private void ApplyAngularMomentum()
{
FlightGlobals.ActiveVessel.IgnoreGForces(2);
if (PreviousBodyName == FlightGlobals.ActiveVessel.mainBody)
{
Krakensbane.ResetVelocityFrame(true);
if ((FlightGlobals.ActiveVessel.orbit.eccentricity >= 1) && (ElipMode == 0)) //For Hyperbolic Orbits. Conserve angular momentum by making orbit.h constant. GMp=h^2, so semi-latus rectum must be constant as well.).
{
Speed = Math.Sqrt(FlightGlobals.ActiveVessel.mainBody.gravParameter * ((2 / FlightGlobals.ActiveVessel.orbit.radius) - ((SemiLatusOriginal * FlightGlobals.ActiveVessel.mainBody.gravParameter) / (FlightGlobals.ActiveVessel.orbit.semiMajorAxis * OriginalMomentumSqr))));
var VelocityOffset = (TravelDirection * Speed);
FlightGlobals.ActiveVessel.SetWorldVelocity(VelocityOffset);
}
if ((FlightGlobals.ActiveVessel.orbit.eccentricity < 1) && (ElipMode == 1)) // For Elliptical Orbits. Conserve Angular Momentum directly by altering state vectors
{
Speed = OriginalSpeed * (OriginalFrameTrueRadius / (FlightGlobals.ActiveVessel.orbit.radius));
var VelocityOffset = (TravelDirection * Speed);
FlightGlobals.ActiveVessel.SetWorldVelocity(VelocityOffset);
if (((FlightGlobals.ActiveVessel.orbit.radius / OriginalFrameTrueRadius) >= 0.85) || ((FlightGlobals.ActiveVessel.orbit.radius / OriginalFrameTrueRadius) <= 1.15)) // re-set variables when ratio between current ratio and original gets too far from 1
{
OriginalSpeed = Vector3d.Magnitude(FlightGlobals.ActiveVessel.orbit.GetRelativeVel());
OriginalFrameTrueRadius = FlightGlobals.ActiveVessel.orbit.radius;
}
}
}
if (((FlightGlobals.ActiveVessel.orbit.eccentricity < 1) && (ElipMode == 0)) || ((FlightGlobals.ActiveVessel.orbit.eccentricity > 1) && (ElipMode == 1)) || (PreviousBodyName != FlightGlobals.currentMainBody))
{
if (PreviousBodyName != FlightGlobals.ActiveVessel.mainBody)
{
SetAMStartStateVars();
}
}
}
