#include "SafeCtrl.h" #include #include #include #include SafeCtrl::SafeCtrl(AcsParameters *acsParameters_) { acsParameters = acsParameters_; } SafeCtrl::~SafeCtrl() {} acs::ControlModeStrategy SafeCtrl::safeCtrlStrategy(const bool magFieldValid, const bool mekfValid, const bool satRotRateValid, const bool sunDirValid, const bool fusedRateTotalValid, const uint8_t mekfEnabled, const uint8_t gyrEnabled, const uint8_t dampingEnabled) { if (not magFieldValid) { return acs::ControlModeStrategy::CTRL_NO_MAG_FIELD_FOR_CONTROL; } else if (mekfEnabled and mekfValid) { return acs::ControlModeStrategy::SAFECTRL_MEKF; } else if (sunDirValid) { if (gyrEnabled and satRotRateValid) { return acs::ControlModeStrategy::SAFECTRL_GYR; } else if (not gyrEnabled and fusedRateTotalValid) { return acs::ControlModeStrategy::SAFECTRL_SUSMGM; } else { return acs::ControlModeStrategy::CTRL_NO_SENSORS_FOR_CONTROL; } } else if (not sunDirValid) { if (dampingEnabled) { if (gyrEnabled and satRotRateValid) { return acs::ControlModeStrategy::SAFECTRL_ECLIPSE_DAMPING_GYR; } else if (not gyrEnabled and satRotRateValid and fusedRateTotalValid) { return acs::ControlModeStrategy::SAFECTRL_ECLIPSE_DAMPING_SUSMGM; } else { return acs::ControlModeStrategy::CTRL_NO_SENSORS_FOR_CONTROL; } } else if (not dampingEnabled and satRotRateValid) { return acs::ControlModeStrategy::SAFECTRL_ECLIPSE_IDELING; } else { return acs::ControlModeStrategy::CTRL_NO_SENSORS_FOR_CONTROL; } } else { return acs::ControlModeStrategy::CTRL_NO_SENSORS_FOR_CONTROL; } } void SafeCtrl::safeMekf(const double *magFieldB, const double *satRotRateB, const double *sunDirModelI, const double *quatBI, const double *sunDirRefB, double *magMomB, double &errorAngle) { // convert magFieldB from uT to T VectorOperations::mulScalar(magFieldB, 1e-6, magFieldBT, 3); // convert sunDirModel to body rf double sunDirB[3] = {0, 0, 0}; QuaternionOperations::multiplyVector(quatBI, sunDirModelI, sunDirB); // calculate angle alpha between sunDirRef and sunDir double dotSun = VectorOperations::dot(sunDirRefB, sunDirB); errorAngle = acos(dotSun); splitRotationalRate(satRotRateB, sunDirB); calculateRotationalRateTorque(acsParameters->safeModeControllerParameters.k_parallelMekf, acsParameters->safeModeControllerParameters.k_orthoMekf); calculateAngleErrorTorque(sunDirB, sunDirRefB, acsParameters->safeModeControllerParameters.k_alignMekf); // sum of all torques for (uint8_t i = 0; i < 3; i++) { cmdTorque[i] = cmdAlign[i] + cmdOrtho[i] + cmdParallel[i]; } calculateMagneticMoment(magMomB); } void SafeCtrl::safeGyr(const double *magFieldB, const double *satRotRateB, const double *sunDirB, const double *sunDirRefB, double *magMomB, double &errorAngle) { // convert magFieldB from uT to T VectorOperations::mulScalar(magFieldB, 1e-6, magFieldBT, 3); // calculate error angle between sunDirRef and sunDir double dotSun = VectorOperations::dot(sunDirRefB, sunDirB); errorAngle = acos(dotSun); splitRotationalRate(satRotRateB, sunDirB); calculateRotationalRateTorque(acsParameters->safeModeControllerParameters.k_parallelGyr, acsParameters->safeModeControllerParameters.k_orthoGyr); calculateAngleErrorTorque(sunDirB, sunDirRefB, acsParameters->safeModeControllerParameters.k_alignGyr); // sum of all torques for (uint8_t i = 0; i < 3; i++) { cmdTorque[i] = cmdAlign[i] + cmdOrtho[i] + cmdParallel[i]; } calculateMagneticMoment(magMomB); } void SafeCtrl::safeSusMgm(const double *magFieldB, const double *rotRateTotalB, const double *rotRateParallelB, const double *rotRateOrthogonalB, const double *sunDirB, const double *sunDirRefB, double *magMomB, double &errorAngle) { // convert magFieldB from uT to T VectorOperations::mulScalar(magFieldB, 1e-6, magFieldBT, 3); // calculate error angle between sunDirRef and sunDir double dotSun = VectorOperations::dot(sunDirRefB, sunDirB); errorAngle = acos(dotSun); if (VectorOperations::norm(rotRateParallelB, 3) != 0 and VectorOperations::norm(rotRateOrthogonalB, 3) != 0) { std::memcpy(satRotRateParallelB, rotRateParallelB, sizeof(satRotRateParallelB)); std::memcpy(satRotRateOrthogonalB, rotRateOrthogonalB, sizeof(satRotRateOrthogonalB)); } else { splitRotationalRate(rotRateTotalB, sunDirB); } calculateRotationalRateTorque(acsParameters->safeModeControllerParameters.k_parallelSusMgm, acsParameters->safeModeControllerParameters.k_orthoSusMgm); calculateAngleErrorTorque(sunDirB, sunDirRefB, acsParameters->safeModeControllerParameters.k_alignSusMgm); // sum of all torques for (uint8_t i = 0; i < 3; i++) { cmdTorque[i] = cmdAlign[i] + cmdOrtho[i] + cmdParallel[i]; } calculateMagneticMoment(magMomB); } void SafeCtrl::safeRateDampingGyr(const double *magFieldB, const double *satRotRateB, const double *sunDirRefB, double *magMomB, double &errorAngle) { // convert magFieldB from uT to T VectorOperations::mulScalar(magFieldB, 1e-6, magFieldBT, 3); // no error angle available for eclipse errorAngle = NAN; splitRotationalRate(satRotRateB, sunDirRefB); calculateRotationalRateTorque(acsParameters->safeModeControllerParameters.k_parallelGyr, acsParameters->safeModeControllerParameters.k_orthoGyr); // sum of all torques VectorOperations::add(cmdParallel, cmdOrtho, cmdTorque, 3); // calculate magnetic moment to command calculateMagneticMoment(magMomB); } void SafeCtrl::safeRateDampingSusMgm(const double *magFieldB, const double *satRotRateB, const double *sunDirRefB, double *magMomB, double &errorAngle) { // convert magFieldB from uT to T VectorOperations::mulScalar(magFieldB, 1e-6, magFieldBT, 3); // no error angle available for eclipse errorAngle = NAN; splitRotationalRate(satRotRateB, sunDirRefB); calculateRotationalRateTorque(acsParameters->safeModeControllerParameters.k_parallelSusMgm, acsParameters->safeModeControllerParameters.k_orthoSusMgm); // sum of all torques VectorOperations::add(cmdParallel, cmdOrtho, cmdTorque, 3); // calculate magnetic moment to command calculateMagneticMoment(magMomB); } void SafeCtrl::splitRotationalRate(const double *satRotRateB, const double *sunDirB) { // split rotational rate into parallel and orthogonal parts double parallelLength = VectorOperations::dot(satRotRateB, sunDirB) * pow(VectorOperations::norm(sunDirB, 3), -2); VectorOperations::mulScalar(sunDirB, parallelLength, satRotRateParallelB, 3); VectorOperations::subtract(satRotRateB, satRotRateParallelB, satRotRateOrthogonalB, 3); } void SafeCtrl::calculateRotationalRateTorque(const double gainParallel, const double gainOrtho) { // calculate torque for parallel rotational rate VectorOperations::mulScalar(satRotRateParallelB, -gainParallel, cmdParallel, 3); // calculate torque for orthogonal rotational rate VectorOperations::mulScalar(satRotRateOrthogonalB, -gainOrtho, cmdOrtho, 3); } void SafeCtrl::calculateAngleErrorTorque(const double *sunDirB, const double *sunDirRefB, const double gainAlign) { // calculate torque for alignment double crossAlign[3] = {0, 0, 0}; VectorOperations::cross(sunDirRefB, sunDirB, crossAlign); VectorOperations::mulScalar(crossAlign, gainAlign, cmdAlign, 3); } void SafeCtrl::calculateMagneticMoment(double *magMomB) { double torqueMgt[3] = {0, 0, 0}; VectorOperations::cross(magFieldBT, cmdTorque, torqueMgt); double normMag = VectorOperations::norm(magFieldBT, 3); VectorOperations::mulScalar(torqueMgt, pow(normMag, -2), magMomB, 3); }