forked from Archive/PX4-Autopilot
multicopter land detector: make threshold for _has_low_thrust
configurable Signed-off-by: Roman <bapstroman@gmail.com>
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@ -82,6 +82,7 @@ MulticopterLandDetector::MulticopterLandDetector()
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_paramHandle.freefall_trigger_time = param_find("LNDMC_FFALL_TTRI");
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_paramHandle.altitude_max = param_find("LNDMC_ALT_MAX");
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_paramHandle.landSpeed = param_find("MPC_LAND_SPEED");
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_paramHandle.low_thrust_threshold = param_find("LNDMC_LOW_T_THR");
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// Use Trigger time when transitioning from in-air (false) to landed (true) / ground contact (true).
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_landed_hysteresis.set_hysteresis_time_from(false, LAND_DETECTOR_TRIGGER_TIME_US);
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@ -126,6 +127,8 @@ void MulticopterLandDetector::_update_params()
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_freefall_hysteresis.set_hysteresis_time_from(false, (hrt_abstime)(1e6f * _params.freefall_trigger_time));
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param_get(_paramHandle.altitude_max, &_params.altitude_max);
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param_get(_paramHandle.landSpeed, &_params.landSpeed);
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param_get(_paramHandle.low_thrust_threshold, &_params.low_thrust_threshold);
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}
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@ -314,7 +317,8 @@ bool MulticopterLandDetector::_is_climb_rate_enabled()
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bool MulticopterLandDetector::_has_low_thrust()
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{
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// 30% of throttle range between min and hover
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float sys_min_throttle = _params.minThrottle + (_params.hoverThrottle - _params.minThrottle) * 0.3f;
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float sys_min_throttle = _params.minThrottle + (_params.hoverThrottle - _params.minThrottle) *
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_params.low_thrust_threshold;
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// Check if thrust output is less than the minimum auto throttle param.
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return _actuators.control[actuator_controls_s::INDEX_THROTTLE] <= sys_min_throttle;
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@ -107,6 +107,7 @@ private:
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param_t freefall_trigger_time;
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param_t altitude_max;
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param_t landSpeed;
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param_t low_thrust_threshold;
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} _paramHandle{};
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struct {
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@ -120,6 +121,7 @@ private:
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float freefall_trigger_time;
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float altitude_max;
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float landSpeed;
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float low_thrust_threshold;
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} _params{};
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int _vehicleLocalPositionSub{ -1};
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@ -113,3 +113,21 @@ PARAM_DEFINE_FLOAT(LNDMC_FFALL_TTRI, 0.3);
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*
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*/
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PARAM_DEFINE_FLOAT(LNDMC_ALT_MAX, -1.0f);
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/**
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* Low throttle detection threshold.
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*
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* Defines the commanded throttle value below which the land detector
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* considers the vehicle to have "low thrust". This is one condition that
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* is used to detect the ground contact state. The value is calculated as
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* val = (MPC_THR_HOVER - MPC_THR_MIN) * LNDMC_LOW_T_THR + MPC_THR_MIN
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* Increase this value if the system takes long time to detect landing.
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*
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* @unit norm
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* @min 0.1
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* @max 0.9
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* @decimal 2
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* @group Land Detector
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*
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*/
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PARAM_DEFINE_FLOAT(LNDMC_LOW_T_THR, 0.3);
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