Merge pull request 'Fixes for Pointing Modes' (#851) from ptg-fixes into main

Reviewed-on: #851

CHANGELOG.md

@@ -16,6 +16,9 @@ will consitute of a breaking change warranting a new major release:
 
 # [unreleased]
 
+- Bumped `eive-tmtc` to 
+- Bumped `eive-fsfw`
+
 ## Added
 
 - Added new parameter for MPSoC which allows to skip SUPV commanding.
@@ -40,6 +43,13 @@ will consitute of a breaking change warranting a new major release:
   `AcsController` being allowed sending invalid speed commands to the RW Handler, which
   would then trigger FDIR and turning off the functioning device
 - `RwHandler` returnvalues would use the `INTERFACE_ID` of the `DeviceHandlerBase`
+- The `AcsController` will reset its stored guidance values on mode change and lost
+  orientation.
+- The nullspace controller will only be used if all RWs are available.
+- Calculation of required rotation rate in pointing modes has been fixed to actual
+  calculation of rotation rate from two quaternions.
+- Fixed alignment matrix and pseudo inverses of RWs, to match the wrong definition of
+  positive rotation.
 
 # [v7.5.5] 2024-01-22
 

fsfw

@@ -1 +1 @@
-Subproject commit e64e8b274d436502d5c5b87865b9006e52e4b1aa
+Subproject commit b5e7179af1da085b9be598b4897f2664012781af

mission/controller/AcsController.cpp

@@ -49,7 +49,7 @@ ReturnValue_t AcsController::executeAction(ActionId_t actionId, MessageQueueId_t
     case SOLAR_ARRAY_DEPLOYMENT_SUCCESSFUL: {
       ReturnValue_t result = guidance.solarArrayDeploymentComplete();
       if (result == returnvalue::FAILED) {
-        return FILE_DELETION_FAILED;
+        return acsctrl::FILE_DELETION_FAILED;
       }
       return HasActionsIF::EXECUTION_FINISHED;
     }
@@ -360,6 +360,7 @@ void AcsController::performPointingCtrl() {
       triggerEvent(acs::PTG_CTRL_NO_ATTITUDE_INFORMATION);
       ptgCtrlLostCounter = 0;
     }
+    guidance.resetValues();
     updateCtrlValData(ptgCtrlStrat);
     updateActuatorCmdData(ZERO_VEC4, cmdSpeedRws, ZERO_VEC3_INT16);
     commandActuators(0, 0, 0, acsParameters.magnetorquerParameter.torqueDuration, cmdSpeedRws[0],
@@ -393,9 +394,10 @@ void AcsController::performPointingCtrl() {
       break;
   }
 
+  bool allRwAvailable = true;
   double rwPseudoInv[4][3] = {{0, 0, 0}, {0, 0, 0}, {0, 0, 0}, {0, 0, 0}};
   ReturnValue_t result = guidance.getDistributionMatrixRw(&sensorValues, *rwPseudoInv);
-  if (result == returnvalue::FAILED) {
+  if (result == acsctrl::MULTIPLE_RW_UNAVAILABLE) {
     if (multipleRwUnavailableCounter >=
         acsParameters.rwHandlingParameters.multipleRwInvalidTimeout) {
       triggerEvent(acs::MULTIPLE_RW_INVALID);
@@ -403,8 +405,10 @@ void AcsController::performPointingCtrl() {
     }
     multipleRwUnavailableCounter++;
     return;
-  } else {
+  }
   multipleRwUnavailableCounter = 0;
+  if (result == acsctrl::SINGLE_RW_UNAVAILABLE) {
+    allRwAvailable = false;
   }
 
   // Variables required for guidance
@@ -422,7 +426,7 @@ void AcsController::performPointingCtrl() {
                           errorSatRotRate, errorAngle);
       ptgCtrl.ptgLaw(&acsParameters.idleModeControllerParameters, errorQuat, errorSatRotRate,
                      *rwPseudoInv, torquePtgRws);
-      ptgCtrl.ptgNullspace(&acsParameters.idleModeControllerParameters,
+      ptgCtrl.ptgNullspace(allRwAvailable, &acsParameters.idleModeControllerParameters,
                            sensorValues.rw1Set.currSpeed.value, sensorValues.rw2Set.currSpeed.value,
                            sensorValues.rw3Set.currSpeed.value, sensorValues.rw4Set.currSpeed.value,
                            rwTrqNs);
@@ -445,7 +449,7 @@ void AcsController::performPointingCtrl() {
                           errorSatRotRate, errorAngle);
       ptgCtrl.ptgLaw(&acsParameters.targetModeControllerParameters, errorQuat, errorSatRotRate,
                      *rwPseudoInv, torquePtgRws);
-      ptgCtrl.ptgNullspace(&acsParameters.targetModeControllerParameters,
+      ptgCtrl.ptgNullspace(allRwAvailable, &acsParameters.targetModeControllerParameters,
                            sensorValues.rw1Set.currSpeed.value, sensorValues.rw2Set.currSpeed.value,
                            sensorValues.rw3Set.currSpeed.value, sensorValues.rw4Set.currSpeed.value,
                            rwTrqNs);
@@ -465,7 +469,7 @@ void AcsController::performPointingCtrl() {
                           errorSatRotRate, errorAngle);
       ptgCtrl.ptgLaw(&acsParameters.gsTargetModeControllerParameters, errorQuat, errorSatRotRate,
                      *rwPseudoInv, torquePtgRws);
-      ptgCtrl.ptgNullspace(&acsParameters.gsTargetModeControllerParameters,
+      ptgCtrl.ptgNullspace(allRwAvailable, &acsParameters.gsTargetModeControllerParameters,
                            sensorValues.rw1Set.currSpeed.value, sensorValues.rw2Set.currSpeed.value,
                            sensorValues.rw3Set.currSpeed.value, sensorValues.rw4Set.currSpeed.value,
                            rwTrqNs);
@@ -488,7 +492,7 @@ void AcsController::performPointingCtrl() {
                           errorSatRotRate, errorAngle);
       ptgCtrl.ptgLaw(&acsParameters.nadirModeControllerParameters, errorQuat, errorSatRotRate,
                      *rwPseudoInv, torquePtgRws);
-      ptgCtrl.ptgNullspace(&acsParameters.nadirModeControllerParameters,
+      ptgCtrl.ptgNullspace(allRwAvailable, &acsParameters.nadirModeControllerParameters,
                            sensorValues.rw1Set.currSpeed.value, sensorValues.rw2Set.currSpeed.value,
                            sensorValues.rw3Set.currSpeed.value, sensorValues.rw4Set.currSpeed.value,
                            rwTrqNs);
@@ -510,7 +514,7 @@ void AcsController::performPointingCtrl() {
                           errorSatRotRate, errorAngle);
       ptgCtrl.ptgLaw(&acsParameters.inertialModeControllerParameters, errorQuat, errorSatRotRate,
                      *rwPseudoInv, torquePtgRws);
-      ptgCtrl.ptgNullspace(&acsParameters.inertialModeControllerParameters,
+      ptgCtrl.ptgNullspace(allRwAvailable, &acsParameters.inertialModeControllerParameters,
                            sensorValues.rw1Set.currSpeed.value, sensorValues.rw2Set.currSpeed.value,
                            sensorValues.rw3Set.currSpeed.value, sensorValues.rw4Set.currSpeed.value,
                            rwTrqNs);
@@ -899,6 +903,7 @@ void AcsController::modeChanged(Mode_t mode, Submode_t submode) {
       rw4SpeedSet.setRwSpeed(0, 10);
     }
   }
+  guidance.resetValues();
   return ExtendedControllerBase::modeChanged(mode, submode);
 }
 
@@ -1095,7 +1100,7 @@ ReturnValue_t AcsController::writeTleToFs(const uint8_t *tle) {
     tleFile << "\n";
     tleFile.write(reinterpret_cast<const char *>(tle + 69), 69);
   } else {
-    return WRITE_FILE_FAILED;
+    return acsctrl::WRITE_FILE_FAILED;
   }
   tleFile.close();
   return returnvalue::OK;
@@ -1119,12 +1124,12 @@ ReturnValue_t AcsController::readTleFromFs(uint8_t *line1, uint8_t *line2) {
       std::memcpy(line2, tleLine2.c_str(), 69);
     } else {
       triggerEvent(acs::TLE_FILE_READ_FAILED);
-      return READ_FILE_FAILED;
+      return acsctrl::READ_FILE_FAILED;
     }
     tleFile.close();
   } else {
     triggerEvent(acs::TLE_FILE_READ_FAILED);
-    return READ_FILE_FAILED;
+    return acsctrl::READ_FILE_FAILED;
   }
   return returnvalue::OK;
 }

mission/controller/AcsController.h

@@ -112,14 +112,6 @@ class AcsController : public ExtendedControllerBase, public ReceivesParameterMes
   static const DeviceCommandId_t UPDATE_TLE = 0x3;
   static const DeviceCommandId_t READ_TLE = 0x4;
 
-  static const uint8_t INTERFACE_ID = CLASS_ID::ACS_CTRL;
-  //! [EXPORT] : [COMMENT] File deletion failed and at least one file is still existent.
-  static constexpr ReturnValue_t FILE_DELETION_FAILED = MAKE_RETURN_CODE(0);
-  //! [EXPORT] : [COMMENT] Writing the TLE to the file has failed.
-  static constexpr ReturnValue_t WRITE_FILE_FAILED = MAKE_RETURN_CODE(1);
-  //! [EXPORT] : [COMMENT] Reading the TLE to the file has failed.
-  static constexpr ReturnValue_t READ_FILE_FAILED = MAKE_RETURN_CODE(2);
-
   ReturnValue_t initialize() override;
   ReturnValue_t handleCommandMessage(CommandMessage* message) override;
   void performControlOperation() override;

mission/controller/acs/AcsParameters.cpp

@@ -333,16 +333,16 @@ ReturnValue_t AcsParameters::getParameter(uint8_t domainId, uint8_t parameterId,
           parameterWrapper->setMatrix(rwMatrices.pseudoInverse);
           break;
         case 0x2:
-          parameterWrapper->setMatrix(rwMatrices.without1);
+          parameterWrapper->setMatrix(rwMatrices.pseudoInverseWithoutRW1);
           break;
         case 0x3:
-          parameterWrapper->setMatrix(rwMatrices.without2);
+          parameterWrapper->setMatrix(rwMatrices.pseudoInverseWithoutRW2);
           break;
         case 0x4:
-          parameterWrapper->setMatrix(rwMatrices.without3);
+          parameterWrapper->setMatrix(rwMatrices.pseudoInverseWithoutRW3);
           break;
         case 0x5:
-          parameterWrapper->setMatrix(rwMatrices.without4);
+          parameterWrapper->setMatrix(rwMatrices.pseudoInverseWithoutRW4);
           break;
         case 0x6:
           parameterWrapper->setVector(rwMatrices.nullspaceVector);

mission/controller/acs/AcsParameters.h

@@ -812,19 +812,19 @@ class AcsParameters : public HasParametersIF {
   } rwHandlingParameters;
 
   struct RwMatrices {
-    double alignmentMatrix[3][4] = {{0.9205, 0.0000, -0.9205, 0.0000},
-                                    {0.0000, -0.9205, 0.0000, 0.9205},
-                                    {0.3907, 0.3907, 0.3907, 0.3907}};
+    double alignmentMatrix[3][4] = {{-0.9205, 0.0000, 0.9205, 0.0000},
+                                    {0.0000, 0.9205, 0.0000, -0.9205},
+                                    {-0.3907, -0.3907, -0.3907, -0.3907}};
     double pseudoInverse[4][3] = {
-        {0.5432, 0, 0.6398}, {0, -0.5432, 0.6398}, {-0.5432, 0, 0.6398}, {0, 0.5432, 0.6398}};
-    double without1[4][3] = {
-        {0, 0, 0}, {0.5432, -0.5432, 1.2797}, {-1.0864, 0, 0}, {0.5432, 0.5432, 1.2797}};
-    double without2[4][3] = {
-        {0.5432, -0.5432, 1.2797}, {0, 0, 0}, {-0.5432, -0.5432, 1.2797}, {0, 1.0864, 0}};
-    double without3[4][3] = {
-        {1.0864, 0, 0}, {-0.5432, -0.5432, 1.2797}, {0, 0, 0}, {-0.5432, 0.5432, 1.2797}};
-    double without4[4][3] = {
-        {0.5432, 0.5432, 1.2797}, {0, -1.0864, 0}, {-0.5432, 0.5432, 1.2797}, {0, 0, 0}};
+        {-0.5432, 0, -0.6399}, {0, 0.5432, -0.6399}, {0.5432, 0, -0.6399}, {0, -0.5432, -0.6399}};
+    double pseudoInverseWithoutRW1[4][3] = {
+        {0, 0, 0}, {-0.5432, 0.5432, -1.2798}, {1.0864, 0, 0}, {-0.5432, -0.5432, -1.2798}};
+    double pseudoInverseWithoutRW2[4][3] = {
+        {-0.5432, 0.5432, -1.2798}, {0, 0, 0}, {0.5432, 0.5432, -1.2798}, {0, -1.0864, 0}};
+    double pseudoInverseWithoutRW3[4][3] = {
+        {-1.0864, 0, 0}, {0.5432, 0.5432, -1.2798}, {0, 0, 0}, {0.5432, -0.5432, -1.2798}};
+    double pseudoInverseWithoutRW4[4][3] = {
+        {-0.5432, -0.5432, -1.2798}, {0, 1.0864, 0}, {0.5432, -0.5432, -1.2798}, {0, 0, 0}};
     double nullspaceVector[4] = {-1, 1, -1, 1};
   } rwMatrices;
 

mission/controller/acs/Guidance.cpp

@@ -1,15 +1,5 @@
 #include "Guidance.h"
 
-#include <fsfw/datapool/PoolReadGuard.h>
-#include <fsfw/globalfunctions/math/MatrixOperations.h>
-#include <fsfw/globalfunctions/math/QuaternionOperations.h>
-#include <fsfw/globalfunctions/math/VectorOperations.h>
-#include <mission/controller/acs/util/MathOperations.h>
-
-#include <cmath>
-#include <filesystem>
-#include <string>
-
 Guidance::Guidance(AcsParameters *acsParameters_) { acsParameters = acsParameters_; }
 
 Guidance::~Guidance() {}
@@ -431,7 +421,11 @@ void Guidance::comparePtg(double currentQuat[4], double currentSatRotRate[3], do
   errorAngle = QuaternionOperations::getAngle(errorQuat, true);
 
   // Calculate error satellite rotational rate
-  // First combine the target and reference satellite rotational rates
+  // Convert target rotational rate into body RF
+  double errorQuatInv[4] = {0, 0, 0, 0}, targetSatRotRateB[3] = {0, 0, 0};
+  QuaternionOperations::inverse(errorQuat, errorQuatInv);
+  QuaternionOperations::multiplyVector(errorQuatInv, targetSatRotRate, targetSatRotRateB);
+  // Combine the target and reference satellite rotational rates
   double combinedRefSatRotRate[3] = {0, 0, 0};
   VectorOperations<double>::add(targetSatRotRate, refSatRotRate, combinedRefSatRotRate, 3);
   // Then subtract the combined required satellite rotational rates from the actual rate
@@ -455,44 +449,16 @@ void Guidance::comparePtg(double currentQuat[4], double currentSatRotRate[3], do
 }
 
 void Guidance::targetRotationRate(const int8_t timeElapsedMax, const double timeDelta,
-                                  double quatInertialTarget[4], double *refSatRate) {
-  //-------------------------------------------------------------------------------------
-  //	Calculation of target rotation rate
-  //-------------------------------------------------------------------------------------
-  if (VectorOperations<double>::norm(savedQuaternion, 4) == 0) {
-    std::memcpy(savedQuaternion, quatInertialTarget, sizeof(savedQuaternion));
+                                  double quatIX[4], double *refSatRate) {
+  if (VectorOperations<double>::norm(quatIXprev, 4) == 0) {
+    std::memcpy(quatIXprev, quatIX, sizeof(quatIXprev));
   }
-  if (timeDelta < timeElapsedMax and timeDelta != 0.0) {
-    double q[4] = {0, 0, 0, 0}, qS[4] = {0, 0, 0, 0};
-    QuaternionOperations::inverse(quatInertialTarget, q);
-    QuaternionOperations::inverse(savedQuaternion, qS);
-    double qDiff[4] = {0, 0, 0, 0};
-    VectorOperations<double>::subtract(q, qS, qDiff, 4);
-    VectorOperations<double>::mulScalar(qDiff, 1. / timeDelta, qDiff, 4);
-
-    double tgtQuatVec[3] = {q[0], q[1], q[2]};
-    double qDiffVec[3] = {qDiff[0], qDiff[1], qDiff[2]};
-    double sum1[3] = {0, 0, 0}, sum2[3] = {0, 0, 0}, sum3[3] = {0, 0, 0}, sum[3] = {0, 0, 0};
-    VectorOperations<double>::cross(tgtQuatVec, qDiffVec, sum1);
-    VectorOperations<double>::mulScalar(tgtQuatVec, qDiff[3], sum2, 3);
-    VectorOperations<double>::mulScalar(qDiffVec, q[3], sum3, 3);
-    VectorOperations<double>::add(sum1, sum2, sum, 3);
-    VectorOperations<double>::subtract(sum, sum3, sum, 3);
-    double omegaRefNew[3] = {0, 0, 0};
-    VectorOperations<double>::mulScalar(sum, -2, omegaRefNew, 3);
-
-    VectorOperations<double>::mulScalar(omegaRefNew, 2, refSatRate, 3);
-    VectorOperations<double>::subtract(refSatRate, omegaRefSaved, refSatRate, 3);
-    omegaRefSaved[0] = omegaRefNew[0];
-    omegaRefSaved[1] = omegaRefNew[1];
-    omegaRefSaved[2] = omegaRefNew[2];
+  if (timeDelta != 0.0) {
+    QuaternionOperations::rotationFromQuaternions(quatIX, quatIXprev, timeDelta, refSatRate);
   } else {
-    refSatRate[0] = 0;
-    refSatRate[1] = 0;
-    refSatRate[2] = 0;
+    std::memcpy(refSatRate, ZERO_VEC3, 3 * sizeof(double));
   }
-
-  std::memcpy(savedQuaternion, quatInertialTarget, sizeof(savedQuaternion));
+  std::memcpy(quatIXprev, quatIX, sizeof(quatIXprev));
 }
 
 ReturnValue_t Guidance::getDistributionMatrixRw(ACS::SensorValues *sensorValues,
@@ -506,22 +472,27 @@ ReturnValue_t Guidance::getDistributionMatrixRw(ACS::SensorValues *sensorValues,
     std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverse, 12 * sizeof(double));
     return returnvalue::OK;
   } else if (not rw1valid and rw2valid and rw3valid and rw4valid) {
-    std::memcpy(rwPseudoInv, acsParameters->rwMatrices.without1, 12 * sizeof(double));
-    return returnvalue::OK;
+    std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverseWithoutRW1,
+                12 * sizeof(double));
+    return acsctrl::SINGLE_RW_UNAVAILABLE;
   } else if (rw1valid and not rw2valid and rw3valid and rw4valid) {
-    std::memcpy(rwPseudoInv, acsParameters->rwMatrices.without2, 12 * sizeof(double));
-    return returnvalue::OK;
+    std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverseWithoutRW2,
+                12 * sizeof(double));
+    return acsctrl::SINGLE_RW_UNAVAILABLE;
   } else if (rw1valid and rw2valid and not rw3valid and rw4valid) {
-    std::memcpy(rwPseudoInv, acsParameters->rwMatrices.without3, 12 * sizeof(double));
-    return returnvalue::OK;
+    std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverseWithoutRW3,
+                12 * sizeof(double));
+    return acsctrl::SINGLE_RW_UNAVAILABLE;
   } else if (rw1valid and rw2valid and rw3valid and not rw4valid) {
-    std::memcpy(rwPseudoInv, acsParameters->rwMatrices.without4, 12 * sizeof(double));
-    return returnvalue::OK;
-  } else {
-    return returnvalue::FAILED;
+    std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverseWithoutRW4,
+                12 * sizeof(double));
+    return acsctrl::SINGLE_RW_UNAVAILABLE;
   }
+  return acsctrl::MULTIPLE_RW_UNAVAILABLE;
 }
 
+void Guidance::resetValues() { std::memcpy(quatIXprev, ZERO_VEC4, sizeof(quatIXprev)); }
+
 void Guidance::getTargetParamsSafe(double sunTargetSafe[3]) {
   std::error_code e;
   if (not std::filesystem::exists(SD_0_SKEWED_PTG_FILE, e) or

mission/controller/acs/Guidance.h

@@ -1,11 +1,19 @@
 #ifndef GUIDANCE_H_
 #define GUIDANCE_H_
 
+#include <fsfw/datapool/PoolReadGuard.h>
+#include <fsfw/globalfunctions/math/MatrixOperations.h>
+#include <fsfw/globalfunctions/math/QuaternionOperations.h>
+#include <fsfw/globalfunctions/math/VectorOperations.h>
+#include <mission/controller/acs/AcsParameters.h>
+#include <mission/controller/acs/SensorValues.h>
+#include <mission/controller/acs/util/MathOperations.h>
+#include <mission/controller/controllerdefinitions/AcsCtrlDefinitions.h>
 #include <time.h>
 
-#include "../controllerdefinitions/AcsCtrlDefinitions.h"
-#include "AcsParameters.h"
-#include "SensorValues.h"
+#include <cmath>
+#include <filesystem>
+#include <string>
 
 class Guidance {
  public:
@@ -14,6 +22,7 @@ class Guidance {
 
   void getTargetParamsSafe(double sunTargetSafe[3]);
   ReturnValue_t solarArrayDeploymentComplete();
+  void resetValues();
 
   // Function to get the target quaternion and reference rotation rate from gps position and
   // position of the ground station
@@ -59,9 +68,11 @@ class Guidance {
  private:
   const AcsParameters *acsParameters;
 
+  static constexpr double ZERO_VEC3[3] = {0, 0, 0};
+  static constexpr double ZERO_VEC4[4] = {0, 0, 0, 0};
+
   bool strBlindAvoidFlag = false;
-  double savedQuaternion[4] = {0, 0, 0, 0};
-  double omegaRefSaved[3] = {0, 0, 0};
+  double quatIXprev[4] = {0, 0, 0, 0};
 
   static constexpr char SD_0_SKEWED_PTG_FILE[] = "/mnt/sd0/conf/acsDeploymentConfirm";
   static constexpr char SD_1_SKEWED_PTG_FILE[] = "/mnt/sd1/conf/acsDeploymentConfirm";

mission/controller/acs/control/PtgCtrl.cpp

@@ -39,7 +39,7 @@ void PtgCtrl::ptgLaw(AcsParameters::PointingLawParameters *pointingLawParameters
   double qError[3] = {errorQuat[0], errorQuat[1], errorQuat[2]};
 
   double cInt = 2 * om * zeta;
-  double kInt = 2 * pow(om, 2);
+  double kInt = 2 * om * om;
 
   double qErrorLaw[3] = {0, 0, 0};
 
@@ -111,9 +111,13 @@ void PtgCtrl::ptgLaw(AcsParameters::PointingLawParameters *pointingLawParameters
   VectorOperations<double>::mulScalar(torqueRws, -1, torqueRws, 4);
 }
 
-void PtgCtrl::ptgNullspace(AcsParameters::PointingLawParameters *pointingLawParameters,
+void PtgCtrl::ptgNullspace(const bool allRwAvabilable,
+                           AcsParameters::PointingLawParameters *pointingLawParameters,
                            const int32_t speedRw0, const int32_t speedRw1, const int32_t speedRw2,
                            const int32_t speedRw3, double *rwTrqNs) {
+  if (not allRwAvabilable) {
+    return;
+  }
   // concentrate RW speeds as vector and convert to double
   double speedRws[4] = {static_cast<double>(speedRw0), static_cast<double>(speedRw1),
                         static_cast<double>(speedRw2), static_cast<double>(speedRw3)};

mission/controller/acs/control/PtgCtrl.h

@@ -33,7 +33,8 @@ class PtgCtrl {
   void ptgLaw(AcsParameters::PointingLawParameters *pointingLawParameters, const double *qError,
               const double *deltaRate, const double *rwPseudoInv, double *torqueRws);
 
-  void ptgNullspace(AcsParameters::PointingLawParameters *pointingLawParameters,
+  void ptgNullspace(const bool allRwAvabilable,
+                    AcsParameters::PointingLawParameters *pointingLawParameters,
                     const int32_t speedRw0, const int32_t speedRw1, const int32_t speedRw2,
                     const int32_t speedRw3, double *rwTrqNs);
 

mission/controller/acs/util/MathOperations.h

@@ -4,15 +4,12 @@
 #include <fsfw/src/fsfw/globalfunctions/constants.h>
 #include <fsfw/src/fsfw/globalfunctions/math/MatrixOperations.h>
 #include <fsfw/src/fsfw/globalfunctions/sign.h>
-#include <stdint.h>
-#include <string.h>
-#include <sys/time.h>
+#include <fsfw/src/fsfw/serviceinterface.h>
 
 #include <cmath>
+#include <cstring>
 #include <iostream>
 
-#include "fsfw/serviceinterface.h"
-
 template <typename T1, typename T2 = T1>
 class MathOperations {
  public:
@@ -46,7 +43,7 @@ class MathOperations {
   static void selectionSort(const T1 *matrix, T1 *result, uint8_t rowSize, uint8_t colSize) {
     int min_idx;
     T1 temp;
-    memcpy(result, matrix, rowSize * colSize * sizeof(*result));
+    std::memcpy(result, matrix, rowSize * colSize * sizeof(*result));
     // One by one move boundary of unsorted subarray
     for (int k = 0; k < rowSize; k++) {
       for (int i = 0; i < colSize - 1; i++) {

mission/controller/controllerdefinitions/AcsCtrlDefinitions.h

@@ -1,6 +1,7 @@
 #ifndef MISSION_CONTROLLER_CONTROLLERDEFINITIONS_ACSCTRLDEFINITIONS_H_
 #define MISSION_CONTROLLER_CONTROLLERDEFINITIONS_ACSCTRLDEFINITIONS_H_
 
+#include <common/config/eive/resultClassIds.h>
 #include <fsfw/datapoollocal/StaticLocalDataSet.h>
 #include <fsfw/datapoollocal/localPoolDefinitions.h>
 
@@ -8,6 +9,22 @@
 
 namespace acsctrl {
 
+static const uint8_t IF_ACS_CTRL_ID = CLASS_ID::ACS_CTRL;
+//! [EXPORT] : [COMMENT] File deletion failed and at least one file is still existent.
+static constexpr ReturnValue_t FILE_DELETION_FAILED =
+    returnvalue::makeCode(acsctrl::IF_ACS_CTRL_ID, 0);
+//! [EXPORT] : [COMMENT] Writing the TLE to the file has failed.
+static constexpr ReturnValue_t WRITE_FILE_FAILED =
+    returnvalue::makeCode(acsctrl::IF_ACS_CTRL_ID, 1);
+//! [EXPORT] : [COMMENT] Reading the TLE to the file has failed.
+static constexpr ReturnValue_t READ_FILE_FAILED = returnvalue::makeCode(acsctrl::IF_ACS_CTRL_ID, 2);
+//! [EXPORT] : [COMMENT] A single RW has failed.
+static constexpr ReturnValue_t SINGLE_RW_UNAVAILABLE =
+    returnvalue::makeCode(acsctrl::IF_ACS_CTRL_ID, 3);
+//! [EXPORT] : [COMMENT] Multiple RWs have failed.
+static constexpr ReturnValue_t MULTIPLE_RW_UNAVAILABLE =
+    returnvalue::makeCode(acsctrl::IF_ACS_CTRL_ID, 4);
+
 enum SetIds : uint32_t {
   MGM_SENSOR_DATA,
   MGM_PROCESSED_DATA,