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mission/controller/acs/AcsParameters.cpp
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mission/controller/acs/AcsParameters.cpp
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#include <fsfw/src/fsfw/globalfunctions/constants.h>
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#include "AcsParameters.h"
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#include <stddef.h>
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#include <cmath>
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AcsParameters::AcsParameters() {
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onBoardParams.sampleTime = 0.1;
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inertiaEIVE.inertiaMatrix = {{ 1, 0, 0},
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{ 0, 1, 0},
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{ 0,0.5, 1}};
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mgmHandlingParameters.mgm0orientationMatrix = {{ 0, 0,-1},
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{ 0, 1, 0},
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{ 1, 0, 0}};
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/*mgmHandlingParameters.mgm1orientationMatrix = {{ 0, 0, 1},
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{ 0,-1, 0},
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{ 1, 0, 0}};
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mgmHandlingParameters.mgm2orientationMatrix = {{ 0, 0,-1},
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{ 0, 1, 0},
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{ 1 ,0, 0}};
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mgmHandlingParameters.mgm3orientationMatrix = {{ 0, 0, 1},
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{ 0,-1, 0},
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{ 1, 0, 0}};
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mgmHandlingParameters.mgm4orientationMatrix = {{ 0, 0,-1},
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{-1, 0, 0},
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{ 0, 1, 0}};*/
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rwHandlingParameters.inertiaWheel = 0.000028198;
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rwHandlingParameters.maxTrq = 0.0032; //3.2 [mNm]
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//Geometry frame
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rwMatrices.alignmentMatrix = {{ 0.9205, 0,-0.9205, 0},
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{ 0,-0.9205, 0, 0.9205},
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{ 0.3907, 0.3907, 0.3907, 0.3907}};
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rwMatrices.pseudoInverse = {{ 0.4434,-0.2845, 0.3597},
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{ 0.2136,-0.3317, 1.0123},
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{-0.8672,-0.1406, 0.1778},
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{ 0.6426, 0.4794, 1.3603}};
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rwMatrices.nullspace = {-0.7358, 0.5469,-0.3637,-0.1649};
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kalmanFilterParameters.sensorNoiseSS = 8 * Math::PI / 180;
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kalmanFilterParameters.sensorNoiseMAG = 4 * Math::PI / 180;
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kalmanFilterParameters.sensorNoiseSTR = 0.1 * Math::PI / 180;
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sunModelParameters.domega = 36000.771;
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sunModelParameters.omega_0 = 282.94 * Math::PI / 180.;
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sunModelParameters.dm = 35999.049;
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sunModelParameters.m_0 = 357.5256;
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sunModelParameters.e = 23.4392911 * Math::PI / 180.;
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sunModelParameters.e = 0.74508 * Math::PI / 180.;
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sunModelParameters.p1 = 6892. / 3600. * Math::PI / 180.;
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sunModelParameters.p2 = 72. / 3600. * Math::PI / 180.;
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safeModeControllerParameters.k_rate_mekf = 0.00059437;
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safeModeControllerParameters.k_align_mekf = 0.000056875;
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safeModeControllerParameters.sunTargetDir = {1,0,0};
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detumbleCtrlParameters.gainD = pow(10.0,-3.3);
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// Stuttgart
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groundStationParameters.latitudeGs = 48.7495 * Math::PI / 180.;
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groundStationParameters.longitudeGs = 9.10384 * Math::PI / 180.;
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groundStationParameters.altitudeGs = 500;
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groundStationParameters.earthRadiusEquat = 6378137;
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groundStationParameters.earthRadiusPolar = 6356752.314;
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// Geometry frame
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targetModeControllerParameters.refDirection = {1,0,0};
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targetModeControllerParameters.refRotRate = {0,0,0};
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targetModeControllerParameters.quatRef = {0,0,0,1};
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targetModeControllerParameters.avoidBlindStr = true;
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targetModeControllerParameters.blindAvoidStart = 1.5;
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targetModeControllerParameters.blindAvoidStop = 2.5;
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targetModeControllerParameters.blindRotRate = 1 * Math::PI /180;
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targetModeControllerParameters.zeta = 0.3;
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targetModeControllerParameters.om = 0.3;
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targetModeControllerParameters.qiMin = 0.1;
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targetModeControllerParameters.omMax = 1 * Math::PI / 180;
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targetModeControllerParameters.gainNullspace = 0.01;
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targetModeControllerParameters.desatMomentumRef = {0,0,0};
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targetModeControllerParameters.deSatGainFactor = 1000;
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targetModeControllerParameters.desatOn = true;
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targetModeControllerParameters.omegaEarth = 0.000072921158553;
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strParameters.boresightAxis = { 0.7593, 0,-0.6508};
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strParameters.exclusionAngle = 20 * Math::PI /180;
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magnetorquesParameter.mtq0orientationMatrix = {{ 1, 0, 0},
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{ 0, 0, 1},
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{ 0,-1, 0}};
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magnetorquesParameter.mtq1orientationMatrix = {{ 1, 0, 0},
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{ 0, 1, 0},
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{ 0, 0, 1}};
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magnetorquesParameter.mtq2orientationMatrix = {{ 0, 0, 1},
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{ 0, 1, 0},
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{-1, 0, 0}};
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magnetorquesParameter.alignmentMatrixMtq = {{ 0, 0,-1},
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{-1, 0, 0},
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{ 0, 1, 0}};
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magnetorquesParameter.inverseAlignment = {{ 0,-1, 0},
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{ 0, 0, 1},
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{-1, 0, 0}};
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magnetorquesParameter.DipolMax = 0.2;
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}
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AcsParameters::~AcsParameters() {
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}
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/*
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ReturnValue_t AcsParameters::getParameter(uint8_t domainId,
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uint16_t parameterId, ParameterWrapper* parameterWrapper,
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const ParameterWrapper *newValues, uint16_t startAtIndex) {
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return 0;
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}*/
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201
mission/controller/acs/AcsParameters.h
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mission/controller/acs/AcsParameters.h
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/*******************************
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* EIVE Flight Software Framework (FSFW)
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* (c) 2022 IRS, Uni Stuttgart
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*******************************/
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#ifndef ACSPARAMETERS_H_
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#define ACSPARAMETERS_H_
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#include <fsfw/parameters/HasParametersIF.h>
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typedef unsigned char uint8_t;
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class AcsParameters:public HasParametersIF{
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public:
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AcsParameters();
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virtual ~AcsParameters();
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virtual ReturnValue_t getParameter(uint8_t domainId, uint16_t parameterId,
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ParameterWrapper *parameterWrapper,
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const ParameterWrapper *newValues, uint16_t startAtIndex);
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struct OnBoardParams {
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double sampleTime; // [s]
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} onBoardParams;
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struct InertiaEIVE {
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double inertiaMatrix[3][3];
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double inertiaMatrixInverse[3][3];
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} inertiaEIVE;
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struct MgmHandlingParameters {
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float mgm0orientationMatrix[3][3];
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float mgm1orientationMatrix[3][3];
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float mgm2orientationMatrix[3][3];
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float mgm3orientationMatrix[3][3];
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float mgm4orientationMatrix[3][3];
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} mgmHandlingParameters;
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struct SusHandlingParameters {
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float sus0orientationMatrix[3][3];
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float sus1orientationMatrix[3][3];
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float sus2orientationMatrix[3][3];
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float sus3orientationMatrix[3][3];
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float sus4orientationMatrix[3][3];
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float sus5orientationMatrix[3][3];
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float sus6orientationMatrix[3][3];
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float sus7orientationMatrix[3][3];
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float sus8orientationMatrix[3][3];
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float sus9orientationMatrix[3][3];
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float sus10orientationMatrix[3][3];
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float sus11orientationMatrix[3][3];
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float filterAlpha;
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float sunThresh;
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} susHandlingParameters;
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struct RmuHandlingParameters {
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double rmu0orientationMatrix[3][3];
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double rmu1orientationMatrix[3][3];
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double rmu2orientationMatrix[3][3];
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} rmuHandlingParameters;
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struct RwHandlingParameters {
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double rw0orientationMatrix[3][3];
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double rw1orientationMatrix[3][3];
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double rw2orientationMatrix[3][3];
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double rw3orientationMatrix[3][3];
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double inertiaWheel;
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double maxTrq;
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} rwHandlingParameters;
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struct SafeModeControllerParameters {
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double k_rate_mekf;
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double k_align_mekf;
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double k_rate_no_mekf;
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double k_align_no_mekf;
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double sunMagAngleMin;
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double sunTargetDir[3]; //Body frame
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double satRateRef[3]; //Body frame
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} safeModeControllerParameters;
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struct DetumbleCtrlParameters {
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double gainD;
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} detumbleCtrlParameters;
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struct PointingModeControllerParameters {
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double updtFlag;
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double A_rw[3][12];
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double refDirection[3];
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double refRotRate[3];
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double quatRef[4];
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bool avoidBlindStr;
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double blindAvoidStart;
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double blindAvoidStop;
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double blindRotRate;
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double zeta;
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double zetaLow;
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double om;
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double omLow;
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double qiMin;
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double omMax;
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double gainNullspace;
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double desatMomentumRef[3];
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double deSatGainFactor;
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bool desatOn;
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double omegaEarth;
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} inertialModeControllerParameters, nadirModeControllerParameters,
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targetModeControllerParameters;
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struct RWMatrices {
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double alignmentMatrix[3][4];
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double pseudoInverse[4][3];
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double without0[4][3];
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double without1[4][3];
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double without2[4][3];
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double without3[4][3];
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double nullspace[4];
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} rwMatrices;
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struct StrParameters {
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double exclusionAngle;
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// double strOrientationMatrix[3][3];
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double boresightAxis[3]; //in body/geometry frame
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} strParameters;
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struct GpsParameters {
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} gpsParameters;
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struct GroundStationParameters {
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double latitudeGs; // [rad] Latitude
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double longitudeGs; // [rad] Longitude
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double altitudeGs; // [m] Altitude
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double earthRadiusEquat; // [m]
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double earthRadiusPolar; // [m]
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} groundStationParameters;
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struct SunModelParameters {
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enum UseSunModel {
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NO = 0, YES = 3
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};
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uint8_t useSunModel;
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float domega;
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float omega_0; //Rektaszension des Aufsteigenden Knotens plus Argument des Perigäums
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float m_0; //coefficients for mean anomaly
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float dm; //coefficients for mean anomaly
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float e; //angle of earth's rotation axis
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float e1;
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float p1; //some parameter
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float p2; //some parameter
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} sunModelParameters;
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struct KalmanFilterParameters {
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uint8_t activateKalmanFilter;
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uint8_t requestResetFlag;
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double maxToleratedTimeBetweenKalmanFilterExecutionSteps;
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double processNoiseOmega[3];
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double processNoiseQuaternion[4];
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double sensorNoiseSTR;
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double sensorNoiseSS;
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double sensorNoiseMAG;
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double sensorNoiseRMU[3];
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double sensorNoiseArwRmu; //Angular Random Walk
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double sensorNoiseBsRMU; // Bias Stability
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} kalmanFilterParameters;
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struct MagnetorquesParameter {
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double mtq0orientationMatrix[3][3];
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double mtq1orientationMatrix[3][3];
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double mtq2orientationMatrix[3][3];
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double alignmentMatrixMtq[3][3];
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double inverseAlignment[3][3];
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double DipolMax; // [Am^2]
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} magnetorquesParameter;
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struct DetumbleParameter {
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uint8_t detumblecounter;
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double omegaDetumbleStart;
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double omegaDetumbleEnd;
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} detumbleParameter;
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};
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#endif /* ACSPARAMETERS_H_ */
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