diff --git a/mission/controller/acs/MultiplicativeKalmanFilter.cpp b/mission/controller/acs/MultiplicativeKalmanFilter.cpp index 566ef4ca..14c2a2ec 100644 --- a/mission/controller/acs/MultiplicativeKalmanFilter.cpp +++ b/mission/controller/acs/MultiplicativeKalmanFilter.cpp @@ -1,10 +1,3 @@ -/* - * MultiplicativeKalmanFilter.cpp - * - * Created on: 4 Feb 2022 - * Author: rooob - */ - #include "MultiplicativeKalmanFilter.h" #include @@ -31,7 +24,7 @@ MultiplicativeKalmanFilter::~MultiplicativeKalmanFilter() {} void MultiplicativeKalmanFilter::loadAcsParameters(AcsParameters *acsParameters_) { inertiaEIVE = &(acsParameters_->inertiaEIVE); - kalmanFilterParameters = &(acsParameters_->kalmanFilterParameters); /*Sensor noises also here*/ + kalmanFilterParameters = &(acsParameters_->kalmanFilterParameters); } void MultiplicativeKalmanFilter::reset() {} @@ -43,14 +36,11 @@ void MultiplicativeKalmanFilter::init( // check for valid mag/sun if (validMagField_ && validSS && validSSModel && validMagModel) { validInit = true; - // AcsParameters mekfEstParams; - // loadAcsParameters(&mekfEstParams); // QUEST ALGO ----------------------------------------------------------------------- double sigmaSun = 0, sigmaMag = 0, sigmaGyro = 0; sigmaSun = kalmanFilterParameters->sensorNoiseSS; sigmaMag = kalmanFilterParameters->sensorNoiseMAG; - - sigmaGyro = 0.1 * 3.141 / 180; // acs parameters + sigmaGyro = kalmanFilterParameters->sensorNoiseGYR; double normMagB[3] = {0, 0, 0}, normSunB[3] = {0, 0, 0}, normMagJ[3] = {0, 0, 0}, normSunJ[3] = {0, 0, 0}; @@ -138,7 +128,6 @@ void MultiplicativeKalmanFilter::init( matrixMag[3][3] = {{0, 0, 0}, {0, 0, 0}, {0, 0, 0}}, matrixSunMag[3][3] = {{0, 0, 0}, {0, 0, 0}, {0, 0, 0}}, matrixMagSun[3][3] = {{0, 0, 0}, {0, 0, 0}, {0, 0, 0}}; - /* vector*transpose(vector)*/ MatrixOperations::multiply(sunEstB, sunEstB, *matrixSun, 3, 1, 3); MatrixOperations::multiply(magEstB, magEstB, *matrixMag, 3, 1, 3); MatrixOperations::multiply(sunEstB, magEstB, *matrixSunMag, 3, 1, 3); @@ -201,8 +190,6 @@ void MultiplicativeKalmanFilter::init( initialCovarianceMatrix[5][3] = initGyroCov[2][0]; initialCovarianceMatrix[5][4] = initGyroCov[2][1]; initialCovarianceMatrix[5][5] = initGyroCov[2][2]; - // initialCovarianceMatrix[][] = {{0,0,0,0,0,0},{0,0,0,0,0,0},{0,0,0,0,0,0}, - //{0,0,0,0,0,0},{0,0,0,0,0,0},{0,0,0,0,0,0}}; } else { // no initialisation possible, no valid measurements validInit = false; @@ -216,8 +203,6 @@ ReturnValue_t MultiplicativeKalmanFilter::mekfEst( const double *sunDir_, const bool validSS, const double *sunDirJ, const bool validSSModel, const double *magFieldJ, const bool validMagModel, acsctrl::MekfData *mekfData) { // Check for GYR Measurements - // AcsParameters mekfEstParams; - // loadAcsParameters(&mekfEstParams); int MDF = 0; // Matrix Dimension Factor if (!validGYRs_) { { @@ -934,10 +919,6 @@ ReturnValue_t MultiplicativeKalmanFilter::mekfEst( double errStateQuat[3] = {errStateVec[0], errStateVec[1], errStateVec[2]}; double errStateGyroBias[3] = {errStateVec[3], errStateVec[4], errStateVec[5]}; - sif::debug << "errQ=[" << errStateQuat[0] << "," << errStateQuat[1] << "," << errStateQuat[2] - << "]" << std::endl; - sif::debug << "errW_bias=[" << errStateGyroBias[0] << "," << errStateGyroBias[1] << "," - << errStateGyroBias[2] << "]" << std::endl; // State Vector Elements double xi1[3][3] = {{0, 0, 0}, {0, 0, 0}, {0, 0, 0}}, @@ -966,25 +947,18 @@ ReturnValue_t MultiplicativeKalmanFilter::mekfEst( biasGYR[2] = updatedGyroBias[2]; /* ----------- PROPAGATION ----------*/ - // double sigmaU = kalmanFilterParameters->sensorNoiseBsGYR; - // double sigmaV = kalmanFilterParameters->sensorNoiseArwGYR; - double sigmaU = 3 * 3.141 / 180 / 3600; - double sigmaV = 3 * 0.0043 * 3.141 / sqrt(10) / 180; + double sigmaU = kalmanFilterParameters->sensorNoiseBsGYR; + double sigmaV = kalmanFilterParameters->sensorNoiseArwGYR; double discTimeMatrix[6][6] = {{-1, 0, 0, 0, 0, 0}, {0, -1, 0, 0, 0, 0}, {0, 0, -1, 0, 0, 0}, {0, 0, 0, 1, 0, 0}, {0, 0, 0, 0, 1, 0}, {0, 0, 0, 0, 0, 1}}; double rotRateEst[3] = {0, 0, 0}; - sif::debug << "MEKF rateGYR= " << rateGYRs_[0] << " " << rateGYRs_[1] << " " << rateGYRs_[2] - << std::endl; - sif::debug << "MEKF bias= " << updatedGyroBias[0] << " " << updatedGyroBias[1] << " " - << updatedGyroBias[2] << std::endl; VectorOperations::subtract(rateGYRs_, updatedGyroBias, rotRateEst, 3); double normRotEst = VectorOperations::norm(rotRateEst, 3); double crossRotEst[3][3] = {{0, -rotRateEst[2], rotRateEst[1]}, {rotRateEst[2], 0, -rotRateEst[0]}, {-rotRateEst[1], rotRateEst[0], 0}}; - // ToDo // Discrete Process Noise Covariance Q double discProcessNoiseCov[6][6] = {{0, 0, 0, 0, 0, 0}, {0, 0, 0, 0, 0, 0}, {0, 0, 0, 0, 0, 0}, {0, 0, 0, 0, 0, 0}, {0, 0, 0, 0, 0, 0}, {0, 0, 0, 0, 0, 0}}; @@ -1072,7 +1046,6 @@ ReturnValue_t MultiplicativeKalmanFilter::mekfEst( discProcessNoiseCov[5][4] = covQ22[2][1]; discProcessNoiseCov[5][5] = covQ22[2][2]; - // ToDo // State Transition Matrix phi double phi11[3][3] = {{0, 0, 0}, {0, 0, 0}, {0, 0, 0}}, phi12[3][3] = {{0, 0, 0}, {0, 0, 0}, {0, 0, 0}},