void FindRV(OrbitalElements oe, double time, out Vector3d r, out Vector3d v)
{
var tempOe = oe.CopyOE();
tempOe.tra = OrbitalTools.Program.anomalyAfterTime(OrbitData.parentGM, oe, time);
OrbitalTools.Util.oe2rv(OrbitData.parentGM, tempOe, out r, out v);
}
//assumes time is absolute
void FindRV(OrbitalElements oe, double absTime, out Vector3d r, out Vector3d v)
{
var tempOe = oe.CopyOE();
//Note: SHOULD be oe.computeTime, not mComputeTime
tempOe.tra = OrbitalTools.Program.anomalyAfterTime(OrbitData.parentGM, oe, absTime - oe.computeTime);
OrbitalTools.Util.oe2rv(OrbitData.parentGM, tempOe, out r, out v);
}
public OrbitalElements GetOE()
{
//TODO move this into OrbitalElements class as an overload assignment operator
return oe.CopyOE();
}
