forked from Archive/PX4-Autopilot
land_detector: relax data timeouts uniformly
* if we're hitting these timeouts there are much larger problems in the system
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@ -66,7 +66,7 @@ bool FixedwingLandDetector::_get_landed_state()
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bool landDetected = false;
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if (hrt_elapsed_time(&_vehicle_local_position.timestamp) < 500_ms) {
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if (hrt_elapsed_time(&_vehicle_local_position.timestamp) < 1_s) {
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// Horizontal velocity complimentary filter.
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float val = 0.97f * _velocity_xy_filtered + 0.03f * sqrtf(_vehicle_local_position.vx * _vehicle_local_position.vx +
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@ -147,7 +147,6 @@ bool MulticopterLandDetector::_get_ground_contact_state()
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vertical_movement = fabsf(_vehicle_local_position.vz) > _param_lndmc_z_vel_max.get() * 2.5f;
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} else {
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// Adjust max_climb_rate if land_speed is lower than 2x max_climb_rate
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float max_climb_rate = ((land_speed_threshold * 0.5f) < _param_lndmc_z_vel_max.get()) ? (0.5f * land_speed_threshold) :
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_param_lndmc_z_vel_max.get();
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@ -171,9 +170,6 @@ bool MulticopterLandDetector::_get_ground_contact_state()
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bool MulticopterLandDetector::_get_maybe_landed_state()
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{
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// Time base for this function
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const hrt_abstime now = hrt_absolute_time();
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// When not armed, consider to be maybe-landed
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if (!_actuator_armed.armed) {
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return true;
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@ -181,7 +177,7 @@ bool MulticopterLandDetector::_get_maybe_landed_state()
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if (_has_minimal_thrust()) {
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if (_min_trust_start == 0) {
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_min_trust_start = now;
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_min_trust_start = hrt_absolute_time();
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}
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} else {
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@ -224,19 +220,15 @@ bool MulticopterLandDetector::_get_landed_state()
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// reset the landed_time
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if (!_maybe_landed_hysteresis.get_state()) {
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_landed_time = 0;
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} else if (_landed_time == 0) {
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_landed_time = hrt_absolute_time();
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}
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// if we have maybe_landed, the mc_pos_control goes into idle (thrust_sp = 0.0)
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// therefore check if all other condition of the landed state remain true
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return _maybe_landed_hysteresis.get_state();
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}
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float MulticopterLandDetector::_get_max_altitude()
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@ -265,9 +257,7 @@ float MulticopterLandDetector::_get_max_altitude()
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bool MulticopterLandDetector::_has_altitude_lock()
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{
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return _vehicle_local_position.timestamp != 0 &&
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hrt_elapsed_time(&_vehicle_local_position.timestamp) < 500_ms &&
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_vehicle_local_position.z_valid;
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return (hrt_elapsed_time(&_vehicle_local_position.timestamp) < 1_s) && _vehicle_local_position.z_valid;
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}
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bool MulticopterLandDetector::_has_position_lock()
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@ -277,8 +267,7 @@ bool MulticopterLandDetector::_has_position_lock()
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bool MulticopterLandDetector::_is_climb_rate_enabled()
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{
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bool has_updated = (_vehicle_local_position_setpoint.timestamp != 0)
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&& (hrt_elapsed_time(&_vehicle_local_position_setpoint.timestamp) < 500_ms);
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bool has_updated = (hrt_elapsed_time(&_vehicle_local_position_setpoint.timestamp) < 1_s);
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return (_vehicle_control_mode.flag_control_climb_rate_enabled && has_updated
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&& PX4_ISFINITE(_vehicle_local_position_setpoint.vz));
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@ -74,7 +74,7 @@ bool VtolLandDetector::_get_landed_state()
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bool landed = MulticopterLandDetector::_get_landed_state();
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// for vtol we additionally consider airspeed
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if (hrt_elapsed_time(&_airspeed.timestamp) < 500 * 1000 && _airspeed.confidence > 0.99f
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if (hrt_elapsed_time(&_airspeed.timestamp) < 1_s && _airspeed.confidence > 0.99f
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&& PX4_ISFINITE(_airspeed.indicated_airspeed_m_s)) {
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_airspeed_filtered = 0.95f * _airspeed_filtered + 0.05f * _airspeed.indicated_airspeed_m_s;
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