void Sub::set_land_complete(bool b)
{
// if no change, exit immediately
if( ap.land_complete == b )
return;
land_detector_count = 0;
if(b){
Log_Write_Event(DATA_LAND_COMPLETE);
} else {
Log_Write_Event(DATA_NOT_LANDED);
}
ap.land_complete = b;
// trigger disarm-on-land if configured
bool disarm_on_land_configured = (g.throttle_behavior & THR_BEHAVE_DISARM_ON_LAND_DETECT) != 0;
bool mode_disarms_on_land = mode_allows_arming(control_mode,false) && !mode_has_manual_throttle(control_mode);
if (ap.land_complete && motors.armed() && disarm_on_land_configured && mode_disarms_on_land) {
init_disarm_motors();
}
}
// arm_checks - perform final checks before arming
// always called just before arming. Return true if ok to arm
// has side-effect that logging is started
bool Copter::arm_checks(bool display_failure, bool arming_from_gcs)
{
#if LOGGING_ENABLED == ENABLED
// start dataflash
start_logging();
#endif
// check accels and gyro are healthy
if ((g.arming_check == ARMING_CHECK_ALL) || (g.arming_check & ARMING_CHECK_INS)) {
//check if accelerometers have calibrated and require reboot
if (ins.accel_cal_requires_reboot()) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL, "PreArm: Accelerometers calibrated requires reboot");
}
return false;
}
if (!ins.get_accel_health_all()) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Accelerometers not healthy");
}
return false;
}
if (!ins.get_gyro_health_all()) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Gyros not healthy");
}
return false;
}
// get ekf attitude (if bad, it's usually the gyro biases)
if (!pre_arm_ekf_attitude_check()) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: gyros still settling");
}
return false;
}
}
// always check if inertial nav has started and is ready
if (!ahrs.healthy()) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Waiting for Nav Checks");
}
return false;
}
if (compass.is_calibrating()) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Compass calibration running");
}
return false;
}
//check if compass has calibrated and requires reboot
if (compass.compass_cal_requires_reboot()) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL, "PreArm: Compass calibrated requires reboot");
}
return false;
}
// always check if the current mode allows arming
if (!mode_allows_arming(control_mode, arming_from_gcs)) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Mode not armable");
}
return false;
}
// always check gps
if (!pre_arm_gps_checks(display_failure)) {
return false;
}
// if we are using motor interlock switch and it's enabled, fail to arm
// skip check in Throw mode which takes control of the motor interlock
if (ap.using_interlock && motors.get_interlock()) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Motor Interlock Enabled");
return false;
}
// if we are not using Emergency Stop switch option, force Estop false to ensure motors
// can run normally
if (!check_if_auxsw_mode_used(AUXSW_MOTOR_ESTOP)){
set_motor_emergency_stop(false);
// if we are using motor Estop switch, it must not be in Estop position
} else if (check_if_auxsw_mode_used(AUXSW_MOTOR_ESTOP) && ap.motor_emergency_stop){
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Motor Emergency Stopped");
return false;
}
// succeed if arming checks are disabled
if (g.arming_check == ARMING_CHECK_NONE) {
return true;
}
// baro checks
if ((g.arming_check == ARMING_CHECK_ALL) || (g.arming_check & ARMING_CHECK_BARO)) {
// baro health check
if (!barometer.all_healthy()) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Barometer not healthy");
}
return false;
}
// Check baro & inav alt are within 1m if EKF is operating in an absolute position mode.
// Do not check if intending to operate in a ground relative height mode as EKF will output a ground relative height
// that may differ from the baro height due to baro drift.
nav_filter_status filt_status = inertial_nav.get_filter_status();
bool using_baro_ref = (!filt_status.flags.pred_horiz_pos_rel && filt_status.flags.pred_horiz_pos_abs);
if (using_baro_ref && (fabsf(inertial_nav.get_altitude() - baro_alt) > PREARM_MAX_ALT_DISPARITY_CM)) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Altitude disparity");
}
return false;
}
}
#if AC_FENCE == ENABLED
// check vehicle is within fence
if (!fence.pre_arm_check()) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: check fence");
}
return false;
}
#endif
// check lean angle
if ((g.arming_check == ARMING_CHECK_ALL) || (g.arming_check & ARMING_CHECK_INS)) {
if (degrees(acosf(ahrs.cos_roll()*ahrs.cos_pitch()))*100.0f > aparm.angle_max) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Leaning");
}
return false;
}
}
// check battery voltage
if ((g.arming_check == ARMING_CHECK_ALL) || (g.arming_check & ARMING_CHECK_VOLTAGE)) {
if (failsafe.battery || (!ap.usb_connected && battery.exhausted(g.fs_batt_voltage, g.fs_batt_mah))) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Check Battery");
}
return false;
}
}
// check for missing terrain data
if ((g.arming_check == ARMING_CHECK_ALL) || (g.arming_check & ARMING_CHECK_PARAMETERS)) {
if (!pre_arm_terrain_check(display_failure)) {
return false;
}
}
// check adsb
if ((g.arming_check == ARMING_CHECK_ALL) || (g.arming_check & ARMING_CHECK_PARAMETERS)) {
if (failsafe.adsb) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"PreArm: ADSB threat detected");
}
return false;
}
}
// check throttle
if ((g.arming_check == ARMING_CHECK_ALL) || (g.arming_check & ARMING_CHECK_RC)) {
// check throttle is not too low - must be above failsafe throttle
if (g.failsafe_throttle != FS_THR_DISABLED && channel_throttle->get_radio_in() < g.failsafe_throttle_value) {
if (display_failure) {
#if FRAME_CONFIG == HELI_FRAME
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Collective below Failsafe");
#else
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Throttle below Failsafe");
#endif
}
return false;
}
// check throttle is not too high - skips checks if arming from GCS in Guided
if (!(arming_from_gcs && (control_mode == GUIDED || control_mode == GUIDED_NOGPS))) {
// above top of deadband is too always high
if (get_pilot_desired_climb_rate(channel_throttle->get_control_in()) > 0.0f) {
if (display_failure) {
#if FRAME_CONFIG == HELI_FRAME
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Collective too high");
#else
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Throttle too high");
#endif
}
return false;
}
// in manual modes throttle must be at zero
if ((mode_has_manual_throttle(control_mode) || control_mode == DRIFT) && channel_throttle->get_control_in() > 0) {
if (display_failure) {
#if FRAME_CONFIG == HELI_FRAME
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Collective too high");
#else
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Throttle too high");
#endif
}
return false;
}
}
}
// check if safety switch has been pushed
if (hal.util->safety_switch_state() == AP_HAL::Util::SAFETY_DISARMED) {
if (display_failure) {
gcs_send_text(MAV_SEVERITY_CRITICAL,"Arm: Safety Switch");
}
return false;
}
// if we've gotten this far all is ok
return true;
}
// arm_checks - perform final checks before arming
// always called just before arming. Return true if ok to arm
// has side-effect that logging is started
bool Copter::arm_checks(bool display_failure, bool arming_from_gcs)
{
#if LOGGING_ENABLED == ENABLED
// start dataflash
start_logging();
#endif
// check accels and gyro are healthy
if ((g.arming_check == ARMING_CHECK_ALL) || (g.arming_check & ARMING_CHECK_INS)) {
if(!ins.get_accel_health_all()) {
if (display_failure) {
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Accelerometers not healthy"));
}
return false;
}
if(!ins.get_gyro_health_all()) {
if (display_failure) {
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Gyros not healthy"));
}
return false;
}
// get ekf attitude (if bad, it's usually the gyro biases)
if (!pre_arm_ekf_attitude_check()) {
if (display_failure) {
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: gyros still settling"));
}
return false;
}
}
// always check if inertial nav has started and is ready
if(!ahrs.healthy()) {
if (display_failure) {
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Waiting for Nav Checks Arm"));
}
return false;
}
if(compass.is_calibrating()) {
if (display_failure) {
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Compass calibration running"));
}
return false;
}
// always check if the current mode allows arming
if (!mode_allows_arming(control_mode, arming_from_gcs)) {
if (display_failure) {
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Mode not armable"));
}
return false;
}
// always check gps
if (!pre_arm_gps_checks(display_failure)) {
return false;
}
// heli specific arming check
#if FRAME_CONFIG == HELI_FRAME
// check if rotor is spinning on heli because this could disrupt gyro calibration
if (!motors.allow_arming()){
if (display_failure) {
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Rotor is Spinning")); }
return false;
}
#endif // HELI_FRAME
// succeed if arming checks are disabled
if (g.arming_check == ARMING_CHECK_NONE) {
return true;
}
// baro checks
if ((g.arming_check == ARMING_CHECK_ALL) || (g.arming_check & ARMING_CHECK_BARO)) {
// baro health check
if (!barometer.all_healthy()) {
if (display_failure) {
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Barometer not healthy"));
}
return false;
}
// Check baro & inav alt are within 1m if EKF is operating in an absolute position mode.
// Do not check if intending to operate in a ground relative height mode as EKF will output a ground relative height
// that may differ from the baro height due to baro drift.
nav_filter_status filt_status = inertial_nav.get_filter_status();
bool using_baro_ref = (!filt_status.flags.pred_horiz_pos_rel && filt_status.flags.pred_horiz_pos_abs);
if (using_baro_ref && (fabsf(inertial_nav.get_altitude() - baro_alt) > PREARM_MAX_ALT_DISPARITY_CM)) {
if (display_failure) {
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Altitude disparity"));
}
return false;
}
}
#if AC_FENCE == ENABLED
// check vehicle is within fence
if(!fence.pre_arm_check()) {
if (display_failure) {
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: check fence"));
}
return false;
}
#endif
// check lean angle
if ((g.arming_check == ARMING_CHECK_ALL) || (g.arming_check & ARMING_CHECK_INS)) {
if (degrees(acosf(ahrs.cos_roll()*ahrs.cos_pitch()))*100.0f > aparm.angle_max) {
if (display_failure) {
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Leaning"));
}
return false;
}
}
// check battery voltage
if ((g.arming_check == ARMING_CHECK_ALL) || (g.arming_check & ARMING_CHECK_VOLTAGE)) {
if (failsafe.battery || (!ap.usb_connected && battery.exhausted(g.fs_batt_voltage, g.fs_batt_mah))) {
if (display_failure) {
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Check Battery"));
}
return false;
}
}
// check throttle
if ((g.arming_check == ARMING_CHECK_ALL) || (g.arming_check & ARMING_CHECK_RC)) {
// check throttle is not too low - must be above failsafe throttle
if (g.failsafe_throttle != FS_THR_DISABLED && channel_throttle->radio_in < g.failsafe_throttle_value) {
if (display_failure) {
#if FRAME_CONFIG == HELI_FRAME
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Collective below Failsafe"));
#else
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Throttle below Failsafe"));
#endif
}
return false;
}
// check throttle is not too high - skips checks if arming from GCS in Guided
if (!(arming_from_gcs && control_mode == GUIDED)) {
// above top of deadband is too always high
if (channel_throttle->control_in > get_takeoff_trigger_throttle()) {
if (display_failure) {
#if FRAME_CONFIG == HELI_FRAME
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Collective too high"));
#else
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Throttle too high"));
#endif
}
return false;
}
// in manual modes throttle must be at zero
if ((mode_has_manual_throttle(control_mode) || control_mode == DRIFT) && channel_throttle->control_in > 0) {
if (display_failure) {
#if FRAME_CONFIG == HELI_FRAME
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Collective too high"));
#else
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Throttle too high"));
#endif
}
return false;
}
}
}
// check if safety switch has been pushed
if (hal.util->safety_switch_state() == AP_HAL::Util::SAFETY_DISARMED) {
if (display_failure) {
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("Arm: Safety Switch"));
}
return false;
}
// if we've gotten this far all is ok
return true;
}
// update_land_detector - checks if we have landed and updates the ap.land_complete flag
// called at MAIN_LOOP_RATE
void Copter::update_land_detector()
{
// land detector can not use the following sensors because they are unreliable during landing
// barometer altitude : ground effect can cause errors larger than 4m
// EKF vertical velocity or altitude : poor barometer and large acceleration from ground impact
// earth frame angle or angle error : landing on an uneven surface will force the airframe to match the ground angle
// gyro output : on uneven surface the airframe may rock back an forth after landing
// range finder : tend to be problematic at very short distances
// input throttle : in slow land the input throttle may be only slightly less than hover
if (!motors.armed()) {
// if disarmed, always landed.
set_land_complete(true);
} else if (ap.land_complete) {
#if FRAME_CONFIG == HELI_FRAME
// if rotor speed and collective pitch are high then clear landing flag
if (motors.get_throttle() > get_non_takeoff_throttle() && !motors.limit.throttle_lower && motors.rotor_runup_complete()) {
#else
// if throttle output is high then clear landing flag
if (motors.get_throttle() > get_non_takeoff_throttle()) {
#endif
set_land_complete(false);
}
} else {
#if FRAME_CONFIG == HELI_FRAME
// check that collective pitch is on lower limit (should be constrained by LAND_COL_MIN)
bool motor_at_lower_limit = motors.limit.throttle_lower;
#else
// check that the average throttle output is near minimum (less than 12.5% hover throttle)
bool motor_at_lower_limit = motors.limit.throttle_lower && attitude_control.is_throttle_mix_min();
#endif
// check that the airframe is not accelerating (not falling or breaking after fast forward flight)
bool accel_stationary = (land_accel_ef_filter.get().length() <= LAND_DETECTOR_ACCEL_MAX);
// check that vertical speed is within 1m/s of zero
bool descent_rate_low = fabsf(inertial_nav.get_velocity_z()) < 100;
// if we have a healthy rangefinder only allow landing detection below 2 meters
bool rangefinder_check = (!rangefinder_alt_ok() || rangefinder_state.alt_cm_filt.get() < LAND_RANGEFINDER_MIN_ALT_CM);
if (motor_at_lower_limit && accel_stationary && descent_rate_low && rangefinder_check) {
// landed criteria met - increment the counter and check if we've triggered
if( land_detector_count < ((float)LAND_DETECTOR_TRIGGER_SEC)*scheduler.get_loop_rate_hz()) {
land_detector_count++;
} else {
set_land_complete(true);
}
} else {
// we've sensed movement up or down so reset land_detector
land_detector_count = 0;
}
}
set_land_complete_maybe(ap.land_complete || (land_detector_count >= LAND_DETECTOR_MAYBE_TRIGGER_SEC*scheduler.get_loop_rate_hz()));
}
// set land_complete flag and disarm motors if disarm-on-land is configured
void Copter::set_land_complete(bool b)
{
// if no change, exit immediately
if( ap.land_complete == b )
return;
land_detector_count = 0;
if(b){
Log_Write_Event(DATA_LAND_COMPLETE);
} else {
Log_Write_Event(DATA_NOT_LANDED);
}
ap.land_complete = b;
// trigger disarm-on-land if configured
bool disarm_on_land_configured = (g.throttle_behavior & THR_BEHAVE_DISARM_ON_LAND_DETECT) != 0;
bool mode_disarms_on_land = mode_allows_arming(control_mode,false) && !mode_has_manual_throttle(control_mode);
if (ap.land_complete && motors.armed() && disarm_on_land_configured && mode_disarms_on_land) {
init_disarm_motors();
}
}
// set land complete maybe flag
void Copter::set_land_complete_maybe(bool b)
{
// if no change, exit immediately
if (ap.land_complete_maybe == b)
return;
if (b) {
Log_Write_Event(DATA_LAND_COMPLETE_MAYBE);
}
ap.land_complete_maybe = b;
}
// update_throttle_thr_mix - sets motors throttle_low_comp value depending upon vehicle state
// low values favour pilot/autopilot throttle over attitude control, high values favour attitude control over throttle
// has no effect when throttle is above hover throttle
void Copter::update_throttle_thr_mix()
{
#if FRAME_CONFIG != HELI_FRAME
// if disarmed or landed prioritise throttle
if(!motors.armed() || ap.land_complete) {
attitude_control.set_throttle_mix_min();
return;
}
if (mode_has_manual_throttle(control_mode)) {
// manual throttle
if(channel_throttle->get_control_in() <= 0) {
attitude_control.set_throttle_mix_min();
} else {
attitude_control.set_throttle_mix_mid();
}
} else {
// autopilot controlled throttle
// check for aggressive flight requests - requested roll or pitch angle below 15 degrees
const Vector3f angle_target = attitude_control.get_att_target_euler_cd();
bool large_angle_request = (norm(angle_target.x, angle_target.y) > LAND_CHECK_LARGE_ANGLE_CD);
// check for large external disturbance - angle error over 30 degrees
const float angle_error = attitude_control.get_att_error_angle_deg();
bool large_angle_error = (angle_error > LAND_CHECK_ANGLE_ERROR_DEG);
// check for large acceleration - falling or high turbulence
Vector3f accel_ef = ahrs.get_accel_ef_blended();
accel_ef.z += GRAVITY_MSS;
bool accel_moving = (accel_ef.length() > LAND_CHECK_ACCEL_MOVING);
// check for requested decent
bool descent_not_demanded = pos_control.get_desired_velocity().z >= 0.0f;
if ( large_angle_request || large_angle_error || accel_moving || descent_not_demanded) {
attitude_control.set_throttle_mix_max();
} else {
attitude_control.set_throttle_mix_min();
}
}
#endif
}