private void LEGACY_UpdateWingAeroModels(bool updateWingInteractions)
{
List <Part> partsList = EditorLogic.SortedShipList;
_wingAerodynamicModel.Clear();
for (int i = 0; i < partsList.Count; i++)
{
Part p = partsList[i];
if (p != null)
{
if (p.Modules.Contains <FARWingAerodynamicModel>())
{
FARWingAerodynamicModel w = p.Modules.GetModule <FARWingAerodynamicModel>();
if (updateWingInteractions)
{
w.EditorUpdateWingInteractions();
}
_wingAerodynamicModel.Add(w);
}
else if (p.Modules.Contains <FARControllableSurface>())
{
FARControllableSurface c = p.Modules.GetModule <FARControllableSurface>();
if (updateWingInteractions)
{
c.EditorUpdateWingInteractions();
}
_wingAerodynamicModel.Add(c);
}
}
}
}
private void LEGACY_UpdateWingAeroModels(bool updateWingInteractions)
{
List <Part> partsList = EditorLogic.SortedShipList;
_wingAerodynamicModel.Clear();
foreach (Part p in partsList)
{
if (p == null)
{
continue;
}
if (p.Modules.Contains <FARWingAerodynamicModel>())
{
FARWingAerodynamicModel w = p.Modules.GetModule <FARWingAerodynamicModel>();
if (updateWingInteractions)
{
w.EditorUpdateWingInteractions();
}
_wingAerodynamicModel.Add(w);
}
else if (p.Modules.Contains <FARControllableSurface>())
{
FARControllableSurface c = p.Modules.GetModule <FARControllableSurface>();
if (updateWingInteractions)
{
c.EditorUpdateWingInteractions();
}
_wingAerodynamicModel.Add(c);
}
}
}
/// <summary>
/// Sets spoilers to a certain value on this vessel
/// </summary>
public static void VesselSetSpoilers(Vessel v, bool spoilerActive)
{
foreach (Part p in v.parts)
{
if (!p.Modules.Contains <FARControllableSurface>())
{
continue;
}
FARControllableSurface surface = p.Modules.GetModule <FARControllableSurface>();
surface.brake = spoilerActive;
}
}
/// <summary>
/// Decreases flap deflection level for all control surfaces on this vessel, down to min setting of 0
/// </summary>
public static void VesselDecreaseFlapDeflection(Vessel v)
{
foreach (Part p in v.parts)
{
if (!p.Modules.Contains <FARControllableSurface>())
{
continue;
}
FARControllableSurface surface = p.Modules.GetModule <FARControllableSurface>();
surface.SetDeflection(surface.flapDeflectionLevel - 1);
}
}
protected override void DI_Start(StartState state)
{
if (HighLogic.LoadedSceneIsFlight)
{
this.controlSurfaceModule = this.part.Modules.OfType <FARControllableSurface>().Single();
this.wasFlap = controlSurfaceModule.isFlap;
this.AoAFromFlap = typeof(FARControllableSurface).GetField("AoAFromFlap", BindingFlags.NonPublic);
this.AoAOffset = typeof(FARControllableSurface).GetField("AoAOffset", BindingFlags.NonPublic);
if (AoAOffset == null || AoAFromFlap == null)
{
throw new Exception("Could not get the field info from FAR!");
}
}
}
/// <summary>
/// Returns spoiler setting for this vessel
/// </summary>
/// <param name="v"></param>
/// <returns>Spoiler setting; true indicates active spoilers, false indicates inactive or no spoilers in existence</returns>
public static bool VesselSpoilerSetting(Vessel v)
{
foreach (Part p in v.parts)
{
if (!p.Modules.Contains <FARControllableSurface>())
{
continue;
}
FARControllableSurface surface = p.Modules.GetModule <FARControllableSurface>();
if (surface.isSpoiler)
{
return(surface.brake);
}
}
return(false);
}
/// <summary>
/// Returns flap setting for this vessel
/// </summary>
/// <param name="v"></param>
/// <returns>Flap setting; 0 - 3 indicates no to full flap deflections; -1 indicates lack of any control surface parts</returns>
public static int VesselFlapSetting(Vessel v)
{
foreach (Part p in v.parts)
{
if (!p.Modules.Contains <FARControllableSurface>())
{
continue;
}
FARControllableSurface surface = p.Modules.GetModule <FARControllableSurface>();
if (surface.isFlap)
{
return(surface.flapDeflectionLevel);
}
}
return(-1);
}
private void partModuleUpdate(PartModule pm)
{
if (isFarLoaded && pm is FARControllableSurface)
{
FARControllableSurface fcs = (FARControllableSurface)pm;
if (vessel.atmDensity > 0)
{
Vector3d forcePosition = fcs.AerodynamicCenter - vesselState.CoM;
Vector3 velocity = fcs.GetVelocity();
double soundspeed, v_scalar = velocity.magnitude;
double rho = FARAeroUtil.GetCurrentDensity(vessel, out soundspeed);
if (rho <= 0.0 || v_scalar <= 0.1 || fcs.isShielded)
{
return;
}
// First we save the curent state of the part
double YmaxForce = fcs.YmaxForce;
double XZmaxForce = fcs.XZmaxForce;
double AoAcurrentFlap = (double)(FieldAoAcurrentFlap.GetValue(fcs));
double MaxAoAdesiredControl = 0;
if (fcs.pitchaxis != 0.0)
{
MaxAoAdesiredControl += (double)(FieldPitchLocation.GetValue(fcs)) * fcs.pitchaxis * 0.01;
}
if (fcs.yawaxis != 0.0)
{
MaxAoAdesiredControl += (double)(FieldYawLocation.GetValue(fcs)) * fcs.yawaxis * 0.01;;
}
if (fcs.rollaxis != 0.0)
{
MaxAoAdesiredControl += (double)(FieldRollLocation.GetValue(fcs)) * fcs.rollaxis * 0.01;;
}
MaxAoAdesiredControl *= fcs.maxdeflect;
if (fcs.pitchaxisDueToAoA != 0.0)
{
double _AoA = (fcs as FARWingAerodynamicModel).CalculateAoA(velocity.normalized);
_AoA = FARMathUtil.rad2deg * Math.Asin(_AoA);
if (double.IsNaN(_AoA))
{
_AoA = 0;
}
MaxAoAdesiredControl += _AoA * fcs.pitchaxisDueToAoA * 0.01;
}
MaxAoAdesiredControl = FARMathUtil.Clamp(MaxAoAdesiredControl, -Math.Abs(fcs.maxdeflect), Math.Abs(fcs.maxdeflect));
double MachNumber = v_scalar / soundspeed;
fcs.YmaxForce = double.MaxValue;
fcs.XZmaxForce = double.MaxValue;
// Then we turn it one way
double AoA = fcs.CalculateAoA(velocity, AoAcurrentFlap + MaxAoAdesiredControl);
vesselState.ctrlTorqueAvailable.Add(vessel.GetTransform().InverseTransformDirection(Vector3.Cross(forcePosition, fcs.CalculateForces(velocity, MachNumber, AoA))));
// We restore it to the initial state
AoA = fcs.CalculateAoA(velocity);
fcs.CalculateForces(velocity, MachNumber, AoA);
// And we turn it the other way
AoA = fcs.CalculateAoA(velocity, AoAcurrentFlap - MaxAoAdesiredControl);
vesselState.ctrlTorqueAvailable.Add(vessel.GetTransform().InverseTransformDirection(Vector3.Cross(forcePosition, fcs.CalculateForces(velocity, MachNumber, AoA))));
// And in the end we restore its initial state
AoA = fcs.CalculateAoA(velocity);
fcs.CalculateForces(velocity, MachNumber, AoA);
fcs.YmaxForce = YmaxForce;
fcs.XZmaxForce = XZmaxForce;
}
}
}
