private void CalculateTotalAeroForce()
{
totalAeroForceVector = Vector3.zero;
if (_vessel.dynamicPressurekPa <= 0.00001)
{
return;
}
if (_currentAeroModules != null)
{
for (int i = 0; i < _currentAeroModules.Count; i++)
{
FARAeroPartModule m = _currentAeroModules[i];
if ((object)m != null)
{
totalAeroForceVector += m.totalWorldSpaceAeroForce;
}
}
}
/*for (int i = 0; i < _LEGACY_currentWingAeroModel.Count; i++)
* {
* FARWingAerodynamicModel w = _LEGACY_currentWingAeroModel[i];
* if ((object)w != null)
* totalAeroForceVector += w.worldSpaceForce;
* }*/
/*for(int i = 0; i < _vessel.parts.Count; i++)
* {
* Part p = _vessel.parts[i];
* totalAeroForceVector += -p.dragVectorDir * p.dragScalar; // dragVectorDir is actually the velocity vector direction
* }*/
}
private void CalculateTotalAeroForce()
{
aeroForces.ClearAll();
if (_vessel.dynamicPressurekPa <= 0.00001)
{
return;
}
if (_currentAeroModules != null)
{
for (int i = 0; i < _currentAeroModules.Count; i++)
{
FARAeroPartModule m = _currentAeroModules[i];
if ((object)m != null)
{
aeroForces.AddForce(m.transform.position, m.totalWorldSpaceAeroForce);
aeroForces.AddTorque(m.worldSpaceTorque);
}
}
}
/*
* for (int i = 0; i < _LEGACY_currentWingAeroModel.Count; i++)
* {
* FARWingAerodynamicModel w = _LEGACY_currentWingAeroModel[i];
* if ((object)w == null)
* continue;
* totalAeroForceVector += w.worldSpaceForce;
* aeroForces.AddForce(w.AerodynamicCenter, w.worldSpaceForce);
*
* totalAeroForceVector += w.worldSpaceForce;
* totalAeroTorqueVector += Vector3.Cross(w.AerodynamicCenter - _vessel.CoM, w.worldSpaceForce);
* }
*
* for(int i = 0; i < _vessel.parts.Count; i++)
* {
* Part p = _vessel.parts[i];
* totalAeroForceVector += -p.dragVectorDir * p.dragScalar; // dragVectorDir is actually the velocity vector direction
* }
*/
}