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
* }
*/
}
private void CalculateTotalAeroForce()
{
aeroForces.ClearAll();
if (_vessel.dynamicPressurekPa <= 0.00001)
{
return;
}
if (_currentAeroModules == null)
{
return;
}
foreach (FARAeroPartModule m in _currentAeroModules)
{
if (m is null)
{
continue;
}
aeroForces.AddForce(m.transform.position, m.totalWorldSpaceAeroForce);
aeroForces.AddTorque(m.worldSpaceTorque);
}
}
void UpdateAerodynamicCenter()
{
FARCenterQuery aeroSection, dummy;
aeroSection = new FARCenterQuery();
dummy = new FARCenterQuery();
if ((object)EditorLogic.RootPart == null)
{
return;
}
Vector3 vel_base, vel_fuzz;
Transform rootPartTrans = EditorLogic.RootPart.partTransform;
if (EditorDriver.editorFacility == EditorFacility.SPH)
{
vel_base = Vector3.forward;
vel_fuzz = 0.02f * Vector3.up;
}
else
{
vel_base = Vector3.up;
vel_fuzz = -0.02f * Vector3.forward;
}
Vector3 vel = (vel_base - vel_fuzz).normalized;
for (int i = 0; i < _currentAeroSections.Count; i++)
{
FARAeroSection section = _currentAeroSections[i];
section.PredictionCalculateAeroForces(1, 3, 100000, 0.005f, vel, aeroSection);
}
FARBaseAerodynamics.PrecomputeGlobalCenterOfLift(aeroSection, dummy, vel, 1);
Vector3 pos = Vector3.zero;//rootPartTrans.position;
float mass = 0;
for (int i = 0; i < EditorLogic.SortedShipList.Count; i++)
{
Part p = EditorLogic.SortedShipList[i];
float tmpMass = p.mass + p.GetResourceMass();
mass += tmpMass;
pos += p.partTransform.position * tmpMass;
}
pos /= mass;
Vector3 avgForcePos = Vector3.zero;
Vector3 force0, moment0;
force0 = aeroSection.force;
moment0 = aeroSection.TorqueAt(pos);
avgForcePos += aeroSection.GetPos();
//aeroSection.force = -aeroSection.force;
//aeroSection.torque = -aeroSection.torque;
aeroSection.ClearAll();
vel = (vel_base + vel_fuzz).normalized;
for (int i = 0; i < _currentAeroSections.Count; i++)
{
FARAeroSection section = _currentAeroSections[i];
section.PredictionCalculateAeroForces(1, 3, 100000, 0.005f, vel, aeroSection);
}
FARBaseAerodynamics.PrecomputeGlobalCenterOfLift(aeroSection, dummy, vel, 1);
Vector3 force1, moment1;
force1 = aeroSection.force;
moment1 = aeroSection.TorqueAt(pos);
avgForcePos += aeroSection.GetPos();
aeroSection.ClearAll();
avgForcePos *= 0.5f;
Vector3 deltaForce = force1 - force0;
Vector3 deltaMoment = moment1 - moment0;
Vector3 deltaForcePerp = Vector3.ProjectOnPlane(deltaForce, vel_base);
float deltaForcePerpMag = deltaForcePerp.magnitude;
Vector3 deltaForcePerpNorm = deltaForcePerp / deltaForcePerpMag;
Vector3 deltaMomentPerp = deltaMoment - Vector3.Dot(deltaMoment, deltaForcePerpNorm) * deltaForcePerpNorm - Vector3.Project(deltaMoment, vel_base);
//float dist = deltaMomentPerp.magnitude / deltaForcePerpMag;
//vesselRootLocalAeroCenter = vel_base * dist;
vesselRootLocalAeroCenter = deltaMomentPerp.magnitude / deltaForcePerpMag * vel_base * Math.Sign(Vector3.Dot(Vector3.Cross(deltaForce, deltaMoment), vel_base));
//Debug.Log(dist + " " + deltaMomentPerp.magnitude + " " + deltaForcePerpMag);
//vesselRootLocalAeroCenter += avgForcePos;
//avgForcePos = rootPartTrans.worldToLocalMatrix.MultiplyPoint3x4(avgForcePos);
//vesselRootLocalAeroCenter += Vector3.ProjectOnPlane(avgForcePos, Vector3.up);
//vesselRootLocalAeroCenter = aeroSection.GetPos();
vesselRootLocalAeroCenter += pos;//Vector3.ProjectOnPlane(avgForcePos - pos, vesselRootLocalAeroCenter) + pos;
vesselRootLocalAeroCenter = rootPartTrans.worldToLocalMatrix.MultiplyPoint3x4(vesselRootLocalAeroCenter);
}
private void UpdateAerodynamicCenter()
{
var aeroSection = new FARCenterQuery();
var dummy = new FARCenterQuery();
if (EditorLogic.RootPart is null)
{
return;
}
Vector3 vel_base, vel_fuzz;
Transform rootPartTrans = EditorLogic.RootPart.partTransform;
if (EditorDriver.editorFacility == EditorFacility.SPH)
{
vel_base = Vector3.forward;
vel_fuzz = 0.02f * Vector3.up;
}
else
{
vel_base = Vector3.up;
vel_fuzz = -0.02f * Vector3.forward;
}
Vector3 vel = (vel_base - vel_fuzz).normalized;
foreach (FARAeroSection section in _currentAeroSections)
{
section.PredictionCalculateAeroForces(1, 0.5f, 100000, 0, 0.005f, vel, aeroSection);
}
FARBaseAerodynamics.PrecomputeGlobalCenterOfLift(aeroSection, dummy, vel, 1);
Vector3 pos = Vector3.zero;
float mass = 0;
foreach (Part p in EditorLogic.SortedShipList)
{
if (FARAeroUtil.IsNonphysical(p))
{
continue;
}
float tmpMass = p.mass + p.GetResourceMass();
mass += tmpMass;
pos += p.partTransform.position * tmpMass;
}
pos /= mass;
Vector3 force0 = aeroSection.force;
Vector3 moment0 = aeroSection.TorqueAt(pos);
aeroSection.ClearAll();
vel = (vel_base + vel_fuzz).normalized;
foreach (FARAeroSection section in _currentAeroSections)
{
section.PredictionCalculateAeroForces(1, 0.5f, 100000, 0, 0.005f, vel, aeroSection);
}
FARBaseAerodynamics.PrecomputeGlobalCenterOfLift(aeroSection, dummy, vel, 1);
Vector3 force1 = aeroSection.force;
Vector3 moment1 = aeroSection.TorqueAt(pos);
aeroSection.ClearAll();
Vector3 deltaForce = force1 - force0;
Vector3 deltaMoment = moment1 - moment0;
Vector3 deltaForcePerp = Vector3.ProjectOnPlane(deltaForce, vel_base);
float deltaForcePerpMag = deltaForcePerp.magnitude;
Vector3 deltaForcePerpNorm = deltaForcePerp / deltaForcePerpMag;
Vector3 deltaMomentPerp = deltaMoment -
Vector3.Dot(deltaMoment, deltaForcePerpNorm) * deltaForcePerpNorm -
Vector3.Project(deltaMoment, vel_base);
vesselRootLocalAeroCenter = deltaMomentPerp.magnitude /
deltaForcePerpMag *
Math.Sign(Vector3.Dot(Vector3.Cross(deltaForce, deltaMoment), vel_base)) *
vel_base;
vesselRootLocalAeroCenter += pos;
vesselRootLocalAeroCenter = rootPartTrans.worldToLocalMatrix.MultiplyPoint3x4(vesselRootLocalAeroCenter);
}