internal override void ActionCommand(Game game)
{
if (!IsRunning)
{
(Vector3 pos, DateTime eti)targetIntercept = InterceptCalcs.GetInterceptPosition(_entityCommanding, _targetEntity.GetDataBlob <OrbitDB>(), TransitStartDateTime, TargetOffsetPosition_AU);
OrbitDB orbitDB = _entityCommanding.GetDataBlob <OrbitDB>();
Vector3 currentPos = OrbitProcessor.GetAbsolutePosition_AU(orbitDB, TransitStartDateTime);
var ralPos = OrbitProcessor.GetPosition_AU(orbitDB, TransitStartDateTime);
var masses = _entityCommanding.GetDataBlob <MassVolumeDB>().Mass + orbitDB.Parent.GetDataBlob <MassVolumeDB>().Mass;
var sgp = GameConstants.Science.GravitationalConstant * masses / 3.347928976e33;
//Vector4 currentVec = OrbitProcessor.PreciseOrbitalVector(sgp, ralPos, orbitDB.SemiMajorAxis);
Vector2 currentVec = OrbitProcessor.GetOrbitalVector(orbitDB, TransitStartDateTime);
_db = new TranslateMoveDB(targetIntercept.pos);
_db.TranslateRalitiveExit_AU = TargetOffsetPosition_AU;
_db.EntryDateTime = TransitStartDateTime;
_db.PredictedExitTime = targetIntercept.eti;
_db.TranslateEntryPoint_AU = currentPos;
_db.SavedNewtonionVector_AU = currentVec;
_db.ExpendDeltaV_AU = ExpendDeltaV;
if (_targetEntity.HasDataBlob <SensorInfoDB>())
{
_db.TargetEntity = _targetEntity.GetDataBlob <SensorInfoDB>().DetectedEntity;
}
else
{
_db.TargetEntity = _targetEntity;
}
if (EntityCommanding.HasDataBlob <OrbitDB>())
{
EntityCommanding.RemoveDataBlob <OrbitDB>();
}
EntityCommanding.SetDataBlob(_db);
TranslateMoveProcessor.StartNonNewtTranslation(EntityCommanding);
IsRunning = true;
var distance = (currentPos - targetIntercept.Item1).Length();
var distancekm = Distance.AuToKm(distance);
var time = targetIntercept.Item2 - TransitStartDateTime;
double spd = _entityCommanding.GetDataBlob <PropulsionAbilityDB>().MaximumSpeed_MS;
spd = Distance.MToAU(spd);
var distb = spd * time.TotalSeconds;
var distbKM = Distance.AuToKm(distb);
var dif = distancekm - distbKM;
//Assert.AreEqual(distancekm, distbKM);
}
}
internal override void ActionCommand(Game game)
{
if (!IsRunning)
{
var targetIntercept = InterceptCalcs.GetInterceptPosition(_entityCommanding, _targetEntity.GetDataBlob <OrbitDB>(), _entityCommanding.Manager.ManagerSubpulses.StarSysDateTime);
_db = new TranslateMoveDB(targetIntercept.Item1);
_db.EntryDateTime = _entityCommanding.Manager.ManagerSubpulses.StarSysDateTime;
_db.PredictedExitTime = targetIntercept.Item2;
_db.TranslateEntryPoint_AU = _entityCommanding.GetDataBlob <PositionDB>().AbsolutePosition_AU;
_db.TargetEntity = _targetEntity;
if (EntityCommanding.HasDataBlob <OrbitDB>())
{
EntityCommanding.RemoveDataBlob <OrbitDB>();
}
EntityCommanding.SetDataBlob(_db);
TranslateMoveProcessor.StartNonNewtTranslation(EntityCommanding);
IsRunning = true;
}
}
public static double CalcDVDifference_m(Entity entity1, Entity entity2)
{
double dvDif = 0;
Entity parent;
double parentMass;
double sgp;
double r1;
double r2;
Entity soi1 = Entity.GetSOIParentEntity(entity1);
Entity soi2 = Entity.GetSOIParentEntity(entity2);
if (soi1 == soi2)
{
parent = soi1;
parentMass = parent.GetDataBlob <MassVolumeDB>().MassDry;
sgp = OrbitMath.CalculateStandardGravityParameterInM3S2(0, parentMass);
var state1 = Entity.GetRalitiveState(entity1);
var state2 = Entity.GetRalitiveState(entity2);
r1 = state1.pos.Length();
r2 = state2.pos.Length();
}
else
{
StaticRefLib.EventLog.AddEvent(new Event("Cargo calc failed, entities must have same soi parent"));
return(double.PositiveInfinity);
}
var hohmann = InterceptCalcs.Hohmann(sgp, r1, r2);
return(dvDif = hohmann[0].deltaV.Length() + hohmann[1].deltaV.Length());
}
