eive-obsw/mission/controller/acs/Guidance.h

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2022-09-19 15:17:39 +02:00
/*
* Guidance.h
*
* Created on: 6 Jun 2022
* Author: Robin Marquardt
*/
#ifndef GUIDANCE_H_
#define GUIDANCE_H_
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#include "AcsParameters.h"
#include "SensorValues.h"
#include "OutputValues.h"
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#include <time.h>
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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 targetQuatPtg(ACS::SensorValues* sensorValues, ACS::OutputValues *outputValues, timeval now,
double targetQuat[4], double refSatRate[3]);
// @note: compares target Quaternion and reference quaternion, also actual satellite rate and desired
void comparePtg( double targetQuat[4], ACS::OutputValues *outputValues, double refSatRate[3], double quatError[3], double deltaRate[3] );
// @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;
};
#endif /* ACS_GUIDANCE_H_ */