void InsertionCalcs()
{
_deltaV_MS = _newtonUI.DeltaV;
OrbitDB targetOrbit = TargetEntity.Entity.GetDataBlob <OrbitDB>();
(Vector3 position, DateTime eti)targetIntercept = OrbitProcessor.GetInterceptPosition_m(OrderingEntityState.Entity, TargetEntity.Entity.GetDataBlob <OrbitDB>(), _departureDateTime);
DateTime estArivalDateTime = targetIntercept.eti; //rough calc.
Vector3 insertionVector = OrbitProcessor.GetOrbitalInsertionVector_m(_departureOrbitalVelocity_m, targetOrbit, estArivalDateTime); //_departureOrbitalVelocity - parentOrbitalVector;
_insertionOrbitalVelocity_m = insertionVector;
_insertionOrbitalVelocity_m += _deltaV_MS;
_insertionOrbitalSpeed_m = _insertionOrbitalVelocity_m.Length();
_insertionAngle = Math.Atan2(_insertionOrbitalVelocity_m.Y, _insertionOrbitalVelocity_m.X);
_moveWidget.SetArivalProgradeAngle(_insertionAngle);
/*
* var sgpCBAU = GameConstants.Science.GravitationalConstant * (_massCurrentBody + _massOrderingEntity) / 3.347928976e33;// (149597870700 * 149597870700 * 149597870700);
* var ralPosCBAU = OrderingEntity.Entity.GetDataBlob<PositionDB>().RelativePosition_AU;
* var smaCurrOrbtAU = OrderingEntity.Entity.GetDataBlob<OrbitDB>().SemiMajorAxis;
* var velAU = OrbitProcessor.PreciseOrbitalVector(sgpCBAU, ralPosCBAU, smaCurrOrbtAU);
*/
}