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/**
 * @file FixedwingLandDetector.cpp
 *
 * @author Johan Jansen <jnsn.johan@gmail.com>
 * @author Lorenz Meier <lorenz@px4.io>
 * @author Julian Oes <julian@oes.ch>
 */

#include "FixedwingLandDetector.h"

namespace land_detector
{

FixedwingLandDetector::FixedwingLandDetector()
{
	// Use Trigger time when transitioning from in-air (false) to landed (true) / ground contact (true).
	_landed_hysteresis.set_hysteresis_time_from(false, LANDED_TRIGGER_TIME_US);
	_landed_hysteresis.set_hysteresis_time_from(true, FLYING_TRIGGER_TIME_US);
}

bool FixedwingLandDetector::_get_landed_state()
{
	// Only trigger flight conditions if we are armed.
	if (!_armed) {
		return true;
	}

	bool landDetected = false;

	if (hrt_elapsed_time(&_vehicle_local_position.timestamp) < 1_s) {

		// Horizontal velocity complimentary filter.
		float val = 0.97f * _velocity_xy_filtered + 0.03f * sqrtf(_vehicle_local_position.vx * _vehicle_local_position.vx +
				_vehicle_local_position.vy * _vehicle_local_position.vy);

		if (PX4_ISFINITE(val)) {
			_velocity_xy_filtered = val;
		}

		// Vertical velocity complimentary filter.
		val = 0.99f * _velocity_z_filtered + 0.01f * fabsf(_vehicle_local_position.vz);

		if (PX4_ISFINITE(val)) {
			_velocity_z_filtered = val;
		}

		airspeed_validated_s airspeed_validated{};
		_airspeed_validated_sub.copy(&airspeed_validated);

		// set _airspeed_filtered to 0 if airspeed data is invalid
		if (!PX4_ISFINITE(airspeed_validated.true_airspeed_m_s) || hrt_elapsed_time(&airspeed_validated.timestamp) > 1_s) {
			_airspeed_filtered = 0.0f;

		} else {
			_airspeed_filtered = 0.95f * _airspeed_filtered + 0.05f * airspeed_validated.true_airspeed_m_s;
		}

		// A leaking lowpass prevents biases from building up, but
		// gives a mostly correct response for short impulses.
		const float acc_hor = matrix::Vector2f(_acceleration).norm();
		_xy_accel_filtered = _xy_accel_filtered * 0.8f + acc_hor * 0.18f;

		// Crude land detector for fixedwing.
		landDetected = _airspeed_filtered       < _param_lndfw_airspd.get()
			       && _velocity_xy_filtered < _param_lndfw_vel_xy_max.get()
			       && _velocity_z_filtered  < _param_lndfw_vel_z_max.get()
			       && _xy_accel_filtered    < _param_lndfw_xyaccel_max.get();

	} else {
		// Control state topic has timed out and we need to assume we're landed.
		landDetected = true;
	}

	return landDetected;
}

} // namespace land_detector