PX4-Autopilot/src/modules/ekf2/EKF/control.cpp

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/**
 * @file control.cpp
 * Control functions for ekf attitude and position estimator.
 *
 * @author Paul Riseborough <p_riseborough@live.com.au>
 *
 */


#include "ekf.h"
#include <mathlib/mathlib.h>

void Ekf::controlFusionModes(const imuSample &imu_delayed)
{
	// Store the status to enable change detection
	_control_status_prev.value = _control_status.value;
	_state_reset_count_prev = _state_reset_status.reset_count;

	if (_system_flag_buffer) {
		systemFlagUpdate system_flags_delayed;

		if (_system_flag_buffer->pop_first_older_than(imu_delayed.time_us, &system_flags_delayed)) {

			set_vehicle_at_rest(system_flags_delayed.at_rest);
			set_in_air_status(system_flags_delayed.in_air);

			set_is_fixed_wing(system_flags_delayed.is_fixed_wing);

			if (system_flags_delayed.gnd_effect) {
				set_gnd_effect();
			}
		}
	}

	// monitor the tilt alignment
	if (!_control_status.flags.tilt_align) {
		// whilst we are aligning the tilt, monitor the variances
		// Once the tilt variances have reduced to equivalent of 3 deg uncertainty
		// and declare the tilt alignment complete
		if (getTiltVariance() < sq(math::radians(3.f))) {
			_control_status.flags.tilt_align = true;

			// send alignment status message to the console
			const char *height_source = "unknown";

			if (_control_status.flags.baro_hgt) {
				height_source = "baro";

			} else if (_control_status.flags.ev_hgt) {
				height_source = "ev";

			} else if (_control_status.flags.gps_hgt) {
				height_source = "gps";

			} else if (_control_status.flags.rng_hgt) {
				height_source = "rng";
			}

			ECL_INFO("%llu: EKF aligned, (%s hgt, IMU buf: %i, OBS buf: %i)",
				 (unsigned long long)imu_delayed.time_us, height_source, (int)_imu_buffer_length, (int)_obs_buffer_length);

			ECL_DEBUG("tilt aligned, roll: %.3f, pitch %.3f, yaw: %.3f",
				  (double)matrix::Eulerf(_state.quat_nominal).phi(),
				  (double)matrix::Eulerf(_state.quat_nominal).theta(),
				  (double)matrix::Eulerf(_state.quat_nominal).psi()
				 );
		}
	}

#if defined(CONFIG_EKF2_MAGNETOMETER)
	// control use of observations for aiding
	controlMagFusion();
#endif // CONFIG_EKF2_MAGNETOMETER

#if defined(CONFIG_EKF2_OPTICAL_FLOW)
	controlOpticalFlowFusion(imu_delayed);
#endif // CONFIG_EKF2_OPTICAL_FLOW

#if defined(CONFIG_EKF2_GNSS)
	controlGpsFusion(imu_delayed);
#endif // CONFIG_EKF2_GNSS

#if defined(CONFIG_EKF2_AUX_GLOBAL_POSITION) && defined(MODULE_NAME)
	_aux_global_position.update(*this, imu_delayed);
#endif // CONFIG_EKF2_AUX_GLOBAL_POSITION

#if defined(CONFIG_EKF2_AIRSPEED)
	controlAirDataFusion(imu_delayed);
#endif // CONFIG_EKF2_AIRSPEED

#if defined(CONFIG_EKF2_SIDESLIP)
	controlBetaFusion(imu_delayed);
#endif // CONFIG_EKF2_SIDESLIP

#if defined(CONFIG_EKF2_DRAG_FUSION)
	controlDragFusion(imu_delayed);
#endif // CONFIG_EKF2_DRAG_FUSION

	controlHeightFusion(imu_delayed);

#if defined(CONFIG_EKF2_GRAVITY_FUSION)
	controlGravityFusion(imu_delayed);
#endif // CONFIG_EKF2_GRAVITY_FUSION

#if defined(CONFIG_EKF2_EXTERNAL_VISION)
	// Additional data odometry data from an external estimator can be fused.
	controlExternalVisionFusion();
#endif // CONFIG_EKF2_EXTERNAL_VISION

#if defined(CONFIG_EKF2_AUXVEL)
	// Additional horizontal velocity data from an auxiliary sensor can be fused
	controlAuxVelFusion();
#endif // CONFIG_EKF2_AUXVEL

	controlZeroInnovationHeadingUpdate();

	_zero_velocity_update.update(*this, imu_delayed);

	if (_params.imu_ctrl & static_cast<int32_t>(ImuCtrl::GyroBias)) {
		_zero_gyro_update.update(*this, imu_delayed);
	}

	// Fake position measurement for constraining drift when no other velocity or position measurements
	controlFakePosFusion();
	controlFakeHgtFusion();

	// check if we are no longer fusing measurements that directly constrain velocity drift
	updateDeadReckoningStatus();
}