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YASIM: move updating of model from Airplane to Wing

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This commit is contained in:
Henning Stahlke 2017-11-19 23:30:35 +01:00
parent fb6f965db7
commit 6b473fde68
3 changed files with 31 additions and 22 deletions
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20
src/FDM/YASim/Airplane.cpp
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@ -310,25 +310,7 @@ float Airplane::compileWing(Wing* w)
}
float wgt = 0;
for(int i=0; i<w->numSurfaces(); i++) {
Surface* s = (Surface*)w->getSurface(i);
float td = s->getDragCoefficient();
int sid = s->getID();
_model.addSurface(s);
float mass = w->getSurfaceWeight(i);
mass = mass * Math::sqrt(mass);
float pos[3];
s->getPosition(pos);
int mid = _model.getBody()->addMass(mass, pos, true);
if (_wingsN != 0) {
SGPropertyNode_ptr n = _wingsN->getNode("surfaces", true)->getChild("surface", sid, true);
n->getNode("drag", true)->setFloatValue(td);
n->getNode("mass-id", true)->setIntValue(mid);
}
wgt += mass;
}
wgt = w->updateModel(&_model);
return wgt;
}

29
src/FDM/YASim/Wing.cpp
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@ -1,4 +1,5 @@
#include "yasim-common.hpp"
#include "Model.hpp"
#include "Surface.hpp"
#include "Wing.hpp"
@ -361,8 +362,8 @@ void Wing::writeInfoToProptree()
float dragSum = 0;
for(int surf=0; surf < numSurfaces(); surf++) {
Surface* s = (Surface*)getSurface(surf);
float td = s->getDragCoefficient();
dragSum += td;
float drag = s->getDragCoefficient();
dragSum += drag;
float mass = getSurfaceWeight(surf);
mass = mass * Math::sqrt(mass);
@ -371,4 +372,28 @@ void Wing::writeInfoToProptree()
_wingN->getNode("weight", true)->setFloatValue(wgt);
_wingN->getNode("drag", true)->setFloatValue(dragSum);
}
float Wing::updateModel(Model* model)
{
float wgt = 0;
for(int surf=0; surf < numSurfaces(); surf++) {
Surface* s = (Surface*)getSurface(surf);
model->addSurface(s);
float mass = getSurfaceWeight(surf);
mass = mass * Math::sqrt(mass);
wgt += mass;
float pos[3];
s->getPosition(pos);
int mid = model->getBody()->addMass(mass, pos, true);
if (_wingN != nullptr) {
SGPropertyNode_ptr n = _wingN->getNode("surfaces", true)->getChild("surface", s->getID(), true);
n->getNode("drag", true)->setFloatValue(s->getDragCoefficient());
n->getNode("mass-id", true)->setIntValue(mid);
}
}
return wgt;
}
}; // namespace yasim

4
src/FDM/YASim/Wing.hpp
View file

@ -9,6 +9,7 @@
namespace yasim {
class Surface;
class Model;
struct FlapParams {
float start {0};
@ -99,6 +100,7 @@ public:
float getLiftRatio() const { return _liftRatio; }
void setPropertyNode(SGPropertyNode_ptr n) { _wingN = n; };
float updateModel(Model* model);
private:
void interp(const float* v1, const float* v2, const float frac, float* out);
@ -112,7 +114,7 @@ private:
void addSurface(Surface* s, float weight, float twist);
void writeInfoToProptree();
struct SurfRec { Surface * surface; float weight; };
// all surfaces of this wing