122 lines
3 KiB
C++
122 lines
3 KiB
C++
#ifndef _WING_HPP
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#define _WING_HPP
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#include "Vector.hpp"
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namespace yasim {
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class Surface;
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// FIXME: need to handle "inverted" controls for mirrored wings.
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class Wing {
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public:
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Wing();
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~Wing();
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// Do we mirror ourselves about the XZ plane?
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void setMirror(bool mirror);
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// Wing geometry:
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void setBase(float* base); // in local coordinates
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void setLength(float length); // dist. ALONG wing (not span!)
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void setChord(float chord); // at base, measured along X axis
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void setTaper(float taper); // fraction, 0-1
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void setSweep(float sweep); // radians
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void setDihedral(float dihedral); // radians, positive is "up"
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void setStall(float aoa);
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void setStallWidth(float angle);
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void setStallPeak(float fraction);
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void setCamber(float camber);
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void setIncidence(float incidence);
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void setFlap0(float start, float end, float lift, float drag);
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void setFlap1(float start, float end, float lift, float drag);
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void setSpoiler(float start, float end, float lift, float drag);
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void setSlat(float start, float end, float aoa, float drag);
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// Set the control axes for the sub-surfaces
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void setFlap0(float lval, float rval);
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void setFlap1(float lval, float rval);
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void setSpoiler(float lval, float rval);
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void setSlat(float val);
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// Compile the thing into a bunch of Surface objects
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void compile();
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void getTip(float* tip);
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bool isMirrored();
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// Ground effect information
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float getGroundEffect(float* posOut);
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// Query the list of Surface objects
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int numSurfaces();
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Surface* getSurface(int n);
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float getSurfaceWeight(int n);
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// The overall drag coefficient for the wing as a whole. Units are
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// arbitrary.
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void setDragScale(float scale);
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float getDragScale();
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// The ratio of force along the Z (lift) direction of each wing
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// segment to that along the X (drag) direction.
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void setLiftRatio(float ratio);
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float getLiftRatio();
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private:
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void interp(float* v1, float* v2, float frac, float* out);
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Surface* newSurface(float* pos, float* orient, float chord,
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bool flap0, bool flap1, bool slat, bool spoiler);
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struct SurfRec { Surface * surface; float weight; };
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Vector _surfs;
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Vector _flap0Surfs;
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Vector _flap1Surfs;
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Vector _slatSurfs;
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Vector _spoilerSurfs;
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bool _mirror;
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float _base[3];
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float _length;
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float _chord;
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float _taper;
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float _sweep;
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float _dihedral;
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float _stall;
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float _stallWidth;
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float _stallPeak;
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float _camber;
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float _incidence;
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float _dragScale;
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float _liftRatio;
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float _flap0Start;
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float _flap0End;
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float _flap0Lift;
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float _flap0Drag;
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float _flap1Start;
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float _flap1End;
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float _flap1Lift;
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float _flap1Drag;
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float _spoilerStart;
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float _spoilerEnd;
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float _spoilerLift;
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float _spoilerDrag;
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float _slatStart;
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float _slatEnd;
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float _slatAoA;
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float _slatDrag;
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};
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}; // namespace yasim
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#endif // _WING_HPP
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