#include "GCS_Plane.h" #include "Plane.h" uint8_t GCS_Plane::sysid_this_mav() const { return plane.g.sysid_this_mav; } void GCS_Plane::update_vehicle_sensor_status_flags(void) { // reverse thrust if (plane.have_reverse_thrust()) { control_sensors_present |= MAV_SYS_STATUS_REVERSE_MOTOR; } if (plane.have_reverse_thrust() && is_negative(SRV_Channels::get_output_scaled(SRV_Channel::k_throttle))) { control_sensors_enabled |= MAV_SYS_STATUS_REVERSE_MOTOR; control_sensors_health |= MAV_SYS_STATUS_REVERSE_MOTOR; } // flightmode-specific control_sensors_present |= MAV_SYS_STATUS_SENSOR_ANGULAR_RATE_CONTROL | MAV_SYS_STATUS_SENSOR_ATTITUDE_STABILIZATION | MAV_SYS_STATUS_SENSOR_YAW_POSITION | MAV_SYS_STATUS_SENSOR_Z_ALTITUDE_CONTROL | MAV_SYS_STATUS_SENSOR_XY_POSITION_CONTROL; bool rate_controlled = false; bool attitude_stabilized = false; switch (plane.control_mode->mode_number()) { case Mode::Number::MANUAL: break; case Mode::Number::ACRO: #if HAL_QUADPLANE_ENABLED case Mode::Number::QACRO: #endif rate_controlled = true; break; case Mode::Number::STABILIZE: case Mode::Number::FLY_BY_WIRE_A: case Mode::Number::AUTOTUNE: #if HAL_QUADPLANE_ENABLED case Mode::Number::QSTABILIZE: case Mode::Number::QHOVER: case Mode::Number::QLAND: case Mode::Number::QLOITER: #if QAUTOTUNE_ENABLED case Mode::Number::QAUTOTUNE: #endif #endif // HAL_QUADPLANE_ENABLED case Mode::Number::FLY_BY_WIRE_B: case Mode::Number::CRUISE: rate_controlled = true; attitude_stabilized = true; break; case Mode::Number::TRAINING: if (!plane.training_manual_roll || !plane.training_manual_pitch) { rate_controlled = true; attitude_stabilized = true; } break; case Mode::Number::AUTO: case Mode::Number::RTL: case Mode::Number::LOITER: case Mode::Number::AVOID_ADSB: case Mode::Number::GUIDED: case Mode::Number::CIRCLE: case Mode::Number::TAKEOFF: #if HAL_QUADPLANE_ENABLED case Mode::Number::QRTL: case Mode::Number::LOITER_ALT_QLAND: #endif case Mode::Number::THERMAL: rate_controlled = true; attitude_stabilized = true; control_sensors_enabled |= MAV_SYS_STATUS_SENSOR_YAW_POSITION; control_sensors_health |= MAV_SYS_STATUS_SENSOR_YAW_POSITION; control_sensors_enabled |= MAV_SYS_STATUS_SENSOR_Z_ALTITUDE_CONTROL; control_sensors_health |= MAV_SYS_STATUS_SENSOR_Z_ALTITUDE_CONTROL; control_sensors_enabled |= MAV_SYS_STATUS_SENSOR_XY_POSITION_CONTROL; control_sensors_health |= MAV_SYS_STATUS_SENSOR_XY_POSITION_CONTROL; break; case Mode::Number::INITIALISING: break; } if (rate_controlled) { control_sensors_enabled |= MAV_SYS_STATUS_SENSOR_ANGULAR_RATE_CONTROL; // 3D angular rate control control_sensors_health |= MAV_SYS_STATUS_SENSOR_ANGULAR_RATE_CONTROL; // 3D angular rate control } if (attitude_stabilized) { control_sensors_enabled |= MAV_SYS_STATUS_SENSOR_ATTITUDE_STABILIZATION; control_sensors_health |= MAV_SYS_STATUS_SENSOR_ATTITUDE_STABILIZATION; } #if AP_TERRAIN_AVAILABLE switch (plane.terrain.status()) { case AP_Terrain::TerrainStatusDisabled: break; case AP_Terrain::TerrainStatusUnhealthy: control_sensors_present |= MAV_SYS_STATUS_TERRAIN; control_sensors_enabled |= MAV_SYS_STATUS_TERRAIN; break; case AP_Terrain::TerrainStatusOK: control_sensors_present |= MAV_SYS_STATUS_TERRAIN; control_sensors_enabled |= MAV_SYS_STATUS_TERRAIN; control_sensors_health |= MAV_SYS_STATUS_TERRAIN; break; } #endif #if AP_RANGEFINDER_ENABLED const RangeFinder *rangefinder = RangeFinder::get_singleton(); if (rangefinder && rangefinder->has_orientation(ROTATION_PITCH_270)) { control_sensors_present |= MAV_SYS_STATUS_SENSOR_LASER_POSITION; if (plane.g.rangefinder_landing) { control_sensors_enabled |= MAV_SYS_STATUS_SENSOR_LASER_POSITION; } if (rangefinder->has_data_orient(ROTATION_PITCH_270)) { control_sensors_health |= MAV_SYS_STATUS_SENSOR_LASER_POSITION; } } #endif }