eive-obsw/mission/controller/acs/control/SafeCtrl.cpp
2023-03-07 10:04:04 +01:00

159 lines
7.2 KiB
C++

#include "SafeCtrl.h"
#include <fsfw/globalfunctions/constants.h>
#include <fsfw/globalfunctions/math/MatrixOperations.h>
#include <fsfw/globalfunctions/math/QuaternionOperations.h>
#include <fsfw/globalfunctions/math/VectorOperations.h>
#include <math.h>
#include "../util/MathOperations.h"
SafeCtrl::SafeCtrl(AcsParameters *acsParameters_) { acsParameters = acsParameters_; }
SafeCtrl::~SafeCtrl() {}
ReturnValue_t SafeCtrl::safeMekf(timeval now, double *quatBJ, bool quatBJValid,
double *magFieldModel, bool magFieldModelValid,
double *sunDirModel, bool sunDirModelValid, double *satRateMekf,
bool rateMekfValid, double *sunDirRef, double *satRatRef,
double *outputAngle, double *outputMagMomB) {
if (!quatBJValid || !magFieldModelValid || !sunDirModelValid || !rateMekfValid) {
return SAFECTRL_MEKF_INPUT_INVALID;
}
double kRate = acsParameters->safeModeControllerParameters.k_rate_mekf;
double kAlign = acsParameters->safeModeControllerParameters.k_align_mekf;
// Calc sunDirB ,magFieldB with mekf output and model
double dcmBJ[3][3] = {{0, 0, 0}, {0, 0, 0}, {0, 0, 0}};
MathOperations<double>::dcmFromQuat(quatBJ, *dcmBJ);
double sunDirB[3] = {0, 0, 0}, magFieldB[3] = {0, 0, 0};
MatrixOperations<double>::multiply(*dcmBJ, sunDirModel, sunDirB, 3, 3, 1);
MatrixOperations<double>::multiply(*dcmBJ, magFieldModel, magFieldB, 3, 3, 1);
// change unit from uT to T
VectorOperations<double>::mulScalar(magFieldB, 1e-6, magFieldB, 3);
double crossSun[3] = {0, 0, 0};
VectorOperations<double>::cross(sunDirRef, sunDirB, crossSun);
double normCrossSun = VectorOperations<double>::norm(crossSun, 3);
// calc angle alpha between sunDirRef and sunDIr
double dotSun = VectorOperations<double>::dot(sunDirRef, sunDirB);
double alpha = acos(dotSun);
// Law Torque calculations
double torqueCmd[3] = {0, 0, 0}, torqueAlign[3] = {0, 0, 0}, torqueRate[3] = {0, 0, 0},
torqueAll[3] = {0, 0, 0};
double scalarFac = kAlign * alpha / normCrossSun;
VectorOperations<double>::mulScalar(crossSun, scalarFac, torqueAlign, 3);
double rateSafeMode[3] = {0, 0, 0};
VectorOperations<double>::subtract(satRateMekf, satRatRef, rateSafeMode, 3);
VectorOperations<double>::mulScalar(rateSafeMode, -kRate, torqueRate, 3);
VectorOperations<double>::add(torqueRate, torqueAlign, torqueAll, 3);
// Adding factor of inertia for axes
MatrixOperations<double>::multiplyScalar(*(acsParameters->inertiaEIVE.inertiaMatrix), 10,
*gainMatrixInertia, 3,
3); // why only for mekf one and not for no mekf
MatrixOperations<double>::multiply(*gainMatrixInertia, torqueAll, torqueCmd, 3, 3, 1);
// MagMom B (orthogonal torque)
double torqueMgt[3] = {0, 0, 0};
VectorOperations<double>::cross(magFieldB, torqueCmd, torqueMgt);
double normMag = VectorOperations<double>::norm(magFieldB, 3);
VectorOperations<double>::mulScalar(torqueMgt, 1 / pow(normMag, 2), outputMagMomB, 3);
*outputAngle = alpha;
return returnvalue::OK;
}
// Will be the version in worst case scenario in event of no working MEKF (nor GYRs)
ReturnValue_t SafeCtrl::safeNoMekf(timeval now, double *susDirB, bool susDirBValid,
double *sunRateB, bool sunRateBValid, double *magFieldB,
bool magFieldBValid, double *magRateB, bool magRateBValid,
double *sunDirRef, double *satRateRef, double *outputAngle,
double *outputMagMomB) {
// Check for invalid Inputs
if (!susDirBValid || !magFieldBValid || !magRateBValid) {
return returnvalue::FAILED;
}
// change unit from uT to T
double magFieldBT[3] = {0, 0, 0};
VectorOperations<double>::mulScalar(magFieldB, 1e-6, magFieldBT, 3);
// normalize sunDir and magDir
double magDirB[3] = {0, 0, 0};
VectorOperations<double>::normalize(magFieldBT, magDirB, 3);
VectorOperations<double>::normalize(susDirB, susDirB, 3);
// Cosinus angle between sunDir and magDir
double cosAngleSunMag = VectorOperations<double>::dot(magDirB, susDirB);
// Rate parallel to sun direction and magnetic field direction
double dotSunRateMag = VectorOperations<double>::dot(sunRateB, magDirB);
double dotmagRateSun = VectorOperations<double>::dot(magRateB, susDirB);
double rateFactor = 1 - pow(cosAngleSunMag, 2);
double rateParaSun = (dotmagRateSun + cosAngleSunMag * dotSunRateMag) / rateFactor;
double rateParaMag = (dotSunRateMag + cosAngleSunMag * dotmagRateSun) / rateFactor;
// Full rate or estimate
double estSatRate[3] = {0, 0, 0};
double estSatRateMag[3] = {0, 0, 0}, estSatRateSun[3] = {0, 0, 0};
VectorOperations<double>::mulScalar(susDirB, rateParaSun, estSatRateSun, 3);
VectorOperations<double>::add(sunRateB, estSatRateSun, estSatRateSun, 3);
VectorOperations<double>::mulScalar(magDirB, rateParaMag, estSatRateMag, 3);
VectorOperations<double>::add(magRateB, estSatRateMag, estSatRateMag, 3);
VectorOperations<double>::add(estSatRateSun, estSatRateMag, estSatRate, 3);
VectorOperations<double>::mulScalar(estSatRate, 0.5, estSatRate, 3);
/* Only valid if angle between sun direction and magnetic field direction
* is sufficiently large */
double angleSunMag = acos(cosAngleSunMag);
if (angleSunMag < acsParameters->safeModeControllerParameters.sunMagAngleMin) {
return returnvalue::FAILED;
}
// 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 = acsParameters->safeModeControllerParameters.k_rate_no_mekf;
double kAlignNoMekf = acsParameters->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 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);
// Final torque
double torqueB[3] = {0, 0, 0}, torqueAlignRate[3] = {0, 0, 0};
VectorOperations<double>::add(torqueRate, torqueAlign, torqueAlignRate, 3);
MatrixOperations<double>::multiply(*(acsParameters->inertiaEIVE.inertiaMatrix), torqueAlignRate,
torqueB, 3, 3, 1);
// Magnetic moment
double magMomB[3] = {0, 0, 0};
double crossMagFieldTorque[3] = {0, 0, 0};
VectorOperations<double>::cross(magFieldBT, torqueB, crossMagFieldTorque);
double magMomFactor = pow(VectorOperations<double>::norm(magFieldBT, 3), 2);
VectorOperations<double>::mulScalar(crossMagFieldTorque, 1 / magMomFactor, magMomB, 3);
std::memcpy(outputMagMomB, magMomB, 3 * sizeof(double));
*outputAngle = angleAlignErr;
return returnvalue::OK;
}