added param to disable str input for mekf
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@ -180,7 +180,8 @@ void AcsController::performAttitudeControl() {
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mode, &susDataProcessed, &mgmDataProcessed, &gyrDataProcessed, &sensorValues,
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&attitudeEstimationData, timeDelta, &fusedRotRateSourcesData, &fusedRotRateData);
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result = navigation.useMekf(&sensorValues, &gyrDataProcessed, &mgmDataProcessed,
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&susDataProcessed, timeDelta, &attitudeEstimationData);
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&susDataProcessed, timeDelta, &attitudeEstimationData,
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acsParameters.kalmanFilterParameters.allowStr);
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if (result != MultiplicativeKalmanFilter::MEKF_RUNNING and
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result != MultiplicativeKalmanFilter::MEKF_INITIALIZED) {
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@ -734,6 +734,9 @@ ReturnValue_t AcsParameters::getParameter(uint8_t domainId, uint8_t parameterId,
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case 0x5:
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parameterWrapper->set(kalmanFilterParameters.sensorNoiseGyrBs);
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break;
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case 0x6:
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parameterWrapper->set(kalmanFilterParameters.allowStr);
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break;
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default:
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return INVALID_IDENTIFIER_ID;
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}
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@ -947,6 +947,8 @@ class AcsParameters : public HasParametersIF {
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double sensorNoiseGyrArw = 3. * 0.0043 / sqrt(10) * DEG2RAD; // Angular Random Walk
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double sensorNoiseGyrBs = 3. / 3600. * DEG2RAD; // Bias Stability
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uint8_t allowStr = false;
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} kalmanFilterParameters;
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struct MagnetorquerParameter {
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@ -626,11 +626,11 @@ void MultiplicativeKalmanFilter::updateDataSet(
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}
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}
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void MultiplicativeKalmanFilter::setStrData(double qX, double qY, double qZ, double qW,
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bool valid) {
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void MultiplicativeKalmanFilter::setStrData(double qX, double qY, double qZ, double qW, bool valid,
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bool allowStr) {
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strData.strQuat.value[0] = qX;
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strData.strQuat.value[1] = qY;
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strData.strQuat.value[2] = qZ;
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strData.strQuat.value[3] = qW;
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strData.strQuat.valid = valid;
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strData.strQuat.valid = (valid and allowStr);
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}
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@ -38,7 +38,7 @@ class MultiplicativeKalmanFilter {
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void updateStandardDeviations(const AcsParameters *acsParameters);
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void setStrData(const double qX, const double qY, const double qZ, const double qW,
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const bool valid);
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const bool valid, const bool allowStr);
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static constexpr uint8_t IF_MEKF_ID = CLASS_ID::ACS_MEKF;
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static constexpr ReturnValue_t MEKF_UNINITIALIZED = returnvalue::makeCode(IF_MEKF_ID, 2);
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@ -9,11 +9,12 @@ ReturnValue_t Navigation::useMekf(const ACS::SensorValues *sensorValues,
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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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acsctrl::AttitudeEstimationData *attitudeEstimationData) {
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acsctrl::AttitudeEstimationData *attitudeEstimationData,
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const bool allowStr) {
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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());
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sensorValues->strSet.caliQx.isValid(), allowStr);
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if (mekfStatus == MultiplicativeKalmanFilter::MEKF_UNINITIALIZED) {
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mekfStatus = multiplicativeKalmanFilter.init(susDataProcessed, mgmDataProcessed,
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@ -17,7 +17,8 @@ class Navigation {
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const acsctrl::GyrDataProcessed *gyrDataProcessed,
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const acsctrl::MgmDataProcessed *mgmDataProcessed,
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const acsctrl::SusDataProcessed *susDataProcessed, const double timeDelta,
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acsctrl::AttitudeEstimationData *attitudeEstimationData);
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acsctrl::AttitudeEstimationData *attitudeEstimationData,
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const bool allowStr);
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void resetMekf(acsctrl::AttitudeEstimationData *mekfData);
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ReturnValue_t useSpg4(timeval now, acsctrl::GpsDataProcessed *gpsDataProcessed);
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