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flightgear/src/FDM/YASim/Rotorpart.hpp

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#ifndef _ROTORPART_HPP
#define _ROTORPART_HPP
namespace yasim {
class Rotorpart
{
public:
Rotorpart();
// Position of this surface in local coords
void setPosition(float* p);
void getPosition(float* out);
void setPositionForceAttac(float* p);
void getPositionForceAttac(float* out);
void setNormal(float* p);
void getNormal(float* out);
void setMaxPitchForce(float force);
void setCollective(float pos);
void setCyclic(float pos);
void setSpeed(float* p);
void setDirectionofZentipetalforce(float* p);
void setZentipetalForce(float f);
void setMaxpitch(float f);
void setMinpitch(float f);
void setMaxcyclic(float f);
void setMincyclic(float f);
void setDelta3(float f);
void setDynamic(float f);
void setTranslift(float f);
void setC2(float f);
void setZentForce(float f);
void setRelLenHinge(float f);
void setRelamp(float f);
float getAlpha(int i);
float getrealAlpha(void);
char* getAlphaoutput(int i);
void setAlphaoutput(char *text,int i);
void inititeration(float dt,float *rot);
float getWeight(void);
void setWeight(float value);
void calcForce(float* v, float rho, float* forceOut, float* torqueOut);
void setlastnextrp(Rotorpart*lastrp,Rotorpart*nextrp,Rotorpart *oppositerp);
void setTorque(float torque_max_force,float torque_no_force);
void setOmega(float value);
void setOmegaN(float value);
float getIncidence();
float getPhi();
void setAlphamin(float f);
void setAlphamax(float f);
void setAlpha0(float f);
void setAlpha0factor(float f);
void setLen(float value);
private:
void strncpy(char *dest,const char *src,int maxlen);
Rotorpart *_lastrp,*_nextrp,*_oppositerp;
float _dt;
float _pos[3]; // position in local coords
float _posforceattac[3]; // position in local coords
float _normal[3]; //direcetion of the rotation axis
float _torque_max_force;
float _torque_no_force;
float _speed[3];
float _directionofzentipetalforce[3];
float _zentipetalforce;
float _maxpitch;
float _minpitch;
float _maxpitchforce;
float _maxcyclic;
float _mincyclic;
float _cyclic;
float _collective;
float _delta3;
float _dynamic;
float _translift;
float _c2;
float _mass;
float _alpha;
float _alphaalt;
float _alphamin,_alphamax,_alpha0,_alpha0factor;
float _rellenhinge;
float _relamp;
float _omega,_omegan;
float _phi;
float _len;
float _incidence;
char _alphaoutputbuf[2][256];
int _alpha2type;
};
}; // namespace yasim
#endif // _ROTORPART_HPP