SAVE_TRIM 38 |
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#define DATA_SAVEWP_ADD_WP 39 |
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#define DATA_FENCE_ENABLE 41 |
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#define DATA_FENCE_DISABLE 42 |
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#define DATA_ACRO_TRAINER_DISABLED 43 |
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#define DATA_ACRO_TRAINER_LEVELING 44 |
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#define DATA_ACRO_TRAINER_LIMITED 45 |
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#define DATA_GRIPPER_GRAB 46 |
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#define DATA_GRIPPER_RELEASE 47 |
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#define DATA_PARACHUTE_DISABLED 49 |
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#define DATA_PARACHUTE_ENABLED 50 |
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#define DATA_PARACHUTE_RELEASED 51 |
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#define DATA_LANDING_GEAR_DEPLOYED 52 |
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#define DATA_LANDING_GEAR_RETRACTED 53 |
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#define DATA_MOTORS_EMERGENCY_STOPPED 54 |
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#define DATA_MOTORS_EMERGENCY_STOP_CLEARED 55 |
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#define DATA_MOTORS_INTERLOCK_DISABLED 56 |
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#define DATA_MOTORS_INTERLOCK_ENABLED 57 |
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#define DATA_ROTOR_RUNUP_COMPLETE 58 // Heli only |
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#define DATA_ROTOR_SPEED_BELOW_CRITICAL 59 // Heli only |
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#define DATA_EKF_ALT_RESET 60 |
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#define DATA_LAND_CANCELLED_BY_PILOT 61 |
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#define DATA_EKF_YAW_RESET 62 |
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#define DATA_AVOIDANCE_ADSB_ENABLE 63 |
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#define DATA_AVOIDANCE_ADSB_DISABLE 64 |
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#define DATA_AVOIDANCE_PROXIMITY_ENABLE 65 |
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#define DATA_AVOIDANCE_PROXIMITY_DISABLE 66 |
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#define DATA_GPS_PRIMARY_CHANGED 67 |
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#define DATA_WINCH_RELAXED 68 |
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#define DATA_WINCH_LENGTH_CONTROL 69 |
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#define DATA_WINCH_RATE_CONTROL 70 |
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#define DATA_ZIGZAG_STORE_A 71 |
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#define DATA_ZIGZAG_STORE_B 72 |
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#define DATA_LAND_REPO_ACTIVE 73 |
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// Error message sub systems and error codes |
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#define ERROR_SUBSYSTEM_MAIN 1 |
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#define ERROR_SUBSYSTEM_RADIO 2 |
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#define ERROR_SUBSYSTEM_COMPASS 3 |
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#define ERROR_SUBSYSTEM_OPTFLOW 4 |
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#define ERROR_SUBSYSTEM_FAILSAFE_RADIO 5 |
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#define ERROR_SUBSYSTEM_FAILSAFE_BATT 6 |
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#define ERROR_SUBSYSTEM_FAILSAFE_GPS 7 // not used |
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#define ERROR_SUBSYSTEM_FAILSAFE_GCS 8 |
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#define ERROR_SUBSYSTEM_FAILSAFE_FENCE 9 |
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#define ERROR_SUBSYSTEM_FLIGHT_MODE 10 |
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#define ERROR_SUBSYSTEM_GPS 11 |
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#define ERROR_SUBSYSTEM_CRASH_CHECK 12 |
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#define ERROR_SUBSYSTEM_FLIP 13 |
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#define ERROR_SUBSYSTEM_AUTOTUNE 14 |
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#define ERROR_SUBSYSTEM_PARACHUTE 15 |
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#define ERROR_SUBSYSTEM_EKFCHECK 16 |
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#define ERROR_SUBSYSTEM_FAILSAFE_EKFINAV 17 |
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#define ERROR_SUBSYSTEM_BARO 18 |
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#define ERROR_SUBSYSTEM_CPU 19 |
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#define ERROR_SUBSYSTEM_FAILSAFE_ADSB 20 |
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#define ERROR_SUBSYSTEM_TERRAIN 21 |
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#define ERROR_SUBSYSTEM_NAVIGATION 22 |
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#define ERROR_SUBSYSTEM_FAILSAFE_TERRAIN 23 |
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#define ERROR_SUBSYSTEM_EKF_PRIMARY 24 |
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#define ERROR_SUBSYSTEM_THRUST_LOSS_CHECK 25 |
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// general error codes |
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#define ERROR_CODE_ERROR_RESOLVED 0 |
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#define ERROR_CODE_FAILED_TO_INITIALISE 1 |
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#define ERROR_CODE_UNHEALTHY 4 |
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// subsystem specific error codes -- radio |
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#define ERROR_CODE_RADIO_LATE_FRAME 2 |
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// subsystem specific error codes -- failsafe_thr, batt, gps |
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#define ERROR_CODE_FAILSAFE_RESOLVED 0 |
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#define ERROR_CODE_FAILSAFE_OCCURRED 1 |
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// subsystem specific error codes -- compass |
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#define ERROR_CODE_COMPASS_FAILED_TO_READ 2 |
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// subsystem specific error codes -- main |
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#define ERROR_CODE_MAIN_INS_DELAY 1 |
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// subsystem specific error codes -- crash checker |
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#define ERROR_CODE_CRASH_CHECK_CRASH 1 |
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#define ERROR_CODE_CRASH_CHECK_LOSS_OF_CONTROL 2 |
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// subsystem specific error codes -- flip |
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#define ERROR_CODE_FLIP_ABANDONED 2 |
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// subsystem specific error codes -- terrain |
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#define ERROR_CODE_MISSING_TERRAIN_DATA 2 |
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// subsystem specific error codes -- navigation |
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#define ERROR_CODE_FAILED_TO_SET_DESTINATION 2 |
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#define ERROR_CODE_RESTARTED_RTL 3 |
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#define ERROR_CODE_FAILED_CIRCLE_INIT 4 |
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#define ERROR_CODE_DEST_OUTSIDE_FENCE 5 |
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// parachute failed to deploy because of low altitude or landed |
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#define ERROR_CODE_PARACHUTE_TOO_LOW 2 |
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#define ERROR_CODE_PARACHUTE_LANDED 3 |
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// EKF check definitions |
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#define ERROR_CODE_EKFCHECK_BAD_VARIANCE 2 |
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#define ERROR_CODE_EKFCHECK_VARIANCE_CLEARED 0 |
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// Baro specific error codes |
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#define ERROR_CODE_BARO_GLITCH 2 |
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// GPS specific error coces |
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#define ERROR_CODE_GPS_GLITCH 2 |
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// Radio failsafe definitions (FS_THR parameter) |
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#define FS_THR_DISABLED 0 |
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#define FS_THR_ENABLED_ALWAYS_RTL 1 |
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#define FS_THR_ENABLED_CONTINUE_MISSION 2 |
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#define FS_THR_ENABLED_ALWAYS_LAND 3 |
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#define FS_THR_ENABLED_ALWAYS_SMARTRTL_OR_RTL 4 |
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#define FS_THR_ENABLED_ALWAYS_SMARTRTL_OR_LAND 5 |
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// GCS failsafe definitions (FS_GCS_ENABLE parameter) |
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#define FS_GCS_DISABLED 0 |
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#define FS_GCS_ENABLED_ALWAYS_RTL 1 |
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#define FS_GCS_ENABLED_CONTINUE_MISSION 2 |
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#define FS_GCS_ENABLED_ALWAYS_SMARTRTL_OR_RTL 3 |
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#define FS_GCS_ENABLED_ALWAYS_SMARTRTL_OR_LAND 4 |
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// EKF failsafe definitions (FS_EKF_ACTION parameter) |
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#define FS_EKF_ACTION_LAND 1 // switch to LAND mode on EKF failsafe |
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#define FS_EKF_ACTION_ALTHOLD 2 // switch to ALTHOLD mode on EKF failsafe |
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#define FS_EKF_ACTION_LAND_EVEN_STABILIZE 3 // switch to Land mode on EKF failsafe even if in a manual flight mode like stabilize |
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// for mavlink SET_POSITION_TARGET messages |
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#define MAVLINK_SET_POS_TYPE_MASK_POS_IGNORE ((1<<0) | (1<<1) | (1<<2)) |
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#define MAVLINK_SET_POS_TYPE_MASK_VEL_IGNORE ((1<<3) | (1<<4) | (1<<5)) |
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#define MAVLINK_SET_POS_TYPE_MASK_ACC_IGNORE ((1<<6) | (1<<7) | (1<<8)) |
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#define MAVLINK_SET_POS_TYPE_MASK_FORCE (1<<9) |
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#define MAVLINK_SET_POS_TYPE_MASK_YAW_IGNORE (1<<10) |
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#define MAVLINK_SET_POS_TYPE_MASK_YAW_RATE_IGNORE (1<<11) |
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// for PILOT_THR_BHV parameter |
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#define THR_BEHAVE_FEEDBACK_FROM_MID_STICK (1<<0) |
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#define THR_BEHAVE_HIGH_THROTTLE_CANCELS_LAND (1<<1) |
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#define THR_BEHAVE_DISARM_ON_LAND_DETECT (1<<2)
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