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flightgear/src/FDM/YASim/PistonEngine.hpp

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#ifndef _PISTONENGINE_HPP
#define _PISTONENGINE_HPP
#include "Engine.hpp"
namespace yasim {
class PistonEngine : public Engine {
public:
virtual PistonEngine* isPistonEngine() { return this; }
// Initializes an engine from known "takeoff" parameters.
PistonEngine(float power, float spd);
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void setTurboParams(float mul, float maxMP);
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void setDisplacement(float d);
void setCompression(float c);
void setWastegate(float norm) { _wastegate = norm; }
void setSupercharger(float hasSuper) { _hasSuper = hasSuper; }
void setTurboLag(float lag) { _turboLag = lag; }
bool isCranking();
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float getMP();
float getEGT();
float getMaxPower(); // max sea-level power
float getBoost() { return _boostPressure; }
float getOilTemp() { return _oilTemp; }
virtual void calc(float pressure, float temp, float speed);
virtual void stabilize();
virtual void integrate(float dt);
virtual float getTorque();
virtual float getFuelFlow();
private:
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// Static configuration:
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float _power0; // reference power setting
float _omega0; // " engine speed
float _rho0; // " manifold air density
float _f0; // "ideal" fuel flow at P0/omega0
float _mixCoeff; // fuel flow per omega at full mixture
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float _turbo; // (or super-)charger pressure multiplier
bool _hasSuper; // true indicates gear-driven (not turbo)
float _turboLag; // turbo lag time in seconds
float _charge; // current {turbo|super}charge multiplier
float _chargeTarget; // eventual charge value
float _maxMP; // static maximum pressure
float _wastegate; // wastegate setting, [0:1]
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float _displacement; // piston stroke volume
float _compression; // compression ratio (>1)
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// Runtime state/output:
float _mp;
float _torque;
float _fuelFlow;
float _egt;
float _boostPressure;
float _oilTemp;
float _oilTempTarget;
float _dOilTempdt;
};
}; // namespace yasim
#endif // _PISTONENGINE_HPP