2022-09-20 14:15:55 +02:00
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#include "Navigation.h"
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2022-10-12 10:28:44 +02:00
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2024-02-27 16:05:05 +01:00
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Navigation::Navigation(AcsParameters *acsParameters) : multiplicativeKalmanFilter(acsParameters) {}
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2022-09-20 14:15:55 +02:00
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2022-10-12 10:28:44 +02:00
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Navigation::~Navigation() {}
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2024-02-27 16:05:05 +01:00
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ReturnValue_t Navigation::useMekf(const ACS::SensorValues *sensorValues,
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const acsctrl::GyrDataProcessed *gyrDataProcessed,
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const acsctrl::MgmDataProcessed *mgmDataProcessed,
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const acsctrl::SusDataProcessed *susDataProcessed,
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const double timeDelta,
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2024-03-15 13:16:38 +01:00
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acsctrl::AttitudeEstimationData *attitudeEstimationData,
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const bool allowStr) {
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2024-02-27 16:05:05 +01:00
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multiplicativeKalmanFilter.setStrData(
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sensorValues->strSet.caliQx.value, sensorValues->strSet.caliQy.value,
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sensorValues->strSet.caliQz.value, sensorValues->strSet.caliQw.value,
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sensorValues->strSet.caliQx.isValid(), allowStr);
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2022-10-12 10:28:44 +02:00
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2023-02-23 11:26:43 +01:00
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if (mekfStatus == MultiplicativeKalmanFilter::MEKF_UNINITIALIZED) {
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2024-02-27 16:05:05 +01:00
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mekfStatus = multiplicativeKalmanFilter.init(susDataProcessed, mgmDataProcessed,
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gyrDataProcessed, attitudeEstimationData);
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2023-02-23 09:45:11 +01:00
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return mekfStatus;
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} else {
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mekfStatus = multiplicativeKalmanFilter.mekfEst(
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2024-02-27 16:05:05 +01:00
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susDataProcessed, mgmDataProcessed, gyrDataProcessed, timeDelta, attitudeEstimationData);
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2023-02-23 09:45:11 +01:00
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return mekfStatus;
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2022-10-12 10:28:44 +02:00
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}
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2022-09-20 14:15:55 +02:00
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}
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2023-02-21 17:09:49 +01:00
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2023-11-23 16:56:36 +01:00
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void Navigation::resetMekf(acsctrl::AttitudeEstimationData *mekfData) {
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mekfStatus = multiplicativeKalmanFilter.reset(mekfData);
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2023-02-21 17:09:49 +01:00
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}
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2023-08-07 11:23:10 +02:00
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2023-08-09 13:41:25 +02:00
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ReturnValue_t Navigation::useSpg4(timeval now, acsctrl::GpsDataProcessed *gpsDataProcessed) {
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2023-08-07 11:23:10 +02:00
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double position[3] = {0, 0, 0};
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double velocity[3] = {0, 0, 0};
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ReturnValue_t result = sgp4Propagator.propagate(position, velocity, now, 0);
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if (result == returnvalue::OK) {
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{
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PoolReadGuard pg(gpsDataProcessed);
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if (pg.getReadResult() == returnvalue::OK) {
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2023-11-27 10:37:40 +01:00
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gpsDataProcessed->source = acs::gps::Source::SPG4;
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gpsDataProcessed->source.setValid(true);
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2023-08-07 11:23:10 +02:00
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std::memcpy(gpsDataProcessed->gpsPosition.value, position, 3 * sizeof(double));
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gpsDataProcessed->gpsPosition.setValid(true);
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std::memcpy(gpsDataProcessed->gpsVelocity.value, velocity, 3 * sizeof(double));
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gpsDataProcessed->gpsVelocity.setValid(true);
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}
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}
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} else {
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{
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PoolReadGuard pg(gpsDataProcessed);
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if (pg.getReadResult() == returnvalue::OK) {
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2023-11-27 10:37:40 +01:00
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gpsDataProcessed->source = acs::gps::Source::NONE;
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gpsDataProcessed->source.setValid(true);
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2023-08-07 11:23:10 +02:00
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std::memcpy(gpsDataProcessed->gpsPosition.value, position, 3 * sizeof(double));
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gpsDataProcessed->gpsPosition.setValid(false);
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std::memcpy(gpsDataProcessed->gpsVelocity.value, velocity, 3 * sizeof(double));
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gpsDataProcessed->gpsVelocity.setValid(false);
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}
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}
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}
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2023-08-09 13:41:25 +02:00
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return result;
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2023-08-07 11:23:10 +02:00
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}
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ReturnValue_t Navigation::updateTle(const uint8_t *line1, const uint8_t *line2) {
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return sgp4Propagator.initialize(line1, line2);
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}
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2024-02-27 16:05:05 +01:00
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void Navigation::updateMekfStandardDeviations(const AcsParameters *acsParameters) {
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multiplicativeKalmanFilter.updateStandardDeviations(acsParameters);
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}
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