eive-obsw/mission/controller/acs/ActuatorCmd.h
Marius Eggert 84fc44fd5f
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fixed GPS and STR inputs
2022-10-12 15:06:24 +02:00

50 lines
1.4 KiB
C++

/*
* ActuatorCmd.h
*
* Created on: 4 Aug 2022
* Author: Robin Marquardt
*/
#ifndef ACTUATORCMD_H_
#define ACTUATORCMD_H_
#include "AcsParameters.h"
#include "SensorProcessing.h"
#include "MultiplicativeKalmanFilter.h"
#include "SensorValues.h"
#include "OutputValues.h"
class ActuatorCmd{
public:
ActuatorCmd(AcsParameters *acsParameters_); //Input mode ?
virtual ~ActuatorCmd();
/*
* @brief: cmdSpeedToRws() will set the maximum possible torque for the reaction wheels, also
* will calculate the needed revolutions per minute for the RWs, which will be given
* as Input to the RWs
* @param: rwTrqIn given torque from pointing controller
* rwTrqNS Nullspace torque
* rwCmdSpeed output revolutions per minute for every reaction wheel
*/
void cmdSpeedToRws(const int32_t *speedRw0, const int32_t *speedRw1,
const int32_t *speedRw2, const int32_t *speedRw3, const double *rwTrqIn,
const double *rwTrqNS, double *rwCmdSpeed);
/*
* @brief: cmdDipolMtq() gives the commanded dipol moment for the magnetorques
*
* @param: dipolMoment given dipol moment in spacecraft frame
* dipolMomentUnits resulting dipol moment for every unit
*/
void cmdDipolMtq(const double *dipolMoment, double *dipolMomentUnits);
protected:
private:
AcsParameters acsParameters;
};
#endif /* ACTUATORCMD_H_ */