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/***********************************************/
/**
* @file miscAccelerationsAntennaThrust.h
*
* @brief Antenna thrust (simple model).
* @see MiscAccelerations
*
* @author Sebastian Strasser
* @date 2015-03-04
*
*/
/***********************************************/
#ifndef __GROOPS_MISCACCELERATIONSANTENNATHRUST__
#define __GROOPS_MISCACCELERATIONSANTENNATHRUST__
// Latex documentation
#ifdef DOCSTRING_MiscAccelerations
static const char *docstringMiscAccelerationsAntennaThrust = R"(
\subsection{Antenna thrust}\label{miscAccelerationsType:antennaThrust}
The thrust (acceleration) in the opposite direction the antenna is facing
which is generated by satellite antenna broadcasts.
The thrust is defined in the satellite macro model.
)";
#endif
/***********************************************/
#include "classes/miscAccelerations/miscAccelerations.h"
/***** CLASS ***********************************/
/** @brief Antenna thrust (simple model).
* @ingroup miscAccelerationsGroup
* @see MiscAccelerations */
class MiscAccelerationsAntennaThrust : public MiscAccelerationsBase
{
Double factor;
public:
MiscAccelerationsAntennaThrust(Config &config);
Vector3d acceleration(SatelliteModelPtr satellite, const Time &time, const Vector3d &position, const Vector3d &velocity,
const Rotary3d &rotSat, const Rotary3d &rotEarth, EphemeridesPtr ephemerides) override;
};
/***********************************************/
inline MiscAccelerationsAntennaThrust::MiscAccelerationsAntennaThrust(Config &config)
{
try
{
readConfig(config, "factor", factor, Config::DEFAULT, "1.0", "the result is multiplied by this factor");
if(isCreateSchema(config)) return;
}
catch(std::exception &e)
{
GROOPS_RETHROW(e)
}
}
/***********************************************/
inline Vector3d MiscAccelerationsAntennaThrust::acceleration(SatelliteModelPtr satellite, const Time &/*time*/,
const Vector3d &/*pos*/, const Vector3d &/*vel*/,
const Rotary3d &rotSat, const Rotary3d &rotEarth, EphemeridesPtr /*ephemerides*/)
{
try
{
if(!satellite)
throw(Exception("No satellite model given"));
return (-factor/satellite->mass/LIGHT_VELOCITY) * rotEarth.rotate(rotSat.rotate(satellite->thrustPower));
}
catch(std::exception &e)
{
GROOPS_RETHROW(e)
}
}
/***********************************************/
#endif
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