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acsParameters in kalman filter added
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Robin Marquardt 2022-12-05 21:31:52 +01:00
parent 8d1cbd9f8b
commit 2b445369fd
2 changed files with 8 additions and 10 deletions
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10
mission/controller/acs/AcsParameters.h
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@ -872,8 +872,8 @@ class AcsParameters /*: public HasParametersIF*/ {
struct SunModelParameters { struct SunModelParameters {
float domega = 36000.771; float domega = 36000.771;
float omega_0 = 282.94 * M_PI / 180.; // RAAN plus argument of perigee float omega_0 = 280.46 * M_PI / 180.; //282.94 * M_PI / 180.; // RAAN plus argument of perigee
float m_0 = 357.5256; // coefficients for mean anomaly float m_0 = 357.5277; //357.5256; // coefficients for mean anomaly
float dm = 35999.049; // coefficients for mean anomaly float dm = 35999.049; // coefficients for mean anomaly
float e = 23.4392911 * M_PI / 180.; // angle of earth's rotation axis float e = 23.4392911 * M_PI / 180.; // angle of earth's rotation axis
float e1 = 0.74508 * M_PI / 180.; float e1 = 0.74508 * M_PI / 180.;
@ -886,10 +886,10 @@ class AcsParameters /*: public HasParametersIF*/ {
double sensorNoiseSTR = 0.1 * M_PI / 180; double sensorNoiseSTR = 0.1 * M_PI / 180;
double sensorNoiseSS = 8 * M_PI / 180; double sensorNoiseSS = 8 * M_PI / 180;
double sensorNoiseMAG = 4 * M_PI / 180; double sensorNoiseMAG = 4 * M_PI / 180;
double sensorNoiseRMU[3]; double sensorNoiseGYR = 0.1 * M_PI / 180;
double sensorNoiseArwRmu; // Angular Random Walk double sensorNoiseArwGYR = 3*0.0043*M_PI / sqrt(10) / 180; // Angular Random Walk
double sensorNoiseBsRMU; // Bias Stability double sensorNoiseBsGYR = 3 * M_PI / 180 / 3600; // Bias Stability
} kalmanFilterParameters; } kalmanFilterParameters;
struct MagnetorquesParameter { struct MagnetorquesParameter {

8
mission/controller/acs/MultiplicativeKalmanFilter.cpp
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@ -51,7 +51,7 @@ void MultiplicativeKalmanFilter::init(const double *magneticField_, const bool *
sigmaSun = kalmanFilterParameters->sensorNoiseSS; sigmaSun = kalmanFilterParameters->sensorNoiseSS;
sigmaMag = kalmanFilterParameters->sensorNoiseMAG; 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}, double normMagB[3] = {0,0,0}, normSunB[3] = {0,0,0},
normMagJ[3] = {0,0,0}, normSunJ[3] = {0,0,0}; normMagJ[3] = {0,0,0}, normSunJ[3] = {0,0,0};
@ -980,10 +980,8 @@ ReturnValue_t MultiplicativeKalmanFilter::mekfEst(
/* ----------- PROPAGATION ----------*/ /* ----------- PROPAGATION ----------*/
//double sigmaU = kalmanFilterParameters->sensorNoiseBsRMU; double sigmaU = kalmanFilterParameters->sensorNoiseBsGYR;
//double sigmaV = kalmanFilterParameters->sensorNoiseArwRmu; double sigmaV = kalmanFilterParameters->sensorNoiseArwGYR;
double sigmaU = 3*3.141/180/3600;
double sigmaV = 3*0.0043*3.141/sqrt(10)/180;
double discTimeMatrix[6][6] = {{-1,0,0,0,0,0},{0,-1,0,0,0,0},{0,0,-1,0,0,0}, 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}}; {0,0,0,1,0,0},{0,0,0,0,1,0},{0,0,0,0,0,1}};