eive-obsw/mission/controller/acs/ActuatorCmd.h
2023-06-13 07:48:32 +02:00

47 lines
1.6 KiB
C++

#ifndef ACTUATORCMD_H_
#define ACTUATORCMD_H_
#include <cmath>
class ActuatorCmd {
public:
ActuatorCmd();
virtual ~ActuatorCmd();
/*
* @brief: scalingTorqueRws() scales the torque via maximum part in case this part is
* higher then the maximum torque
* @param: rwTrq given torque for reaction wheels which will be
* scaled if needed to be
*/
void scalingTorqueRws(double *rwTrq, double maxTorque);
/*
* @brief: cmdSpeedToRws() Calculates the RPM for the reaction wheel configuration,
* given the required torque calculated by the controller. Will also scale down the RPM of the
* wheels if they exceed the maximum possible RPM
* @param: rwTrq given torque from pointing controller
* 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 sampleTime, const double inertiaWheel,
const int32_t maxRwSpeed, const double *rwTorque, int32_t *rwCmdSpeed);
/*
* @brief: cmdDipoleMtq() gives the commanded dipole moment for the
* magnetorquer
*
* @param: dipoleMoment given dipole moment in spacecraft frame
* dipoleMomentActuator resulting dipole moment in actuator reference frame
*/
void cmdDipoleMtq(const double *inverseAlignment, const double maxDipole,
const double *dipoleMoment, int16_t *dipoleMomentActuator);
protected:
private:
static constexpr double RAD_PER_SEC_TO_RPM = 60 / (2 * M_PI);
};
#endif /* ACTUATORCMD_H_ */