Merge pull request 'Fix Desaturation for Faulty Wheels' (#865) from fix-desaturation into main
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Reviewed-on: #865 Reviewed-by: Robin Müller <muellerr@irs.uni-stuttgart.de>
This commit is contained in:
commit
f6e99f171a
@ -29,6 +29,7 @@ will consitute of a breaking change warranting a new major release:
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- The `PTG_CTRL_NO_ATTITUDE_INFORMATION` will now actually trigger a fallback into safe mode
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and is triggered by the `AcsController` now.
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- Fixed a corner case, in which an invalid speed command could be sent to the `RwHandler`.
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- Fixed calculation of desaturation torque for faulty RWs.
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## Changed
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@ -42,6 +43,7 @@ will consitute of a breaking change warranting a new major release:
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also limits the rotation for the reference target quaternion to prevent spikes in required
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rotation rates.
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- Updated QUEST and Sun Vector Params to new values.
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- Removed the satellites's angular momentum from desaturation calculation.
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## Added
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@ -396,7 +396,7 @@ void AcsController::performPointingCtrl() {
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bool allRwAvailable = 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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ReturnValue_t result = guidance.getDistributionMatrixRw(&sensorValues, *rwPseudoInv);
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ReturnValue_t result = guidance.getDistributionMatrixRw(&sensorValues, *rwPseudoInv, &rwAvail);
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if (result == acsctrl::MULTIPLE_RW_UNAVAILABLE) {
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if (multipleRwUnavailableCounter >=
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acsParameters.rwHandlingParameters.multipleRwInvalidTimeout) {
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@ -433,10 +433,10 @@ void AcsController::performPointingCtrl() {
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VectorOperations<double>::add(torquePtgRws, rwTrqNs, torqueRws, 4);
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actuatorCmd.scalingTorqueRws(torqueRws, acsParameters.rwHandlingParameters.maxTrq);
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ptgCtrl.ptgDesaturation(
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&acsParameters.idleModeControllerParameters, mgmDataProcessed.mgmVecTot.value,
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mgmDataProcessed.mgmVecTot.isValid(), rotRateB, sensorValues.rw1Set.currSpeed.value,
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sensorValues.rw2Set.currSpeed.value, sensorValues.rw3Set.currSpeed.value,
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sensorValues.rw4Set.currSpeed.value, mgtDpDes);
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allRwAvailable, &rwAvail, &acsParameters.idleModeControllerParameters,
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mgmDataProcessed.mgmVecTot.value, mgmDataProcessed.mgmVecTot.isValid(),
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sensorValues.rw1Set.currSpeed.value, sensorValues.rw2Set.currSpeed.value,
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sensorValues.rw3Set.currSpeed.value, sensorValues.rw4Set.currSpeed.value, mgtDpDes);
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break;
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case acs::PTG_TARGET:
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@ -456,10 +456,10 @@ void AcsController::performPointingCtrl() {
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VectorOperations<double>::add(torquePtgRws, rwTrqNs, torqueRws, 4);
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actuatorCmd.scalingTorqueRws(torqueRws, acsParameters.rwHandlingParameters.maxTrq);
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ptgCtrl.ptgDesaturation(
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&acsParameters.targetModeControllerParameters, mgmDataProcessed.mgmVecTot.value,
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mgmDataProcessed.mgmVecTot.isValid(), rotRateB, sensorValues.rw1Set.currSpeed.value,
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sensorValues.rw2Set.currSpeed.value, sensorValues.rw3Set.currSpeed.value,
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sensorValues.rw4Set.currSpeed.value, mgtDpDes);
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allRwAvailable, &rwAvail, &acsParameters.targetModeControllerParameters,
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mgmDataProcessed.mgmVecTot.value, mgmDataProcessed.mgmVecTot.isValid(),
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sensorValues.rw1Set.currSpeed.value, sensorValues.rw2Set.currSpeed.value,
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sensorValues.rw3Set.currSpeed.value, sensorValues.rw4Set.currSpeed.value, mgtDpDes);
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break;
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case acs::PTG_TARGET_GS:
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@ -476,10 +476,10 @@ void AcsController::performPointingCtrl() {
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VectorOperations<double>::add(torquePtgRws, rwTrqNs, torqueRws, 4);
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actuatorCmd.scalingTorqueRws(torqueRws, acsParameters.rwHandlingParameters.maxTrq);
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ptgCtrl.ptgDesaturation(
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&acsParameters.gsTargetModeControllerParameters, mgmDataProcessed.mgmVecTot.value,
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mgmDataProcessed.mgmVecTot.isValid(), rotRateB, sensorValues.rw1Set.currSpeed.value,
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sensorValues.rw2Set.currSpeed.value, sensorValues.rw3Set.currSpeed.value,
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sensorValues.rw4Set.currSpeed.value, mgtDpDes);
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allRwAvailable, &rwAvail, &acsParameters.gsTargetModeControllerParameters,
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mgmDataProcessed.mgmVecTot.value, mgmDataProcessed.mgmVecTot.isValid(),
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sensorValues.rw1Set.currSpeed.value, sensorValues.rw2Set.currSpeed.value,
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sensorValues.rw3Set.currSpeed.value, sensorValues.rw4Set.currSpeed.value, mgtDpDes);
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break;
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case acs::PTG_NADIR:
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@ -498,10 +498,10 @@ void AcsController::performPointingCtrl() {
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VectorOperations<double>::add(torquePtgRws, rwTrqNs, torqueRws, 4);
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actuatorCmd.scalingTorqueRws(torqueRws, acsParameters.rwHandlingParameters.maxTrq);
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ptgCtrl.ptgDesaturation(
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&acsParameters.nadirModeControllerParameters, mgmDataProcessed.mgmVecTot.value,
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mgmDataProcessed.mgmVecTot.isValid(), rotRateB, sensorValues.rw1Set.currSpeed.value,
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sensorValues.rw2Set.currSpeed.value, sensorValues.rw3Set.currSpeed.value,
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sensorValues.rw4Set.currSpeed.value, mgtDpDes);
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allRwAvailable, &rwAvail, &acsParameters.nadirModeControllerParameters,
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mgmDataProcessed.mgmVecTot.value, mgmDataProcessed.mgmVecTot.isValid(),
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sensorValues.rw1Set.currSpeed.value, sensorValues.rw2Set.currSpeed.value,
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sensorValues.rw3Set.currSpeed.value, sensorValues.rw4Set.currSpeed.value, mgtDpDes);
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break;
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case acs::PTG_INERTIAL:
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@ -520,10 +520,10 @@ void AcsController::performPointingCtrl() {
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VectorOperations<double>::add(torquePtgRws, rwTrqNs, torqueRws, 4);
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actuatorCmd.scalingTorqueRws(torqueRws, acsParameters.rwHandlingParameters.maxTrq);
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ptgCtrl.ptgDesaturation(
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&acsParameters.inertialModeControllerParameters, mgmDataProcessed.mgmVecTot.value,
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mgmDataProcessed.mgmVecTot.isValid(), rotRateB, sensorValues.rw1Set.currSpeed.value,
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sensorValues.rw2Set.currSpeed.value, sensorValues.rw3Set.currSpeed.value,
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sensorValues.rw4Set.currSpeed.value, mgtDpDes);
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allRwAvailable, &rwAvail, &acsParameters.inertialModeControllerParameters,
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mgmDataProcessed.mgmVecTot.value, mgmDataProcessed.mgmVecTot.isValid(),
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sensorValues.rw1Set.currSpeed.value, sensorValues.rw2Set.currSpeed.value,
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sensorValues.rw3Set.currSpeed.value, sensorValues.rw4Set.currSpeed.value, mgtDpDes);
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break;
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default:
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sif::error << "AcsController: Invalid mode for performPointingCtrl" << std::endl;
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@ -89,6 +89,8 @@ class AcsController : public ExtendedControllerBase, public ReceivesParameterMes
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int32_t cmdSpeedRws[4] = {0, 0, 0, 0};
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int16_t cmdDipoleMtqs[3] = {0, 0, 0};
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acsctrl::RwAvail rwAvail;
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#if OBSW_THREAD_TRACING == 1
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uint32_t opCounter = 0;
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#endif
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@ -327,28 +327,32 @@ void Guidance::comparePtg(double currentQuat[4], double currentSatRotRate[3], do
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}
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ReturnValue_t Guidance::getDistributionMatrixRw(ACS::SensorValues *sensorValues,
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double *rwPseudoInv) {
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bool rw1valid = (sensorValues->rw1Set.state.value and sensorValues->rw1Set.state.isValid());
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bool rw2valid = (sensorValues->rw2Set.state.value and sensorValues->rw2Set.state.isValid());
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bool rw3valid = (sensorValues->rw3Set.state.value and sensorValues->rw3Set.state.isValid());
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bool rw4valid = (sensorValues->rw4Set.state.value and sensorValues->rw4Set.state.isValid());
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double *rwPseudoInv, acsctrl::RwAvail *rwAvail) {
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rwAvail->rw1avail = (sensorValues->rw1Set.state.value and sensorValues->rw1Set.state.isValid());
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rwAvail->rw2avail = (sensorValues->rw2Set.state.value and sensorValues->rw2Set.state.isValid());
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rwAvail->rw3avail = (sensorValues->rw3Set.state.value and sensorValues->rw3Set.state.isValid());
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rwAvail->rw4avail = (sensorValues->rw4Set.state.value and sensorValues->rw4Set.state.isValid());
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if (rw1valid and rw2valid and rw3valid and rw4valid) {
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if (rwAvail->rw1avail and rwAvail->rw2avail and rwAvail->rw3avail and rwAvail->rw4avail) {
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std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverse, 12 * sizeof(double));
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return returnvalue::OK;
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} else if (not rw1valid and rw2valid and rw3valid and rw4valid) {
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} else if (not rwAvail->rw1avail and rwAvail->rw2avail and rwAvail->rw3avail and
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rwAvail->rw4avail) {
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std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverseWithoutRW1,
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12 * sizeof(double));
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return acsctrl::SINGLE_RW_UNAVAILABLE;
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} else if (rw1valid and not rw2valid and rw3valid and rw4valid) {
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} else if (rwAvail->rw1avail and not rwAvail->rw2avail and rwAvail->rw3avail and
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rwAvail->rw4avail) {
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std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverseWithoutRW2,
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12 * sizeof(double));
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return acsctrl::SINGLE_RW_UNAVAILABLE;
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} else if (rw1valid and rw2valid and not rw3valid and rw4valid) {
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} else if (rwAvail->rw1avail and rwAvail->rw2avail and not rwAvail->rw3avail and
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rwAvail->rw4avail) {
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std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverseWithoutRW3,
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12 * sizeof(double));
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return acsctrl::SINGLE_RW_UNAVAILABLE;
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} else if (rw1valid and rw2valid and rw3valid and not rw4valid) {
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} else if (rwAvail->rw1avail and rwAvail->rw2avail and rwAvail->rw3avail and
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not rwAvail->rw4avail) {
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std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverseWithoutRW4,
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12 * sizeof(double));
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return acsctrl::SINGLE_RW_UNAVAILABLE;
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@ -44,7 +44,8 @@ class Guidance {
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double targetSatRotRate[3], double errorQuat[4], double errorSatRotRate[3],
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double &errorAngle);
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ReturnValue_t getDistributionMatrixRw(ACS::SensorValues *sensorValues, double *rwPseudoInv);
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ReturnValue_t getDistributionMatrixRw(ACS::SensorValues *sensorValues, double *rwPseudoInv,
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acsctrl::RwAvail *rwAvail);
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private:
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const AcsParameters *acsParameters;
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@ -1,11 +1,5 @@
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#include "PtgCtrl.h"
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#include <fsfw/globalfunctions/constants.h>
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#include <fsfw/globalfunctions/math/MatrixOperations.h>
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#include <fsfw/globalfunctions/math/QuaternionOperations.h>
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#include <fsfw/globalfunctions/math/VectorOperations.h>
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#include <fsfw/globalfunctions/sign.h>
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PtgCtrl::PtgCtrl(AcsParameters *acsParameters_) { acsParameters = acsParameters_; }
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PtgCtrl::~PtgCtrl() {}
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@ -68,9 +62,9 @@ void PtgCtrl::ptgLaw(AcsParameters::PointingLawParameters *pointingLawParameters
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// Inverse of gainMatrix
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double gainMatrixInverse[3][3] = {{0, 0, 0}, {0, 0, 0}, {0, 0, 0}};
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gainMatrixInverse[0][0] = 1 / gainMatrix[0][0];
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gainMatrixInverse[1][1] = 1 / gainMatrix[1][1];
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gainMatrixInverse[2][2] = 1 / gainMatrix[2][2];
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gainMatrixInverse[0][0] = 1. / gainMatrix[0][0];
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gainMatrixInverse[1][1] = 1. / gainMatrix[1][1];
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gainMatrixInverse[2][2] = 1. / gainMatrix[2][2];
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double pMatrix[3][3] = {{0, 0, 0}, {0, 0, 0}, {0, 0, 0}};
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MatrixOperations<double>::multiply(
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@ -146,9 +140,10 @@ void PtgCtrl::ptgNullspace(const bool allRwAvabilable,
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4);
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}
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void PtgCtrl::ptgDesaturation(AcsParameters::PointingLawParameters *pointingLawParameters,
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void PtgCtrl::ptgDesaturation(const bool allRwAvailable, const acsctrl::RwAvail *rwAvail,
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AcsParameters::PointingLawParameters *pointingLawParameters,
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const double *magFieldB, const bool magFieldBValid,
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const double *satRate, const int32_t speedRw0, const int32_t speedRw1,
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const int32_t speedRw0, const int32_t speedRw1,
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const int32_t speedRw2, const int32_t speedRw3, double *mgtDpDes) {
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if (not magFieldBValid or not pointingLawParameters->desatOn) {
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return;
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@ -162,17 +157,24 @@ void PtgCtrl::ptgDesaturation(AcsParameters::PointingLawParameters *pointingLawP
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double magFieldBT[3] = {0, 0, 0};
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VectorOperations<double>::mulScalar(magFieldB, 1e-6, magFieldBT, 3);
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// calculate angular momentum of the satellite
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double angMomentumSat[3] = {0, 0, 0};
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MatrixOperations<double>::multiply(*(acsParameters->inertiaEIVE.inertiaMatrixDeployed), satRate,
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angMomentumSat, 3, 3, 1);
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// calculate angular momentum of the reaction wheels with respect to the nullspace RW speed
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// relocate RW speed zero to nullspace RW speed
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double refSpeedRws[4] = {0, 0, 0, 0};
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VectorOperations<double>::mulScalar(acsParameters->rwMatrices.nullspaceVector,
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pointingLawParameters->nullspaceSpeed, refSpeedRws, 4);
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if (not allRwAvailable) {
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if (not rwAvail->rw1avail) {
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refSpeedRws[0] = 0.0;
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} else if (not rwAvail->rw2avail) {
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refSpeedRws[1] = 0.0;
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} else if (not rwAvail->rw3avail) {
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refSpeedRws[2] = 0.0;
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} else if (not rwAvail->rw4avail) {
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refSpeedRws[3] = 0.0;
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}
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}
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VectorOperations<double>::subtract(speedRws, refSpeedRws, speedRws, 4);
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// convert speed from 10 RPM to 1 RPM
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VectorOperations<double>::mulScalar(speedRws, 1e-1, speedRws, 4);
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// convert to rad/s
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@ -188,16 +190,12 @@ void PtgCtrl::ptgDesaturation(AcsParameters::PointingLawParameters *pointingLawP
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// calculate total angular momentum
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double angMomentumTotal[3] = {0, 0, 0};
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VectorOperations<double>::add(angMomentumSat, angMomentumRw, angMomentumTotal, 3);
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// calculating momentum error
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double deltaAngMomentum[3] = {0, 0, 0};
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VectorOperations<double>::subtract(angMomentumTotal, pointingLawParameters->desatMomentumRef,
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deltaAngMomentum, 3);
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VectorOperations<double>::subtract(angMomentumRw, pointingLawParameters->desatMomentumRef,
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angMomentumTotal, 3);
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// resulting magnetic dipole command
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double crossAngMomentumMagField[3] = {0, 0, 0};
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VectorOperations<double>::cross(deltaAngMomentum, magFieldBT, crossAngMomentumMagField);
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VectorOperations<double>::cross(angMomentumTotal, magFieldBT, crossAngMomentumMagField);
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double factor =
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pointingLawParameters->deSatGainFactor / VectorOperations<double>::norm(magFieldBT, 3);
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VectorOperations<double>::mulScalar(crossAngMomentumMagField, factor, mgtDpDes, 3);
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@ -1,11 +1,16 @@
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#ifndef PTGCTRL_H_
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#define PTGCTRL_H_
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#include <math.h>
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#include <fsfw/globalfunctions/math/MatrixOperations.h>
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#include <fsfw/globalfunctions/math/QuaternionOperations.h>
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#include <fsfw/globalfunctions/math/VectorOperations.h>
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#include <fsfw/globalfunctions/sign.h>
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#include <mission/acs/defs.h>
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#include <mission/controller/acs/AcsParameters.h>
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#include <mission/controller/acs/SensorValues.h>
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#include <stdio.h>
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#include <mission/controller/controllerdefinitions/AcsCtrlDefinitions.h>
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#include <cmath>
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class PtgCtrl {
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/*
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@ -38,10 +43,11 @@ class PtgCtrl {
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const int32_t speedRw0, const int32_t speedRw1, const int32_t speedRw2,
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const int32_t speedRw3, double *rwTrqNs);
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void ptgDesaturation(AcsParameters::PointingLawParameters *pointingLawParameters,
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const double *magFieldB, const bool magFieldBValid, const double *satRate,
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const int32_t speedRw0, const int32_t speedRw1, const int32_t speedRw2,
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const int32_t speedRw3, double *mgtDpDes);
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void ptgDesaturation(const bool allRwAvabilable, const acsctrl::RwAvail *rwAvail,
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AcsParameters::PointingLawParameters *pointingLawParameters,
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const double *magFieldB, const bool magFieldBValid, const int32_t speedRw0,
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const int32_t speedRw1, const int32_t speedRw2, const int32_t speedRw3,
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double *mgtDpDes);
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/* @brief: Commands the stiction torque in case wheel speed is to low
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* torqueCommand modified torque after anti-stiction
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@ -21,6 +21,13 @@ static constexpr ReturnValue_t SINGLE_RW_UNAVAILABLE = MAKE_RETURN_CODE(0xA3);
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//! [EXPORT] : [COMMENT] Multiple RWs have failed.
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static constexpr ReturnValue_t MULTIPLE_RW_UNAVAILABLE = MAKE_RETURN_CODE(0xA4);
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struct RwAvail {
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bool rw1avail = false;
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bool rw2avail = false;
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bool rw3avail = false;
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bool rw4avail = false;
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};
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enum SetIds : uint32_t {
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MGM_SENSOR_DATA,
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MGM_PROCESSED_DATA,
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