Fixes for Pointing Modes #851
@ -1,15 +1,5 @@
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#include "Guidance.h"
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#include <fsfw/datapool/PoolReadGuard.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 <mission/controller/acs/util/MathOperations.h>
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#include <cmath>
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#include <filesystem>
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#include <string>
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Guidance::Guidance(AcsParameters *acsParameters_) { acsParameters = acsParameters_; }
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Guidance::~Guidance() {}
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@ -455,44 +445,16 @@ void Guidance::comparePtg(double currentQuat[4], double currentSatRotRate[3], do
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}
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void Guidance::targetRotationRate(const int8_t timeElapsedMax, const double timeDelta,
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double quatInertialTarget[4], double *refSatRate) {
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//-------------------------------------------------------------------------------------
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// Calculation of target rotation rate
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//-------------------------------------------------------------------------------------
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if (VectorOperations<double>::norm(savedQuaternion, 4) == 0) {
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std::memcpy(savedQuaternion, quatInertialTarget, sizeof(savedQuaternion));
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double quatIX[4], double *refSatRate) {
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if (VectorOperations<double>::norm(quatIXprev, 4) == 0) {
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std::memcpy(quatIXprev, quatIX, sizeof(quatIXprev));
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}
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if (timeDelta < timeElapsedMax and timeDelta != 0.0) {
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double q[4] = {0, 0, 0, 0}, qS[4] = {0, 0, 0, 0};
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QuaternionOperations::inverse(quatInertialTarget, q);
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QuaternionOperations::inverse(savedQuaternion, qS);
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double qDiff[4] = {0, 0, 0, 0};
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VectorOperations<double>::subtract(q, qS, qDiff, 4);
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VectorOperations<double>::mulScalar(qDiff, 1. / timeDelta, qDiff, 4);
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double tgtQuatVec[3] = {q[0], q[1], q[2]};
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double qDiffVec[3] = {qDiff[0], qDiff[1], qDiff[2]};
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double sum1[3] = {0, 0, 0}, sum2[3] = {0, 0, 0}, sum3[3] = {0, 0, 0}, sum[3] = {0, 0, 0};
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VectorOperations<double>::cross(tgtQuatVec, qDiffVec, sum1);
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VectorOperations<double>::mulScalar(tgtQuatVec, qDiff[3], sum2, 3);
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VectorOperations<double>::mulScalar(qDiffVec, q[3], sum3, 3);
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VectorOperations<double>::add(sum1, sum2, sum, 3);
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VectorOperations<double>::subtract(sum, sum3, sum, 3);
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double omegaRefNew[3] = {0, 0, 0};
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VectorOperations<double>::mulScalar(sum, -2, omegaRefNew, 3);
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VectorOperations<double>::mulScalar(omegaRefNew, 2, refSatRate, 3);
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VectorOperations<double>::subtract(refSatRate, omegaRefSaved, refSatRate, 3);
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omegaRefSaved[0] = omegaRefNew[0];
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omegaRefSaved[1] = omegaRefNew[1];
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omegaRefSaved[2] = omegaRefNew[2];
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if (not timeDelta != 0.0) {
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QuaternionOperations::rotationFromQuaternions(quatIX, quatIXprev, timeDelta, refSatRate);
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} else {
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refSatRate[0] = 0;
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refSatRate[1] = 0;
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refSatRate[2] = 0;
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std::memcpy(refSatRate, ZERO_VEC3, sizeof(refSatRate));
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}
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std::memcpy(savedQuaternion, quatInertialTarget, sizeof(savedQuaternion));
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std::memcpy(quatIXprev, quatIX, sizeof(quatIXprev));
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}
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ReturnValue_t Guidance::getDistributionMatrixRw(ACS::SensorValues *sensorValues,
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@ -506,22 +468,27 @@ ReturnValue_t Guidance::getDistributionMatrixRw(ACS::SensorValues *sensorValues,
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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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std::memcpy(rwPseudoInv, acsParameters->rwMatrices.without1, 12 * sizeof(double));
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return returnvalue::OK;
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std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverseWithoutRW1,
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12 * sizeof(double));
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return SINGLE_RW_UNAVAILABLE;
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} else if (rw1valid and not rw2valid and rw3valid and rw4valid) {
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std::memcpy(rwPseudoInv, acsParameters->rwMatrices.without2, 12 * sizeof(double));
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return returnvalue::OK;
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std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverseWithoutRW2,
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12 * sizeof(double));
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return SINGLE_RW_UNAVAILABLE;
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} else if (rw1valid and rw2valid and not rw3valid and rw4valid) {
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std::memcpy(rwPseudoInv, acsParameters->rwMatrices.without3, 12 * sizeof(double));
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return returnvalue::OK;
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std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverseWithoutRW3,
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12 * sizeof(double));
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return SINGLE_RW_UNAVAILABLE;
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} else if (rw1valid and rw2valid and rw3valid and not rw4valid) {
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std::memcpy(rwPseudoInv, acsParameters->rwMatrices.without4, 12 * sizeof(double));
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return returnvalue::OK;
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} else {
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return returnvalue::FAILED;
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std::memcpy(rwPseudoInv, acsParameters->rwMatrices.pseudoInverseWithoutRW4,
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12 * sizeof(double));
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return SINGLE_RW_UNAVAILABLE;
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}
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return MULTIPLE_RW_UNAVAILABLE;
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}
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void Guidance::resetValues() { std::memcpy(quatIXprev, ZERO_VEC4, sizeof(quatIXprev)); }
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void Guidance::getTargetParamsSafe(double sunTargetSafe[3]) {
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std::error_code e;
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if (not std::filesystem::exists(SD_0_SKEWED_PTG_FILE, e) or
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@ -1,9 +1,18 @@
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#ifndef GUIDANCE_H_
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#define GUIDANCE_H_
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#include <fsfw/datapool/PoolReadGuard.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 <mission/controller/acs/util/MathOperations.h>
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#include <mission/controller/controllerdefinitions/AcsCtrlDefinitions.h>
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#include <time.h>
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#include "../controllerdefinitions/AcsCtrlDefinitions.h"
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#include <cmath>
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#include <filesystem>
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#include <string>
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#include "AcsParameters.h"
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#include "SensorValues.h"
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@ -14,6 +23,7 @@ class Guidance {
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void getTargetParamsSafe(double sunTargetSafe[3]);
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ReturnValue_t solarArrayDeploymentComplete();
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void resetValues();
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// Function to get the target quaternion and reference rotation rate from gps position and
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// position of the ground station
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@ -56,12 +66,21 @@ class Guidance {
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// reation wheel maybe can be done in "commanding.h"
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ReturnValue_t getDistributionMatrixRw(ACS::SensorValues *sensorValues, double *rwPseudoInv);
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//! [EXPORT] : [COMMENT] A single RW has failed.
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static constexpr ReturnValue_t SINGLE_RW_UNAVAILABLE =
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returnvalue::makeCode(acsctrl::IF_ACS_CTRL_ID, 3);
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//! [EXPORT] : [COMMENT] Multiple RWs have failed.
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static constexpr ReturnValue_t MULTIPLE_RW_UNAVAILABLE =
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returnvalue::makeCode(acsctrl::IF_ACS_CTRL_ID, 4);
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private:
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const AcsParameters *acsParameters;
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static constexpr double ZERO_VEC3[3] = {0, 0, 0};
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static constexpr double ZERO_VEC4[3] = {0, 0, 0, 0};
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bool strBlindAvoidFlag = false;
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double savedQuaternion[4] = {0, 0, 0, 0};
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double omegaRefSaved[3] = {0, 0, 0};
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double quatIXprev[4] = {0, 0, 0, 0};
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static constexpr char SD_0_SKEWED_PTG_FILE[] = "/mnt/sd0/conf/acsDeploymentConfirm";
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static constexpr char SD_1_SKEWED_PTG_FILE[] = "/mnt/sd1/conf/acsDeploymentConfirm";
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