Merge pull request 'Fixes for RW Commanding' (#852) from cmd-rw-fix into main
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Reviewed-on: #852 Reviewed-by: Robin Müller <muellerr@irs.uni-stuttgart.de>
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d065f6257e
@ -29,6 +29,14 @@ will consitute of a breaking change warranting a new major release:
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- If the PCDU handler fails reading data from the IPC store, it will
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not try to do a deserialization anymore.
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- All action commands sent by the PLOC SUPV to itself will have no sender now.
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- RW speed commands get reset to 0 RPM, if the `AcsController` has changed its mode
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to Safe
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- Antistiction for RWs will set commanded speed to 0 RPM, if a wheel is detected as not
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working
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- Removed parameter to disable antistiction, as deactivating it would result in the
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`AcsController` being allowed sending invalid speed commands to the RW Handler, which
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would then trigger FDIR and turning off the functioning device
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- `RwHandler` returnvalues would use the `INTERFACE_ID` of the `DeviceHandlerBase`
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# [v7.5.5] 2024-01-22
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@ -59,6 +59,7 @@ class RwHandler : public DeviceHandlerBase {
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LocalPoolDataSetBase* getDataSetHandle(sid_t sid) override;
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private:
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static const uint8_t INTERFACE_ID = CLASS_ID::RW_HANDLER;
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//! [EXPORT] : [COMMENT] Action Message with invalid speed was received. Valid speeds must be in
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//! the range of [-65000; 1000] or [1000; 65000]
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static const ReturnValue_t INVALID_SPEED = MAKE_RETURN_CODE(0xA0);
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@ -445,7 +445,6 @@ void AcsController::performPointingCtrl() {
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break;
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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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ReturnValue_t result = guidance.getDistributionMatrixRw(&sensorValues, *rwPseudoInv);
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if (result == returnvalue::FAILED) {
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@ -486,7 +485,6 @@ void AcsController::performPointingCtrl() {
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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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enableAntiStiction = acsParameters.idleModeControllerParameters.enableAntiStiction;
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break;
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case acs::PTG_TARGET:
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@ -510,7 +508,6 @@ void AcsController::performPointingCtrl() {
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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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enableAntiStiction = acsParameters.targetModeControllerParameters.enableAntiStiction;
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break;
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case acs::PTG_TARGET_GS:
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@ -531,7 +528,6 @@ void AcsController::performPointingCtrl() {
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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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enableAntiStiction = acsParameters.gsTargetModeControllerParameters.enableAntiStiction;
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break;
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case acs::PTG_NADIR:
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@ -555,7 +551,6 @@ void AcsController::performPointingCtrl() {
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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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enableAntiStiction = acsParameters.nadirModeControllerParameters.enableAntiStiction;
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break;
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case acs::PTG_INERTIAL:
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@ -578,7 +573,6 @@ void AcsController::performPointingCtrl() {
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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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enableAntiStiction = acsParameters.inertialModeControllerParameters.enableAntiStiction;
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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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@ -590,9 +584,7 @@ void AcsController::performPointingCtrl() {
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sensorValues.rw3Set.currSpeed.value, sensorValues.rw4Set.currSpeed.value,
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acsParameters.onBoardParams.sampleTime, acsParameters.rwHandlingParameters.inertiaWheel,
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acsParameters.rwHandlingParameters.maxRwSpeed, torqueRws, cmdSpeedRws);
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if (enableAntiStiction) {
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ptgCtrl.rwAntistiction(&sensorValues, cmdSpeedRws);
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}
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actuatorCmd.cmdDipoleMtq(*acsParameters.magnetorquerParameter.inverseAlignment,
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acsParameters.magnetorquerParameter.dipoleMax, mgtDpDes, cmdDipoleMtqs);
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@ -885,6 +877,24 @@ ReturnValue_t AcsController::checkModeCommand(Mode_t mode, Submode_t submode,
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}
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void AcsController::modeChanged(Mode_t mode, Submode_t submode) {
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if (mode == acs::AcsMode::SAFE) {
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{
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PoolReadGuard pg(&rw1SpeedSet);
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rw1SpeedSet.setRwSpeed(0, 10);
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}
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{
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PoolReadGuard pg(&rw2SpeedSet);
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rw2SpeedSet.setRwSpeed(0, 10);
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}
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{
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PoolReadGuard pg(&rw3SpeedSet);
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rw3SpeedSet.setRwSpeed(0, 10);
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}
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{
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PoolReadGuard pg(&rw4SpeedSet);
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rw4SpeedSet.setRwSpeed(0, 10);
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}
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}
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return ExtendedControllerBase::modeChanged(mode, submode);
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}
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@ -432,9 +432,6 @@ ReturnValue_t AcsParameters::getParameter(uint8_t domainId, uint8_t parameterId,
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parameterWrapper->set(idleModeControllerParameters.desatOn);
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break;
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case 0x9:
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parameterWrapper->set(idleModeControllerParameters.enableAntiStiction);
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break;
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case 0xA:
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parameterWrapper->set(idleModeControllerParameters.useMekf);
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break;
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default:
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@ -471,42 +468,39 @@ ReturnValue_t AcsParameters::getParameter(uint8_t domainId, uint8_t parameterId,
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parameterWrapper->set(targetModeControllerParameters.desatOn);
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break;
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case 0x9:
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parameterWrapper->set(targetModeControllerParameters.enableAntiStiction);
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break;
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case 0xA:
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parameterWrapper->set(targetModeControllerParameters.useMekf);
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break;
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case 0xB:
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case 0xA:
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parameterWrapper->setVector(targetModeControllerParameters.refDirection);
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break;
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case 0xC:
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case 0xB:
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parameterWrapper->setVector(targetModeControllerParameters.refRotRate);
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break;
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case 0xD:
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case 0xC:
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parameterWrapper->setVector(targetModeControllerParameters.quatRef);
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break;
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case 0xE:
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case 0xD:
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parameterWrapper->set(targetModeControllerParameters.timeElapsedMax);
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break;
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case 0xF:
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case 0xE:
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parameterWrapper->set(targetModeControllerParameters.latitudeTgt);
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break;
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case 0x10:
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case 0xF:
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parameterWrapper->set(targetModeControllerParameters.longitudeTgt);
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break;
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case 0x11:
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case 0x10:
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parameterWrapper->set(targetModeControllerParameters.altitudeTgt);
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break;
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case 0x12:
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case 0x11:
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parameterWrapper->set(targetModeControllerParameters.avoidBlindStr);
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break;
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case 0x13:
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case 0x12:
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parameterWrapper->set(targetModeControllerParameters.blindAvoidStart);
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break;
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case 0x14:
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case 0x13:
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parameterWrapper->set(targetModeControllerParameters.blindAvoidStop);
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break;
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case 0x15:
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case 0x14:
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parameterWrapper->set(targetModeControllerParameters.blindRotRate);
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break;
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default:
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@ -543,24 +537,21 @@ ReturnValue_t AcsParameters::getParameter(uint8_t domainId, uint8_t parameterId,
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parameterWrapper->set(gsTargetModeControllerParameters.desatOn);
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break;
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case 0x9:
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parameterWrapper->set(gsTargetModeControllerParameters.enableAntiStiction);
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break;
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case 0xA:
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parameterWrapper->set(gsTargetModeControllerParameters.useMekf);
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break;
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case 0xB:
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case 0xA:
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parameterWrapper->setVector(gsTargetModeControllerParameters.refDirection);
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break;
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case 0xC:
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case 0xB:
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parameterWrapper->set(gsTargetModeControllerParameters.timeElapsedMax);
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break;
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case 0xD:
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case 0xC:
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parameterWrapper->set(gsTargetModeControllerParameters.latitudeTgt);
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break;
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case 0xE:
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case 0xD:
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parameterWrapper->set(gsTargetModeControllerParameters.longitudeTgt);
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break;
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case 0xF:
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case 0xE:
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parameterWrapper->set(gsTargetModeControllerParameters.altitudeTgt);
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break;
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default:
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@ -597,21 +588,18 @@ ReturnValue_t AcsParameters::getParameter(uint8_t domainId, uint8_t parameterId,
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parameterWrapper->set(nadirModeControllerParameters.desatOn);
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break;
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case 0x9:
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parameterWrapper->set(nadirModeControllerParameters.enableAntiStiction);
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break;
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case 0xA:
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parameterWrapper->set(nadirModeControllerParameters.useMekf);
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break;
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case 0xB:
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case 0xA:
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parameterWrapper->setVector(nadirModeControllerParameters.refDirection);
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break;
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case 0xC:
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case 0xB:
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parameterWrapper->setVector(nadirModeControllerParameters.quatRef);
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break;
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case 0xD:
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case 0xC:
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parameterWrapper->setVector(nadirModeControllerParameters.refRotRate);
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break;
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case 0xE:
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case 0xD:
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parameterWrapper->set(nadirModeControllerParameters.timeElapsedMax);
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break;
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default:
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@ -648,18 +636,15 @@ ReturnValue_t AcsParameters::getParameter(uint8_t domainId, uint8_t parameterId,
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parameterWrapper->set(inertialModeControllerParameters.desatOn);
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break;
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case 0x9:
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parameterWrapper->set(inertialModeControllerParameters.enableAntiStiction);
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break;
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case 0xA:
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parameterWrapper->set(inertialModeControllerParameters.useMekf);
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break;
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case 0xB:
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case 0xA:
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parameterWrapper->setVector(inertialModeControllerParameters.tgtQuat);
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break;
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case 0xC:
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case 0xB:
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parameterWrapper->setVector(inertialModeControllerParameters.refRotRate);
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break;
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case 0xD:
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case 0xC:
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parameterWrapper->setVector(inertialModeControllerParameters.quatRef);
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break;
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default:
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@ -863,7 +863,6 @@ class AcsParameters : public HasParametersIF {
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double desatMomentumRef[3] = {0, 0, 0};
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double deSatGainFactor = 1000;
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uint8_t desatOn = true;
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uint8_t enableAntiStiction = true;
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uint8_t useMekf = false;
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} pointingLawParameters;
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@ -220,6 +220,8 @@ void PtgCtrl::rwAntistiction(ACS::SensorValues *sensorValues, int32_t *rwCmdSpee
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}
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}
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}
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} else {
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rwCmdSpeeds[i] = 0;
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}
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}
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}
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