Once upon a time Robin was made happy #800
@ -122,26 +122,6 @@ void AcsController::performControlOperation() {
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}
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}
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timeval timeAbsolute;
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Clock::getClock_timeval(&timeAbsolute);
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timeval timeRelative;
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Clock::getClockMonotonic(&timeRelative);
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ReturnValue_t result = navigation.useSpg4(timeAbsolute, &gpsDataProcessed);
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if (result == Sgp4Propagator::TLE_TOO_OLD and not tleTooOldFlag) {
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triggerEvent(acs::TLE_TOO_OLD);
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tleTooOldFlag = true;
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} else if (result != Sgp4Propagator::TLE_TOO_OLD) {
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tleTooOldFlag = false;
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}
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sensorProcessing.process(now, &sensorValues, &mgmDataProcessed, &susDataProcessed,
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&gyrDataProcessed, &gpsDataProcessed, &acsParameters);
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fusedRotationEstimation.estimateFusedRotationRateSafe(&susDataProcessed, &mgmDataProcessed,
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&gyrDataProcessed, &fusedRotRateData);
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result = navigation.useMekf(&sensorValues, &gyrDataProcessed, &mgmDataProcessed,
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&susDataProcessed, &mekfData, &acsParameters);
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switch (internalState) {
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case InternalState::STARTUP: {
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initialCountdown.resetTimer();
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@ -156,25 +136,7 @@ void AcsController::performControlOperation() {
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}
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case InternalState::READY: {
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if (mode != MODE_OFF) {
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switch (mode) {
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case acs::SAFE:
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switch (submode) {
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case SUBMODE_NONE:
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performSafe();
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break;
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case acs::DETUMBLE:
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performDetumble();
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break;
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}
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break;
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case acs::PTG_IDLE:
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case acs::PTG_TARGET:
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case acs::PTG_TARGET_GS:
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case acs::PTG_NADIR:
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case acs::PTG_INERTIAL:
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performPointingCtrl();
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break;
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}
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performAttitudeControl();
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}
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break;
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}
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@ -183,23 +145,29 @@ void AcsController::performControlOperation() {
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}
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}
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void AcsController::performSafe() {
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timeval now;
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Clock::getClock_timeval(&now);
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void AcsController::performAttitudeControl() {
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timeval timeAbsolute;
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Clock::getClock_timeval(&timeAbsolute);
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timeval timeRelative;
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Clock::getClockMonotonic(&timeRelative);
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ReturnValue_t result = navigation.useSpg4(now, &gpsDataProcessed);
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ReturnValue_t result = navigation.useSpg4(timeAbsolute, &gpsDataProcessed);
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if (result == Sgp4Propagator::TLE_TOO_OLD and not tleTooOldFlag) {
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triggerEvent(acs::TLE_TOO_OLD);
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tleTooOldFlag = true;
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} else if (result != Sgp4Propagator::TLE_TOO_OLD) {
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tleTooOldFlag = false;
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}
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sensorProcessing.process(now, &sensorValues, &mgmDataProcessed, &susDataProcessed,
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&gyrDataProcessed, &gpsDataProcessed, &acsParameters);
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sensorProcessing.process(timeAbsolute, timeRelative, &sensorValues, &mgmDataProcessed,
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&susDataProcessed, &gyrDataProcessed, &gpsDataProcessed, &acsParameters);
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fusedRotationEstimation.estimateFusedRotationRateSafe(&susDataProcessed, &mgmDataProcessed,
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&gyrDataProcessed, &fusedRotRateData);
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result = navigation.useMekf(&sensorValues, &gyrDataProcessed, &mgmDataProcessed,
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&susDataProcessed, &mekfData, &acsParameters);
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switch (mode) {
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case acs::SAFE:
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if (result != MultiplicativeKalmanFilter::MEKF_RUNNING &&
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result != MultiplicativeKalmanFilter::MEKF_INITIALIZED) {
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if (not mekfInvalidFlag) {
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@ -215,7 +183,55 @@ void AcsController::performSafe() {
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triggerEvent(acs::MEKF_RECOVERY);
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mekfInvalidFlag = false;
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}
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switch (submode) {
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case SUBMODE_NONE:
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performSafe();
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break;
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case acs::DETUMBLE:
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performDetumble();
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break;
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}
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break;
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case acs::PTG_IDLE:
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case acs::PTG_TARGET:
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case acs::PTG_TARGET_GS:
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case acs::PTG_NADIR:
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case acs::PTG_INERTIAL:
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if (result != MultiplicativeKalmanFilter::MEKF_RUNNING &&
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result != MultiplicativeKalmanFilter::MEKF_INITIALIZED) {
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mekfInvalidCounter++;
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if (not mekfInvalidFlag) {
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triggerEvent(acs::MEKF_INVALID_INFO, (uint32_t)mekfData.mekfStatus.value);
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mekfInvalidFlag = true;
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}
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if (result == MultiplicativeKalmanFilter::MEKF_NOT_FINITE && !mekfLost) {
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triggerEvent(acs::MEKF_AUTOMATIC_RESET);
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navigation.resetMekf(&mekfData);
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mekfLost = true;
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}
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if (mekfInvalidCounter > acsParameters.onBoardParams.mekfViolationTimer) {
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// Trigger this so STR FDIR can set the device faulty.
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EventManagerIF::triggerEvent(objects::STAR_TRACKER, acs::MEKF_INVALID_MODE_VIOLATION, 0,
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0);
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mekfInvalidCounter = 0;
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}
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commandActuators(0, 0, 0, acsParameters.magnetorquerParameter.torqueDuration,
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cmdSpeedRws[0], cmdSpeedRws[1], cmdSpeedRws[2], cmdSpeedRws[3],
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acsParameters.rwHandlingParameters.rampTime);
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return;
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} else {
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if (mekfInvalidFlag) {
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triggerEvent(acs::MEKF_RECOVERY);
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mekfInvalidFlag = false;
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}
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mekfInvalidCounter = 0;
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}
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performPointingCtrl();
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break;
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}
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}
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void AcsController::performSafe() {
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// get desired satellite rate, sun direction to align to and inertia
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double sunTargetDir[3] = {0, 0, 0};
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guidance.getTargetParamsSafe(sunTargetDir);
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@ -316,37 +332,6 @@ void AcsController::performSafe() {
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}
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void AcsController::performDetumble() {
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timeval now;
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Clock::getClock_timeval(&now);
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ReturnValue_t result = navigation.useSpg4(now, &gpsDataProcessed);
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if (result == Sgp4Propagator::TLE_TOO_OLD and not tleTooOldFlag) {
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triggerEvent(acs::TLE_TOO_OLD);
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tleTooOldFlag = true;
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} else {
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tleTooOldFlag = false;
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}
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sensorProcessing.process(now, &sensorValues, &mgmDataProcessed, &susDataProcessed,
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&gyrDataProcessed, &gpsDataProcessed, &acsParameters);
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fusedRotationEstimation.estimateFusedRotationRateSafe(&susDataProcessed, &mgmDataProcessed,
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&gyrDataProcessed, &fusedRotRateData);
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result = navigation.useMekf(&sensorValues, &gyrDataProcessed, &mgmDataProcessed,
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&susDataProcessed, &mekfData, &acsParameters);
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if (result != MultiplicativeKalmanFilter::MEKF_RUNNING &&
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result != MultiplicativeKalmanFilter::MEKF_INITIALIZED) {
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if (not mekfInvalidFlag) {
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triggerEvent(acs::MEKF_INVALID_INFO, (uint32_t)mekfData.mekfStatus.value);
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mekfInvalidFlag = true;
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}
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if (result == MultiplicativeKalmanFilter::MEKF_NOT_FINITE && !mekfLost) {
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triggerEvent(acs::MEKF_AUTOMATIC_RESET);
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navigation.resetMekf(&mekfData);
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mekfLost = true;
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}
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} else if (mekfInvalidFlag) {
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triggerEvent(acs::MEKF_RECOVERY);
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mekfInvalidFlag = false;
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}
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acs::SafeModeStrategy safeCtrlStrat = detumble.detumbleStrategy(
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mgmDataProcessed.mgmVecTot.isValid(), gyrDataProcessed.gyrVecTot.isValid(),
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mgmDataProcessed.mgmVecTotDerivative.isValid(),
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@ -409,51 +394,9 @@ void AcsController::performDetumble() {
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}
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void AcsController::performPointingCtrl() {
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timeval now;
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Clock::getClock_timeval(&now);
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ReturnValue_t result = navigation.useSpg4(now, &gpsDataProcessed);
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if (result == Sgp4Propagator::TLE_TOO_OLD and not tleTooOldFlag) {
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triggerEvent(acs::TLE_TOO_OLD);
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tleTooOldFlag = true;
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} else {
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tleTooOldFlag = false;
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}
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sensorProcessing.process(now, &sensorValues, &mgmDataProcessed, &susDataProcessed,
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&gyrDataProcessed, &gpsDataProcessed, &acsParameters);
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result = navigation.useMekf(&sensorValues, &gyrDataProcessed, &mgmDataProcessed,
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&susDataProcessed, &mekfData, &acsParameters);
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if (result != MultiplicativeKalmanFilter::MEKF_RUNNING &&
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result != MultiplicativeKalmanFilter::MEKF_INITIALIZED) {
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mekfInvalidCounter++;
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if (not mekfInvalidFlag) {
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triggerEvent(acs::MEKF_INVALID_INFO, (uint32_t)mekfData.mekfStatus.value);
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mekfInvalidFlag = true;
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}
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if (result == MultiplicativeKalmanFilter::MEKF_NOT_FINITE && !mekfLost) {
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triggerEvent(acs::MEKF_AUTOMATIC_RESET);
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navigation.resetMekf(&mekfData);
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mekfLost = true;
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}
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if (mekfInvalidCounter > acsParameters.onBoardParams.mekfViolationTimer) {
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// Trigger this so STR FDIR can set the device faulty.
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EventManagerIF::triggerEvent(objects::STAR_TRACKER, acs::MEKF_INVALID_MODE_VIOLATION, 0, 0);
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mekfInvalidCounter = 0;
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}
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commandActuators(0, 0, 0, acsParameters.magnetorquerParameter.torqueDuration, cmdSpeedRws[0],
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cmdSpeedRws[1], cmdSpeedRws[2], cmdSpeedRws[3],
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acsParameters.rwHandlingParameters.rampTime);
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return;
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} else {
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if (mekfInvalidFlag) {
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triggerEvent(acs::MEKF_RECOVERY);
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mekfInvalidFlag = false;
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}
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mekfInvalidCounter = 0;
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}
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uint8_t enableAntiStiction = true;
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double rwPseudoInv[4][3] = {{0, 0, 0}, {0, 0, 0}, {0, 0, 0}, {0, 0, 0}};
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result = guidance.getDistributionMatrixRw(&sensorValues, *rwPseudoInv);
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ReturnValue_t result = guidance.getDistributionMatrixRw(&sensorValues, *rwPseudoInv);
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if (result == returnvalue::FAILED) {
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if (multipleRwUnavailableCounter >=
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acsParameters.rwHandlingParameters.multipleRwInvalidTimeout) {
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@ -37,6 +37,7 @@ class AcsController : public ExtendedControllerBase, public ReceivesParameterMes
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uint16_t startAtIndex) override;
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protected:
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void performAttitudeControl();
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void performSafe();
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void performDetumble();
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void performPointingCtrl();
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Loading…
Reference in New Issue
Block a user