First Version of ACS Controller #329
83
mission/controller/acs/ActuatorCmd.cpp
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83
mission/controller/acs/ActuatorCmd.cpp
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/*
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* ActuatorCmd.cpp
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*
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* Created on: 4 Aug 2022
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* Author: Robin Marquardt
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*/
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#include "ActuatorCmd.h"
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#include <math.h>
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#include <acs/util/MathOperations.h>
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#include <fsfw/src/fsfw/globalfunctions/constants.h>
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#include <fsfw/src/fsfw/globalfunctions/math/VectorOperations.h>
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#include <fsfw/src/fsfw/globalfunctions/math/MatrixOperations.h>
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#include <fsfw/src/fsfw/globalfunctions/math/QuaternionOperations.h>
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#include <acs/util/CholeskyDecomposition.h>
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ActuatorCmd::ActuatorCmd(AcsParameters *acsParameters_) {
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acsParameters = *acsParameters_;
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}
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ActuatorCmd::~ActuatorCmd(){
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}
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void ActuatorCmd::cmdSpeedToRws(const double *speedRw0, const double *speedRw1, const double *speedRw2,
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const double *speedRw3, const double *rwTrqIn, const double *rwTrqNS, double *rwCmdSpeed){
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using namespace Math;
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// Scaling the commanded torque to a maximum value
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double torque[4] = {0, 0, 0, 0};
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double maxTrq = acsParameters.rwHandlingParameters.maxTrq;
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VectorOperations<double>::add(rwTrqIn, rwTrqNS, torque, 4);
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double maxValue = 0;
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for (int i = 0; i < 4; i++) { //size of torque, always 4 ?
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if (abs(torque[i]) > maxValue) {
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maxValue = abs(torque[i]);
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}
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}
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if (maxValue > maxTrq) {
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double scalingFactor = maxTrq / maxValue;
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VectorOperations<double>::mulScalar(torque, scalingFactor, torque, 4);
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}
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// Calculating the commanded speed in RPM for every reaction wheel
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double speedRws[4] = {*speedRw0, *speedRw1, *speedRw2, *speedRw3};
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double deltaSpeed[4] = {0, 0, 0, 0};
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double commandTime = acsParameters.onBoardParams.sampleTime,
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inertiaWheel = acsParameters.rwHandlingParameters.inertiaWheel;
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double radToRpm = 60 / (2 * PI); // factor for conversion to RPM
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// W_RW = Torque_RW / I_RW * delta t [rad/s]
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double factor = commandTime / inertiaWheel * radToRpm;
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VectorOperations<double>::mulScalar(torque, factor, deltaSpeed, 4);
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VectorOperations<double>::add(speedRws, deltaSpeed, rwCmdSpeed, 4);
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}
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void ActuatorCmd::cmdDipolMtq(const double *dipolMoment, double *dipolMomentUnits) {
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// Convert to Unit frame
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MatrixOperations<double>::multiply(*acsParameters.magnetorquesParameter.inverseAlignment, dipolMoment, dipolMomentUnits, 3, 3, 1);
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// Scaling along largest element if dipol exceeds maximum
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double maxDipol = acsParameters.magnetorquesParameter.DipolMax;
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double maxValue = 0;
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for (int i = 0; i < 3; i++) {
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if (abs(dipolMomentUnits[i]) > maxDipol) {
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maxValue = abs(dipolMomentUnits[i]);
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}
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}
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if (maxValue > maxDipol) {
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double scalingFactor = maxDipol / maxValue;
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VectorOperations<double>::mulScalar(dipolMomentUnits, scalingFactor, dipolMomentUnits, 3);
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}
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}
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48
mission/controller/acs/ActuatorCmd.h
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48
mission/controller/acs/ActuatorCmd.h
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@ -0,0 +1,48 @@
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/*
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* ActuatorCmd.h
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*
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* Created on: 4 Aug 2022
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* Author: Robin Marquardt
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*/
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#ifndef ACTUATORCMD_H_
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#define ACTUATORCMD_H_
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#include "AcsParameters.h"
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#include "SensorProcessing.h"
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#include <acs/MultiplicativeKalmanFilter.h>
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#include <acs/SensorValues.h>
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#include <acs/OutputValues.h>
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class ActuatorCmd{
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public:
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ActuatorCmd(AcsParameters *acsParameters_); //Input mode ?
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virtual ~ActuatorCmd();
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/*
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* @brief: cmdSpeedToRws() will set the maximum possible torque for the reaction wheels, also
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* will calculate the needed revolutions per minute for the RWs, which will be given
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* as Input to the RWs
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* @param: rwTrqIn given torque from pointing controller
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* rwTrqNS Nullspace torque
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* rwCmdSpeed output revolutions per minute for every reaction wheel
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*/
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void cmdSpeedToRws(const double *speedRw0, const double *speedRw1, const double *speedRw2, const double *speedRw3,
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const double *rwTrqIn, const double *rwTrqNS, double *rwCmdSpeed);
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/*
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* @brief: cmdDipolMtq() gives the commanded dipol moment for the magnetorques
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*
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* @param: dipolMoment given dipol moment in spacecraft frame
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* dipolMomentUnits resulting dipol moment for every unit
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*/
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void cmdDipolMtq(const double *dipolMoment, double *dipolMomentUnits);
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protected:
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private:
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AcsParameters acsParameters;
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};
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#endif /* ACTUATORCMD_H_ */
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