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synced 2026-04-14 10:07:39 +08:00
Better / cleaner initialization of the attitude estimator
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0a89364e3c
commit
706d08055d
@ -4,7 +4,7 @@
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// Define EKF_DEBUG here to enable the debug print calls
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// if the macro is not set, these will be completely
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// optimized out by the compiler.
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//#define EKF_DEBUG
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#define EKF_DEBUG
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#ifdef EKF_DEBUG
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#include <stdio.h>
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@ -2263,21 +2263,29 @@ bool AttPosEKF::StatesNaN(struct ekf_status_report *err_report) {
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if (!isfinite(KH[i][j])) {
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err_report->covarianceNaN = true;
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ekf_debug("KH NaN");
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err = true;
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} // intermediate result used for covariance updates
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if (err) {
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ekf_debug("KH NaN");
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}
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if (!isfinite(KHP[i][j])) {
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err_report->covarianceNaN = true;
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ekf_debug("KHP NaN");
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err = true;
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} // intermediate result used for covariance updates
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if (err) {
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ekf_debug("KHP NaN");
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}
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if (!isfinite(P[i][j])) {
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err_report->covarianceNaN = true;
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ekf_debug("P NaN");
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err = true;
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} // covariance matrix
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if (err) {
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ekf_debug("P NaN");
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}
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}
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if (!isfinite(Kfusion[i])) {
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@ -2461,12 +2469,12 @@ void AttPosEKF::InitializeDynamic(float (&initvelNED)[3])
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summedDelVel.z = 0.0f;
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}
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void AttPosEKF::InitialiseFilter(float (&initvelNED)[3])
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void AttPosEKF::InitialiseFilter(float (&initvelNED)[3], double referenceLat, double referenceLon, float referenceHgt)
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{
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//store initial lat,long and height
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latRef = gpsLat;
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lonRef = gpsLon;
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hgtRef = gpsHgt;
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latRef = referenceLat;
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lonRef = referenceLon;
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hgtRef = referenceHgt;
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memset(&last_ekf_error, 0, sizeof(last_ekf_error));
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@ -308,7 +308,7 @@ void OnGroundCheck();
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void CovarianceInit();
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void InitialiseFilter(float (&initvelNED)[3]);
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void InitialiseFilter(float (&initvelNED)[3], double referenceLat, double referenceLon, float referenceHgt);
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float ConstrainFloat(float val, float min, float max);
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@ -606,7 +606,6 @@ FixedwingEstimator::task_main()
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/* guard against too large deltaT's */
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if (!isfinite(deltaT) || deltaT > 1.0f || deltaT < 0.000001f) {
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deltaT = 0.01f;
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warnx("TS fail");
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}
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@ -650,14 +649,14 @@ FixedwingEstimator::task_main()
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IMUmsec = _sensor_combined.timestamp / 1e3f;
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float deltaT = (_sensor_combined.timestamp - last_run) / 1e6f;
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last_run = _sensor_combined.timestamp;
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/* guard against too large deltaT's */
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if (!isfinite(deltaT) || deltaT > 1.0f || deltaT < 0.000001f) {
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deltaT = 0.01f;
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warnx("TS fail");
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}
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last_run = _sensor_combined.timestamp;
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// Always store data, independent of init status
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/* fill in last data set */
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_ekf->dtIMU = deltaT;
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@ -823,6 +822,8 @@ FixedwingEstimator::task_main()
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*/
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int check = _ekf->CheckAndBound();
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const char* ekfname = "[ekf] ";
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switch (check) {
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case 0:
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/* all ok */
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@ -830,27 +831,34 @@ FixedwingEstimator::task_main()
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case 1:
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{
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const char* str = "NaN in states, resetting";
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warnx(str);
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mavlink_log_critical(_mavlink_fd, str);
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warnx("%s%s", ekfname, str);
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mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str);
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break;
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}
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case 2:
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{
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const char* str = "stale IMU data, resetting";
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warnx(str);
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mavlink_log_critical(_mavlink_fd, str);
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warnx("%s%s", ekfname, str);
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mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str);
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break;
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}
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case 3:
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{
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const char* str = "switching dynamic / static state";
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warnx(str);
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mavlink_log_critical(_mavlink_fd, str);
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const char* str = "switching to dynamic state";
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warnx("%s%s", ekfname, str);
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mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str);
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break;
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}
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default:
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{
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const char* str = "unknown reset condition";
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warnx("%s%s", ekfname, str);
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mavlink_log_critical(_mavlink_fd, "%s%s", ekfname, str);
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}
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}
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// If non-zero, we got a problem
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// If non-zero, we got a filter reset
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if (check) {
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struct ekf_status_report ekf_report;
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@ -912,7 +920,7 @@ FixedwingEstimator::task_main()
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double lon = home.lon;
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float alt = home.alt;
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_ekf->InitialiseFilter(_ekf->velNED);
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_ekf->InitialiseFilter(_ekf->velNED, math::radians(lat), math::radians(lon) - M_PI, alt);
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// Initialize projection
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_local_pos.ref_lat = home.lat * 1e7;
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@ -942,7 +950,7 @@ FixedwingEstimator::task_main()
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_ekf->posNE[0] = _ekf->posNED[0];
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_ekf->posNE[1] = _ekf->posNED[1];
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_ekf->InitialiseFilter(_ekf->velNED);
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_ekf->InitialiseFilter(_ekf->velNED, 0.0, 0.0, 0.0f);
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}
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}
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