private void ApplyIntakeDrag(float currentRamDrag, Vector3 vesselVelNorm, float dynPres)
{
for (int i = _intakeTransforms.Count - 1; i >= 0; i--)
{
ModuleResourceIntake intake = _intakeModules[i];
if (!intake.intakeEnabled)
{
continue;
}
Transform transform = _intakeTransforms[i];
if (transform == null)
{
_intakeModules.RemoveAt(i);
_intakeTransforms.RemoveAt(i);
_aeroModulesWithIntakes.RemoveAt(i);
//++i;
continue;
}
float cosAoA = Vector3.Dot(_intakeTransforms[i].forward, vesselVelNorm);
if (cosAoA < 0)
{
cosAoA = 0;
}
if (cosAoA <= 0)
{
continue;
}
FARAeroPartModule aeroModule = _aeroModulesWithIntakes[i];
Vector3 force = -aeroModule.partLocalVelNorm * cosAoA * currentRamDrag * (float)intake.area * 100f;
//if(float.IsNaN(force.sqrMagnitude))
// force = Vector3.zero;
aeroModule.AddLocalForce(force, Vector3.zero);
}
}
private void ApplyIntakeDrag(float currentRamDrag, Vector3 vesselVelNorm, float dynPres)
{
for (int i = 0; i < _intakeTransforms.Count; i++)
{
ModuleResourceIntake intake = _intakeModules[i];
if (!intake.intakeEnabled)
{
continue;
}
Transform transform = _intakeTransforms[i];
if (transform == null)
{
_intakeModules.RemoveAt(i);
_intakeTransforms.RemoveAt(i);
_aeroModulesWithIntakes.RemoveAt(i);
--i;
continue;
}
float cosAoA = Vector3.Dot(_intakeTransforms[i].forward, vesselVelNorm);
if (cosAoA < 0)
{
cosAoA = 0;
}
if (cosAoA <= intake.aoaThreshold)
{
continue;
}
FARAeroPartModule aeroModule = _aeroModulesWithIntakes[i];
aeroModule.AddLocalForce(-aeroModule.partLocalVelNorm * dynPres * cosAoA * currentRamDrag * intake.area * 100, Vector3.zero);
}
}