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Adrian Musceac: #303, YASim solver settings

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The internal solver of YASim which computes drag and lift
coefficients now actually uses the values configured in
the XML input file for approach fuel, cruise fuel and cruise
glide angle.
This commit is contained in:
ThorstenB 2011-04-15 00:15:18 +02:00
parent d88dcba5e8
commit 7f5a0e3518
1 changed files with 3 additions and 3 deletions
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6
src/FDM/YASim/Airplane.cpp
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@ -671,8 +671,8 @@ void Airplane::compile()
t->handle = body->addMass(0, t->pos);
totalFuel += t->cap;
}
_cruiseWeight = _emptyWeight + totalFuel*0.5f;
_approachWeight = _emptyWeight + totalFuel*0.2f;
_cruiseWeight = _emptyWeight + totalFuel*_cruiseFuel;
_approachWeight = _emptyWeight + totalFuel*_approachFuel;
body->recalc();
@ -795,7 +795,7 @@ void Airplane::setupWeights(bool isApproach)
void Airplane::runCruise()
{
setupState(_cruiseAoA, _cruiseSpeed,_approachGlideAngle, &_cruiseState);
setupState(_cruiseAoA, _cruiseSpeed,_cruiseGlideAngle, &_cruiseState);
_model.setState(&_cruiseState);
_model.setAir(_cruiseP, _cruiseT,
Atmosphere::calcStdDensity(_cruiseP, _cruiseT));