eive-obsw/mission/controller/acs/Guidance.h
Marius Eggert 5e557d2d46
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first version of safe mode solar vector for leop
2023-01-12 14:49:37 +01:00

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3.5 KiB
C++

/*
* Guidance.h
*
* Created on: 6 Jun 2022
* Author: Robin Marquardt
*/
#ifndef GUIDANCE_H_
#define GUIDANCE_H_
#include <time.h>
#include "../controllerdefinitions/AcsCtrlDefinitions.h"
#include "AcsParameters.h"
#include "SensorValues.h"
class Guidance {
public:
Guidance(AcsParameters *acsParameters_);
virtual ~Guidance();
void getTargetParamsSafe(double sunTargetSafe[3], double satRateRef[3]);
// Function to get the target quaternion and refence rotation rate from gps position and
// position of the ground station
void targetQuatPtgThreeAxes(ACS::SensorValues *sensorValues,
acsctrl::GpsDataProcessed *gpsDataProcessed,
acsctrl::MekfData *mekfData, timeval now, double targetQuat[4],
double refSatRate[3]);
void targetQuatPtgGs(ACS::SensorValues *sensorValues, acsctrl::MekfData *mekfData,
acsctrl::SusDataProcessed *susDataProcessed,
acsctrl::GpsDataProcessed *gpsDataProcessed, timeval now,
double targetQuat[4], double refSatRate[3]);
void targetQuatPtgSingleAxis(ACS::SensorValues *sensorValues, acsctrl::MekfData *mekfData,
acsctrl::SusDataProcessed *susDataProcessed,
acsctrl::GpsDataProcessed *gpsDataProcessed, timeval now,
double targetQuat[4], double refSatRate[3]);
// Function to get the target quaternion and refence rotation rate for sun pointing after ground
// station
void sunQuatPtg(ACS::SensorValues *sensorValues, acsctrl::MekfData *mekfData,
acsctrl::SusDataProcessed *susDataProcessed,
acsctrl::GpsDataProcessed *gpsDataProcessed, timeval now, double targetQuat[4],
double refSatRate[3]);
// Function to get the target quaternion and refence rotation rate from gps position for Nadir
// pointing
void quatNadirPtgThreeAxes(ACS::SensorValues *sensorValues,
acsctrl::GpsDataProcessed *gpsDataProcessed,
acsctrl::MekfData *mekfData, timeval now, double targetQuat[4],
double refSatRate[3]);
void quatNadirPtgSingleAxis(ACS::SensorValues *sensorValues, acsctrl::MekfData *mekfData,
timeval now, double targetQuat[4], double refSatRate[3]);
// Function to get the target quaternion and refence rotation rate from parameters for inertial
// pointing
void inertialQuatPtg(double targetQuat[4], double refSatRate[3]);
// @note: compares target Quaternion and reference quaternion, also actual satellite rate and
// desired
void comparePtg(double targetQuat[4], acsctrl::MekfData *mekfData, double refSatRate[3],
double quatErrorComplete[4], double quatError[3], double deltaRate[3]);
void refRotationRate(timeval now, double quatInertialTarget[4], double *refSatRate);
// @note: will give back the pseudoinverse matrix for the reaction wheel depending on the valid
// reation wheel maybe can be done in "commanding.h"
void getDistributionMatrixRw(ACS::SensorValues *sensorValues, double *rwPseudoInv);
private:
AcsParameters acsParameters;
bool strBlindAvoidFlag = false;
timeval timeSavedQuaternionNadir;
double savedQuaternionNadir[4] = {0, 0, 0, 0};
double omegaRefSavedNadir[3] = {0, 0, 0};
static constexpr char SD_0_SKEWED_PTG_FILE[] = "/mnt/sd0/conf/deployment";
static constexpr char SD_1_SKEWED_PTG_FILE[] = "/mnt/sd1/conf/deployment";
};
#endif /* ACS_GUIDANCE_H_ */