First Version of ACS Controller #329
@ -8,6 +8,7 @@ AcsController::AcsController(object_id_t objectId)
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navigation(&acsParameters),
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actuatorCmd(&acsParameters),
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guidance(&acsParameters),
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safeCtrl(&acsParameters),
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detumble(&acsParameters),
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ptgCtrl(&acsParameters),
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detumbleCounter{0},
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@ -35,7 +36,7 @@ void AcsController::performControlOperation() {
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if (mode != MODE_OFF) {
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switch (submode) {
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case SUBMODE_SAFE:
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// performSafe();
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performSafe();
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break;
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case SUBMODE_DETUMBLE:
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@ -72,7 +73,66 @@ void AcsController::performControlOperation() {
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// DEBUG END
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}
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void AcsController::performSafe() {}
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void AcsController::performSafe() {
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// Concept: SAFE MODE WITH MEKF
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// -do the sensor processing, maybe is does make more sense do call this class function in
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// another place since we have to do it for every mode regardless of safe or not
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ACS::SensorValues sensorValues;
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ACS::OutputValues outputValues;
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timeval now; // We need to give the actual time here
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sensorProcessing.process(now, &sensorValues, &outputValues, &acsParameters);
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ReturnValue_t validMekf;
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navigation.useMekf(&sensorValues, &outputValues, &validMekf); // DOES THIS WORK WITH VALID?
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// Give desired satellite rate and sun direction to align
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double satRateSafe[3] = {0, 0, 0}, sunTargetDir[3] = {0, 0, 0};
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guidance.getTargetParamsSafe(sunTargetDir, satRateSafe);
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// IF MEKF is working
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double magMomMtq[3] = {0, 0, 0};
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bool magMomMtqValid = false;
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if (validMekf == returnvalue::OK) {
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safeCtrl.safeMekf(now, (outputValues.quatMekfBJ), &(outputValues.quatMekfBJValid),
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(outputValues.magFieldModel), &(outputValues.magFieldModelValid),
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(outputValues.sunDirModel), &(outputValues.sunDirModelValid),
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(outputValues.satRateMekf), &(outputValues.satRateMekfValid), sunTargetDir,
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satRateSafe, magMomMtq, &magMomMtqValid);
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} else {
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safeCtrl.safeNoMekf(now, outputValues.sunDirEst, &outputValues.sunDirEstValid,
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outputValues.sunVectorDerivative, &(outputValues.sunVectorDerivativeValid),
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outputValues.magFieldEst, &(outputValues.magFieldEstValid),
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outputValues.magneticFieldVectorDerivative,
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&(outputValues.magneticFieldVectorDerivativeValid), sunTargetDir,
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satRateSafe, magMomMtq, &magMomMtqValid);
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}
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double dipolCmdUnits[3] = {0, 0, 0};
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actuatorCmd.cmdDipolMtq(magMomMtq, dipolCmdUnits);
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// Detumble check and switch
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if (outputValues.satRateMekfValid && VectorOperations<double>::norm(outputValues.satRateMekf, 3) >
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acsParameters.detumbleParameter.omegaDetumbleStart) {
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detumbleCounter++;
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}
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else if (outputValues.satRateEstValid &&
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VectorOperations<double>::norm(outputValues.satRateEst, 3) >
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acsParameters.detumbleParameter.omegaDetumbleStart) {
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detumbleCounter++;
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}
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else {
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detumbleCounter = 0;
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}
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if (detumbleCounter > acsParameters.detumbleParameter.detumblecounter) {
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submode = SUBMODE_DETUMBLE;
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detumbleCounter = 0;
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}
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// commanding.magnetorquesDipol();
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}
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void AcsController::performDetumble() {
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ACS::SensorValues sensorValues;
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@ -293,6 +353,8 @@ void AcsController::copySusData() {
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PoolReadGuard pg(&susSets[9]);
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if (pg.getReadResult() == returnvalue::OK) {
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std::memcpy(susData.sus9.value, susSets[9].channels.value, 6 * sizeof(uint16_t));
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sif::debug << susData.sus9.isValid() << std::endl;
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sif::debug << susSets[9].channels.isValid() << std::endl;
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}
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}
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{
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@ -11,6 +11,7 @@
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#include "acs/SensorProcessing.h"
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#include "acs/control/Detumble.h"
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#include "acs/control/PtgCtrl.h"
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#include "acs/control/SafeCtrl.h"
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#include "controllerdefinitions/AcsCtrlDefinitions.h"
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#include "fsfw_hal/devicehandlers/MgmLIS3MDLHandler.h"
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#include "fsfw_hal/devicehandlers/MgmRM3100Handler.h"
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@ -29,7 +30,6 @@ class AcsController : public ExtendedControllerBase {
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static const Submode_t SUBMODE_PTG_NADIR = 5;
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protected:
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void performSafe();
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void performDetumble();
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void performPointingCtrl();
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@ -41,6 +41,7 @@ class AcsController : public ExtendedControllerBase {
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ActuatorCmd actuatorCmd;
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Guidance guidance;
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SafeCtrl safeCtrl;
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Detumble detumble;
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PtgCtrl ptgCtrl;
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@ -6,182 +6,172 @@
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*/
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#include "SafeCtrl.h"
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#include "../util/MathOperations.h"
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#include <math.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 <math.h>
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#include "../util/MathOperations.h"
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SafeCtrl::SafeCtrl(AcsParameters *acsParameters_){
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loadAcsParameters(acsParameters_);
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MatrixOperations<double>::multiplyScalar(*(inertiaEIVE->inertiaMatrix), 10, *gainMatrixInertia, 3, 3);
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SafeCtrl::SafeCtrl(AcsParameters *acsParameters_) {
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loadAcsParameters(acsParameters_);
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MatrixOperations<double>::multiplyScalar(*(inertiaEIVE->inertiaMatrix), 10, *gainMatrixInertia, 3,
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3);
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}
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SafeCtrl::~SafeCtrl(){
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SafeCtrl::~SafeCtrl() {}
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}
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void SafeCtrl::loadAcsParameters(AcsParameters *acsParameters_){
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safeModeControllerParameters = &(acsParameters_->safeModeControllerParameters);
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inertiaEIVE = &(acsParameters_->inertiaEIVE);
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void SafeCtrl::loadAcsParameters(AcsParameters *acsParameters_) {
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safeModeControllerParameters = &(acsParameters_->safeModeControllerParameters);
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inertiaEIVE = &(acsParameters_->inertiaEIVE);
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}
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ReturnValue_t SafeCtrl::safeMekf(timeval now, double *quatBJ, bool *quatBJValid,
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double *magFieldModel, bool *magFieldModelValid,
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double *sunDirModel, bool *sunDirModelValid,
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double *satRateMekf, bool *rateMekfValid,
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double *sunDirRef, double *satRatRef,
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double *outputMagMomB, bool *outputValid){
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double *magFieldModel, bool *magFieldModelValid,
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double *sunDirModel, bool *sunDirModelValid, double *satRateMekf,
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bool *rateMekfValid, double *sunDirRef, double *satRatRef,
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double *outputMagMomB, bool *outputValid) {
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if (!(*quatBJValid) || !(*magFieldModelValid) || !(*sunDirModelValid) || !(*rateMekfValid)) {
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*outputValid = false;
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return SAFECTRL_MEKF_INPUT_INVALID;
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}
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if ( !(*quatBJValid) || !(*magFieldModelValid) || !(*sunDirModelValid) ||
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!(*rateMekfValid)) {
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*outputValid = false;
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return SAFECTRL_MEKF_INPUT_INVALID;
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}
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double kRate = 0, kAlign = 0;
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kRate = safeModeControllerParameters->k_rate_mekf;
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kAlign = safeModeControllerParameters->k_align_mekf;
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double kRate = 0, kAlign = 0;
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kRate = safeModeControllerParameters->k_rate_mekf;
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kAlign = safeModeControllerParameters->k_align_mekf;
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// Calc sunDirB ,magFieldB with mekf output and model
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double dcmBJ[3][3] = {{0, 0, 0}, {0, 0, 0}, {0, 0, 0}};
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MathOperations<double>::dcmFromQuat(quatBJ, *dcmBJ);
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double sunDirB[3] = {0, 0, 0}, magFieldB[3] = {0, 0, 0};
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MatrixOperations<double>::multiply(*dcmBJ, sunDirModel, sunDirB, 3, 3, 1);
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MatrixOperations<double>::multiply(*dcmBJ, magFieldModel, magFieldB, 3, 3, 1);
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// Calc sunDirB ,magFieldB with mekf output and model
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double dcmBJ[3][3] = {{0,0,0},{0,0,0},{0,0,0}};
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MathOperations<double>::dcmFromQuat(quatBJ, *dcmBJ);
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double sunDirB[3] = {0,0,0}, magFieldB[3] = {0,0,0};
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MatrixOperations<double>::multiply(*dcmBJ, sunDirModel, sunDirB, 3, 3, 1);
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MatrixOperations<double>::multiply(*dcmBJ, magFieldModel, magFieldB, 3, 3, 1);
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double crossSun[3] = {0, 0, 0};
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double crossSun[3] = {0, 0, 0};
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VectorOperations<double>::cross(sunDirRef, sunDirB, crossSun);
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double normCrossSun = VectorOperations<double>::norm(crossSun, 3);
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VectorOperations<double>::cross(sunDirRef, sunDirB, crossSun);
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double normCrossSun = VectorOperations<double>::norm(crossSun, 3);
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// calc angle alpha between sunDirRef and sunDIr
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double alpha = 0, dotSun = 0;
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dotSun = VectorOperations<double>::dot(sunDirRef, sunDirB);
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alpha = acos(dotSun);
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// calc angle alpha between sunDirRef and sunDIr
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double alpha = 0, dotSun = 0;
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dotSun = VectorOperations<double>::dot(sunDirRef, sunDirB);
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alpha = acos(dotSun);
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// Law Torque calculations
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double torqueCmd[3] = {0, 0, 0}, torqueAlign[3] = {0, 0, 0}, torqueRate[3] = {0, 0, 0},
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torqueAll[3] = {0, 0, 0};
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// Law Torque calculations
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double torqueCmd[3] = {0, 0, 0}, torqueAlign[3] = {0, 0, 0},
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torqueRate[3] = {0, 0, 0}, torqueAll[3] = {0, 0, 0};
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double scalarFac = 0;
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scalarFac = kAlign * alpha / normCrossSun;
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VectorOperations<double>::mulScalar(crossSun, scalarFac, torqueAlign, 3);
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double scalarFac = 0;
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scalarFac = kAlign * alpha / normCrossSun;
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VectorOperations<double>::mulScalar(crossSun, scalarFac, torqueAlign, 3);
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double rateSafeMode[3] = {0, 0, 0};
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VectorOperations<double>::subtract(satRateMekf, satRatRef, rateSafeMode, 3);
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VectorOperations<double>::mulScalar(rateSafeMode, -kRate, torqueRate, 3);
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double rateSafeMode[3] = {0,0,0};
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VectorOperations<double>::subtract(satRateMekf, satRatRef, rateSafeMode, 3);
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VectorOperations<double>::mulScalar(rateSafeMode, -kRate, torqueRate, 3);
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VectorOperations<double>::add(torqueRate, torqueAlign, torqueAll, 3);
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// Adding factor of inertia for axes
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MatrixOperations<double>::multiply(*gainMatrixInertia, torqueAll, torqueCmd, 3, 3, 1);
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VectorOperations<double>::add(torqueRate, torqueAlign, torqueAll, 3);
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// Adding factor of inertia for axes
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MatrixOperations<double>::multiply(*gainMatrixInertia, torqueAll, torqueCmd, 3, 3, 1);
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// MagMom B (orthogonal torque)
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double torqueMgt[3] = {0,0,0};
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VectorOperations<double>::cross(magFieldB, torqueCmd, torqueMgt);
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double normMag = VectorOperations<double>::norm(magFieldB, 3);
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VectorOperations<double>::mulScalar(torqueMgt, 1/pow(normMag,2), outputMagMomB, 3);
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*outputValid = true;
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return returnvalue::OK;
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// MagMom B (orthogonal torque)
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double torqueMgt[3] = {0, 0, 0};
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VectorOperations<double>::cross(magFieldB, torqueCmd, torqueMgt);
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double normMag = VectorOperations<double>::norm(magFieldB, 3);
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VectorOperations<double>::mulScalar(torqueMgt, 1 / pow(normMag, 2), outputMagMomB, 3);
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*outputValid = true;
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return returnvalue::OK;
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}
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// Will be the version in worst case scenario in event of no working MEKF (nor RMUs)
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void SafeCtrl::safeNoMekf(timeval now, double *susDirB, bool *susDirBValid,
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double *sunRateB, bool *sunRateBValid,
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double *magFieldB, bool *magFieldBValid,
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double *magRateB, bool *magRateBValid,
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double *sunDirRef, double *satRateRef,
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double *outputMagMomB, bool *outputValid){
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void SafeCtrl::safeNoMekf(timeval now, double *susDirB, bool *susDirBValid, double *sunRateB,
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bool *sunRateBValid, double *magFieldB, bool *magFieldBValid,
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double *magRateB, bool *magRateBValid, double *sunDirRef,
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double *satRateRef, double *outputMagMomB, bool *outputValid) {
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// Check for invalid Inputs
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if (!susDirBValid || !magFieldBValid || !magRateBValid) {
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*outputValid = false;
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return;
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}
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// Check for invalid Inputs
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if ( !susDirBValid || !magFieldBValid || !magRateBValid) {
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*outputValid = false;
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return;
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}
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// normalize sunDir and magDir
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double magDirB[3] = {0, 0, 0};
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VectorOperations<double>::normalize(magFieldB, magDirB, 3);
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VectorOperations<double>::normalize(susDirB, susDirB, 3);
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// normalize sunDir and magDir
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double magDirB[3] = {0, 0, 0};
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VectorOperations<double>::normalize(magFieldB, magDirB, 3);
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VectorOperations<double>::normalize(susDirB, susDirB, 3);
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// Cosinus angle between sunDir and magDir
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double cosAngleSunMag = VectorOperations<double>::dot(magDirB, susDirB);
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// Cosinus angle between sunDir and magDir
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double cosAngleSunMag = VectorOperations<double>::dot(magDirB, susDirB);
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// Rate parallel to sun direction and magnetic field direction
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double rateParaSun = 0, rateParaMag = 0;
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double dotSunRateMag = 0, dotmagRateSun = 0, rateFactor = 0;
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dotSunRateMag = VectorOperations<double>::dot(sunRateB, magDirB);
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dotmagRateSun = VectorOperations<double>::dot(magRateB, susDirB);
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rateFactor = 1 - pow(cosAngleSunMag, 2);
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rateParaSun = (dotmagRateSun + cosAngleSunMag * dotSunRateMag) / rateFactor;
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rateParaMag = (dotSunRateMag + cosAngleSunMag * dotmagRateSun) / rateFactor;
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// Rate parallel to sun direction and magnetic field direction
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double rateParaSun = 0, rateParaMag = 0;
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double dotSunRateMag = 0, dotmagRateSun = 0,
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rateFactor = 0;
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dotSunRateMag = VectorOperations<double>::dot(sunRateB, magDirB);
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dotmagRateSun = VectorOperations<double>::dot(magRateB, susDirB);
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rateFactor = 1 - pow(cosAngleSunMag,2);
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rateParaSun = ( dotmagRateSun + cosAngleSunMag * dotSunRateMag ) / rateFactor;
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rateParaMag = ( dotSunRateMag + cosAngleSunMag * dotmagRateSun ) / rateFactor;
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// Full rate or estimate
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double estSatRate[3] = {0, 0, 0};
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||||
double estSatRateMag[3] = {0, 0, 0}, estSatRateSun[3] = {0, 0, 0};
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VectorOperations<double>::mulScalar(susDirB, rateParaSun, estSatRateSun, 3);
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||||
VectorOperations<double>::add(sunRateB, estSatRateSun, estSatRateSun, 3);
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VectorOperations<double>::mulScalar(magDirB, rateParaMag, estSatRateMag, 3);
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VectorOperations<double>::add(magRateB, estSatRateMag, estSatRateMag, 3);
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VectorOperations<double>::add(estSatRateSun, estSatRateMag, estSatRate, 3);
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VectorOperations<double>::mulScalar(estSatRate, 0.5, estSatRate, 3);
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||||
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||||
// Full rate or estimate
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||||
double estSatRate[3] = {0, 0, 0};
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||||
double estSatRateMag[3] = {0, 0, 0}, estSatRateSun[3] = {0, 0, 0};
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||||
VectorOperations<double>::mulScalar(susDirB, rateParaSun, estSatRateSun, 3);
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||||
VectorOperations<double>::add(sunRateB, estSatRateSun, estSatRateSun, 3);
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||||
VectorOperations<double>::mulScalar(magDirB, rateParaMag, estSatRateMag, 3);
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||||
VectorOperations<double>::add(magRateB, estSatRateMag, estSatRateMag, 3);
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||||
VectorOperations<double>::add(estSatRateSun, estSatRateMag, estSatRate, 3);
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||||
VectorOperations<double>::mulScalar(estSatRate, 0.5, estSatRate, 3);
|
||||
/* Only valid if angle between sun direction and magnetic field direction
|
||||
is sufficiently large */
|
||||
|
||||
/* Only valid if angle between sun direction and magnetic field direction
|
||||
is sufficiently large */
|
||||
double sinAngle = 0;
|
||||
sinAngle = sin(acos(cos(cosAngleSunMag)));
|
||||
|
||||
double sinAngle = 0;
|
||||
sinAngle = sin(acos(cos(cosAngleSunMag)));
|
||||
if (!(sinAngle > sin(safeModeControllerParameters->sunMagAngleMin * M_PI / 180))) {
|
||||
return;
|
||||
}
|
||||
|
||||
if ( !(sinAngle > sin( safeModeControllerParameters->sunMagAngleMin * M_PI / 180))) {
|
||||
return;
|
||||
}
|
||||
// Rate for Torque Calculation
|
||||
double diffRate[3] = {0, 0, 0}; /* ADD TO MONITORING */
|
||||
VectorOperations<double>::subtract(estSatRate, satRateRef, diffRate, 3);
|
||||
|
||||
// Rate for Torque Calculation
|
||||
double diffRate[3] = {0, 0, 0}; /* ADD TO MONITORING */
|
||||
VectorOperations<double>::subtract(estSatRate, satRateRef, diffRate, 3);
|
||||
// Torque Align calculation
|
||||
double kRateNoMekf = 0, kAlignNoMekf = 0;
|
||||
kRateNoMekf = safeModeControllerParameters->k_rate_no_mekf;
|
||||
kAlignNoMekf = safeModeControllerParameters->k_align_no_mekf;
|
||||
|
||||
// Torque Align calculation
|
||||
double kRateNoMekf = 0, kAlignNoMekf = 0;
|
||||
kRateNoMekf = safeModeControllerParameters->k_rate_no_mekf;
|
||||
kAlignNoMekf = safeModeControllerParameters->k_align_no_mekf;
|
||||
double cosAngleAlignErr = VectorOperations<double>::dot(sunDirRef, susDirB);
|
||||
double crossSusSunRef[3] = {0, 0, 0};
|
||||
VectorOperations<double>::cross(sunDirRef, susDirB, crossSusSunRef);
|
||||
double sinAngleAlignErr = VectorOperations<double>::norm(crossSusSunRef, 3);
|
||||
|
||||
double cosAngleAlignErr = VectorOperations<double>::dot(sunDirRef, susDirB);
|
||||
double crossSusSunRef[3] = {0, 0, 0};
|
||||
VectorOperations<double>::cross(sunDirRef, susDirB, crossSusSunRef);
|
||||
double sinAngleAlignErr = VectorOperations<double>::norm(crossSusSunRef, 3);
|
||||
double torqueAlign[3] = {0, 0, 0};
|
||||
double angleAlignErr = acos(cosAngleAlignErr);
|
||||
double torqueAlignFactor = kAlignNoMekf * angleAlignErr / sinAngleAlignErr;
|
||||
VectorOperations<double>::mulScalar(crossSusSunRef, torqueAlignFactor, torqueAlign, 3);
|
||||
|
||||
double torqueAlign[3] = {0, 0, 0};
|
||||
double angleAlignErr = acos(cosAngleAlignErr);
|
||||
double torqueAlignFactor = kAlignNoMekf * angleAlignErr / sinAngleAlignErr;
|
||||
VectorOperations<double>::mulScalar(crossSusSunRef, torqueAlignFactor, torqueAlign, 3);
|
||||
// Torque Rate Calculations
|
||||
double torqueRate[3] = {0, 0, 0};
|
||||
VectorOperations<double>::mulScalar(diffRate, -kRateNoMekf, torqueRate, 3);
|
||||
|
||||
//Torque Rate Calculations
|
||||
double torqueRate[3] = {0, 0, 0};
|
||||
VectorOperations<double>::mulScalar(diffRate, -kRateNoMekf, torqueRate, 3);
|
||||
// Final torque
|
||||
double torqueB[3] = {0, 0, 0}, torqueAlignRate[3] = {0, 0, 0};
|
||||
VectorOperations<double>::add(torqueRate, torqueAlign, torqueAlignRate, 3);
|
||||
MatrixOperations<double>::multiply(*(inertiaEIVE->inertiaMatrix), torqueAlignRate, torqueB, 3, 3,
|
||||
1);
|
||||
|
||||
//Final torque
|
||||
double torqueB[3] = {0, 0, 0}, torqueAlignRate[3] = {0, 0, 0};
|
||||
VectorOperations<double>::add(torqueRate, torqueAlign, torqueAlignRate, 3);
|
||||
MatrixOperations<double>::multiply(*(inertiaEIVE->inertiaMatrix), torqueAlignRate, torqueB, 3, 3, 1);
|
||||
// Magnetic moment
|
||||
double magMomB[3] = {0, 0, 0};
|
||||
double crossMagFieldTorque[3] = {0, 0, 0};
|
||||
VectorOperations<double>::cross(magFieldB, torqueB, crossMagFieldTorque);
|
||||
double magMomFactor = pow(VectorOperations<double>::norm(magFieldB, 3), 2);
|
||||
VectorOperations<double>::mulScalar(crossMagFieldTorque, 1 / magMomFactor, magMomB, 3);
|
||||
|
||||
//Magnetic moment
|
||||
double magMomB[3] = {0, 0, 0};
|
||||
double crossMagFieldTorque[3] = {0, 0, 0};
|
||||
VectorOperations<double>::cross(magFieldB, torqueB, crossMagFieldTorque);
|
||||
double magMomFactor = pow( VectorOperations<double>::norm(magFieldB, 3), 2 );
|
||||
VectorOperations<double>::mulScalar(crossMagFieldTorque, 1/magMomFactor, magMomB, 3);
|
||||
|
||||
outputMagMomB[0] = magMomB[0];
|
||||
outputMagMomB[1] = magMomB[1];
|
||||
outputMagMomB[2] = magMomB[2];
|
||||
|
||||
*outputValid = true;
|
||||
outputMagMomB[0] = magMomB[0];
|
||||
outputMagMomB[1] = magMomB[1];
|
||||
outputMagMomB[2] = magMomB[2];
|
||||
|
||||
*outputValid = true;
|
||||
}
|
||||
|
||||
|
||||
|
||||
@ -8,57 +8,46 @@
|
||||
#ifndef SAFECTRL_H_
|
||||
#define SAFECTRL_H_
|
||||
|
||||
#include "../SensorValues.h"
|
||||
#include "../OutputValues.h"
|
||||
#include "../AcsParameters.h"
|
||||
#include "../config/classIds.h"
|
||||
#include <string.h>
|
||||
#include <stdio.h>
|
||||
#include <string.h>
|
||||
#include <time.h>
|
||||
#include <fsfw/returnvalues/HasReturnvaluesIF.h>
|
||||
|
||||
#include "../AcsParameters.h"
|
||||
#include "../OutputValues.h"
|
||||
#include "../SensorValues.h"
|
||||
#include "../config/classIds.h"
|
||||
|
||||
class SafeCtrl{
|
||||
class SafeCtrl {
|
||||
public:
|
||||
SafeCtrl(AcsParameters *acsParameters_);
|
||||
virtual ~SafeCtrl();
|
||||
|
||||
public:
|
||||
static const uint8_t INTERFACE_ID = CLASS_ID::SAFE;
|
||||
static const ReturnValue_t SAFECTRL_MEKF_INPUT_INVALID = MAKE_RETURN_CODE(0x01);
|
||||
|
||||
SafeCtrl(AcsParameters *acsParameters_);
|
||||
virtual ~SafeCtrl();
|
||||
void loadAcsParameters(AcsParameters *acsParameters_);
|
||||
|
||||
static const uint8_t INTERFACE_ID = CLASS_ID::SAFE;
|
||||
static const ReturnValue_t SAFECTRL_MEKF_INPUT_INVALID = MAKE_RETURN_CODE(0x01);
|
||||
ReturnValue_t safeMekf(timeval now, double *quatBJ, bool *quatBJValid, double *magFieldModel,
|
||||
bool *magFieldModelValid, double *sunDirModel, bool *sunDirModelValid,
|
||||
double *satRateMekf, bool *rateMekfValid, double *sunDirRef,
|
||||
double *satRatRef, // From Guidance (!)
|
||||
double *outputMagMomB, bool *outputValid);
|
||||
|
||||
void loadAcsParameters(AcsParameters *acsParameters_);
|
||||
void safeNoMekf(timeval now, double *susDirB, bool *susDirBValid, double *sunRateB,
|
||||
bool *sunRateBValid, double *magFieldB, bool *magFieldBValid, double *magRateB,
|
||||
bool *magRateBValid, double *sunDirRef, double *satRateRef, double *outputMagMomB,
|
||||
bool *outputValid);
|
||||
|
||||
ReturnValue_t safeMekf(timeval now, double *quatBJ, bool *quatBJValid,
|
||||
double *magFieldModel, bool *magFieldModelValid,
|
||||
double *sunDirModel, bool *sunDirModelValid,
|
||||
double *satRateMekf, bool *rateMekfValid,
|
||||
double *sunDirRef, double *satRatRef, // From Guidance (!)
|
||||
double *outputMagMomB, bool *outputValid);
|
||||
void idleSunPointing(); // with reaction wheels
|
||||
|
||||
void safeNoMekf(timeval now, double *susDirB, bool *susDirBValid,
|
||||
double *sunRateB, bool *sunRateBValid,
|
||||
double *magFieldB, bool *magFieldBValid,
|
||||
double *magRateB, bool *magRateBValid,
|
||||
double *sunDirRef, double *satRateRef,
|
||||
double *outputMagMomB, bool *outputValid);
|
||||
|
||||
void idleSunPointing(); // with reaction wheels
|
||||
|
||||
protected:
|
||||
|
||||
private:
|
||||
AcsParameters::SafeModeControllerParameters* safeModeControllerParameters;
|
||||
AcsParameters::InertiaEIVE* inertiaEIVE;
|
||||
double gainMatrixInertia[3][3];
|
||||
|
||||
double magFieldBState[3];
|
||||
timeval magFieldBStateTime;
|
||||
protected:
|
||||
private:
|
||||
AcsParameters::SafeModeControllerParameters *safeModeControllerParameters;
|
||||
AcsParameters::InertiaEIVE *inertiaEIVE;
|
||||
double gainMatrixInertia[3][3];
|
||||
|
||||
double magFieldBState[3];
|
||||
timeval magFieldBStateTime;
|
||||
};
|
||||
|
||||
|
||||
|
||||
#endif /* ACS_CONTROL_SAFECTRL_H_ */
|
||||
|
||||
|
||||
Loading…
Reference in New Issue
Block a user