public Orbit(global::Orbit kspOrbit)
{
this.meanAnomalyAtEpoch = kspOrbit.meanAnomalyAtEpoch;
this.LAN = kspOrbit.LAN;
this.ReferenceBody = kspOrbit.referenceBody.name;
this.epoch = kspOrbit.epoch;
this.eccentricity = kspOrbit.eccentricity;
this.semiMajorAxis = kspOrbit.semiMajorAxis;
this.argumentOfPeriapsis = kspOrbit.argumentOfPeriapsis;
this.inclination = kspOrbit.inclination;
}
public void update(global::Orbit orbit, double time)
{
mainBody.update(orbit.referenceBody);
inclination = orbit.inclination * Math.PI / 180;
LAN = orbit.LAN * Math.PI / 180;
eccentricity = orbit.eccentricity;
parameter = new Vector3(orbit.h).magnitudeSquare / mainBody.gravParameter;
argumentOfPeriapsis = orbit.argumentOfPeriapsis * Math.PI / 180;
trueAnomaly = orbit.trueAnomaly * Math.PI / 180;
timeAtPeriapsis = time - timeFromPeriapsis;
}
/// <summary>
/// Construct a an orbit from a KSP orbit object.
/// </summary>
public Orbit(global::Orbit orbit)
{
InternalOrbit = orbit;
}
