private void CalculateExtendedParameters()
{
if (IsStationary)
{
return;
}
// Calculate extended parameters.
// http://en.wikipedia.org/wiki/Standard_gravitational_parameter#Two_bodies_orbiting_each_other
GravitationalParameter = GameConstants.Science.GravitationalConstant * (_parentMass + _myMass) / (1000 * 1000 * 1000); // Normalize GravitationalParameter from m^3/s^2 to km^3/s^2
GravitationalParameterAU = GameConstants.Science.GravitationalConstant * (_parentMass + _myMass) / 3.347928976e33; // (149597870700 * 149597870700 * 149597870700);
// http://en.wikipedia.org/wiki/Orbital_period#Two_bodies_orbiting_each_other
double orbitalPeriod = 2 * Math.PI * Math.Sqrt(Math.Pow(Distance.AuToKm(SemiMajorAxis), 3) / (GravitationalParameter));
if (orbitalPeriod * 10000000 > long.MaxValue)
{
OrbitalPeriod = TimeSpan.MaxValue;
}
else
{
OrbitalPeriod = TimeSpan.FromSeconds(orbitalPeriod);
}
// http://en.wikipedia.org/wiki/Mean_motion
MeanMotion = Math.Sqrt(GravitationalParameter / Math.Pow(Distance.AuToKm(SemiMajorAxis), 3)); // Calculated in radians.
MeanMotion = Angle.ToDegrees(MeanMotion); // Stored in degrees.
Apoapsis = (1 + Eccentricity) * SemiMajorAxis;
Periapsis = (1 - Eccentricity) * SemiMajorAxis;
}
private void CalculateExtendedParameters()
{
if (IsStationary)
{
return;
}
// Calculate extended parameters.
// http://en.wikipedia.org/wiki/Standard_gravitational_parameter#Two_bodies_orbiting_each_other
GravitationalParameter_Km3S2 = GMath.GravitationalParameter_Km3s2(_parentMass + _myMass); // Normalize GravitationalParameter from m^3/s^2 to km^3/s^2
GravitationalParameterAU = GMath.GrabitiationalParameter_Au3s2(_parentMass + _myMass); // (149597870700 * 149597870700 * 149597870700);
GravitationalParameter_m3S2 = GMath.StandardGravitationalParameter(_parentMass + _myMass);
double orbitalPeriod = 2 * Math.PI * Math.Sqrt(Math.Pow(Distance.AuToKm(SemiMajorAxis_AU), 3) / (GravitationalParameter_Km3S2));
if (orbitalPeriod * 10000000 > long.MaxValue)
{
OrbitalPeriod = TimeSpan.MaxValue;
}
else
{
OrbitalPeriod = TimeSpan.FromSeconds(orbitalPeriod);
}
// http://en.wikipedia.org/wiki/Mean_motion
MeanMotion_DegreesSec = Math.Sqrt(GravitationalParameter_Km3S2 / Math.Pow(Distance.AuToKm(SemiMajorAxis_AU), 3)); // Calculated in radians.
MeanMotion_DegreesSec = Angle.ToDegrees(MeanMotion_DegreesSec); // Stored in degrees.
Apoapsis_AU = (1 + Eccentricity) * SemiMajorAxis_AU;
Periapsis_AU = (1 - Eccentricity) * SemiMajorAxis_AU;
SOI_m = OrbitMath.GetSOI(SemiMajorAxis, _myMass, _parentMass);
}
internal static void FirstRun(Entity entity)
{
CargoTransferDB datablob = entity.GetDataBlob <CargoTransferDB>();
double?dv;
if (entity.HasDataBlob <OrbitDB>() && datablob.CargoToEntity.HasDataBlob <OrbitDB>())
{
dv = CalcDVDifferenceKmPerSecond(entity.GetDataBlob <OrbitDB>(), datablob.CargoToEntity.GetDataBlob <OrbitDB>());
}
else
{
OrbitDB orbitDB;
if (entity.HasDataBlob <ColonyInfoDB>())
{
orbitDB = entity.GetDataBlob <ColonyInfoDB>().PlanetEntity.GetDataBlob <OrbitDB>();
}
else//if (datablob.CargoToEntity.HasDataBlob<ColonyInfoDB>())
{
orbitDB = datablob.CargoToEntity.GetDataBlob <ColonyInfoDB>().PlanetEntity.GetDataBlob <OrbitDB>();
}
dv = Distance.AuToKm(OrbitMath.MeanOrbitalVelocityInAU(orbitDB));
}
if (dv != null)
{
datablob.TransferRateInKG = CalcTransferRate((double)dv, datablob.CargoFromDB, datablob.CargoToDB);
}
}
/// <summary>
/// Calculates the DVD ifference.
/// </summary>
/// <returns>The delaV Difference in Km/s, null if not in imediate orbit</returns>
public static double?CalcDVDifferenceKmPerSecond(OrbitDB orbitDBFrom, OrbitDB orbitDBTo)
{
Entity toEntity = orbitDBTo.OwningEntity;
double?dv = null;
if (orbitDBFrom.Parent == toEntity) //Cargo going up the gravity well
{
dv = OrbitMath.MeanOrbitalVelocityInAU(orbitDBFrom);
}
else if (orbitDBFrom.Children.Contains(toEntity)) //Cargo going down the gravity well
{
dv = OrbitMath.MeanOrbitalVelocityInAU(orbitDBTo);
}
else if (orbitDBFrom.Parent == toEntity.GetDataBlob <OrbitDB>().Parent) //cargo going between objects orbiting the same body
{
dv = Math.Abs(OrbitMath.MeanOrbitalVelocityInAU(orbitDBFrom) - OrbitMath.MeanOrbitalVelocityInAU(orbitDBTo));
}
if (dv == null)
{
return(dv);
}
else
{
return(Distance.AuToKm((double)dv));
}
}
/// <summary>
/// Calculates the cartesian coordinates (relative to it's parent) of an orbit for a given angle.
/// </summary>
/// <param name="orbit">OrbitDB to calculate position from.</param>
/// <param name="trueAnomaly">Angle in Radians.</param>
public static Vector4 GetPosition(OrbitDB orbit, double trueAnomaly)
{
if (orbit.IsStationary)
{
return(new Vector4(0, 0, 0, 0));
}
// http://en.wikipedia.org/wiki/True_anomaly#Radius_from_true_anomaly
double radius = Distance.AuToKm(orbit.SemiMajorAxis) * (1 - orbit.Eccentricity * orbit.Eccentricity) / (1 + orbit.Eccentricity * Math.Cos(trueAnomaly));
// Adjust TrueAnomaly by the Argument of Periapsis (converted to radians)
trueAnomaly += Angle.ToRadians(orbit.ArgumentOfPeriapsis);
double inclination = Angle.ToRadians(orbit.Inclination);
// Convert KM to AU
radius = Distance.KmToAU(radius);
//https://downloads.rene-schwarz.com/download/M001-Keplerian_Orbit_Elements_to_Cartesian_State_Vectors.pdf
double lofAN = Angle.ToRadians(orbit.LongitudeOfAscendingNode);
double aofP = Angle.ToRadians(orbit.ArgumentOfPeriapsis);
double tA = trueAnomaly;
double incl = inclination;
double x = Math.Cos(lofAN) * Math.Cos(aofP + tA) - Math.Sin(lofAN) * Math.Sin(aofP + tA) * Math.Cos(incl);
double y = Math.Sin(lofAN) * Math.Cos(aofP + tA) + Math.Cos(lofAN) * Math.Sin(aofP + tA) * Math.Cos(incl);
double z = Math.Sin(incl) * Math.Sin(aofP + tA);
return(new Vector4(x, y, z, 0) * radius);
}
/// <summary>
/// This intercept only works if time to intercept is less than the orbital period.
/// </summary>
/// <returns>The ntercept.</returns>
/// <param name="mover">Mover.</param>
/// <param name="targetOrbit">Target orbit.</param>
/// <param name="atDateTime">At date time.</param>
public static (Vector3, TimeSpan) FTLIntercept(Entity mover, OrbitDB targetOrbit, DateTime atDateTime)
{
//OrbitDB targetOrbit = target.GetDataBlob<OrbitDB>();
//PositionDB targetPosition = target.GetDataBlob<PositionDB>();
//PositionDB moverPosition = mover.GetDataBlob<PositionDB>();
OrbitDB moverOrbit = mover.GetDataBlob <OrbitDB>();
Vector3 moverPosInKM = Distance.AuToKm(OrbitProcessor.GetAbsolutePosition_AU(moverOrbit, atDateTime));
PropulsionAbilityDB moverPropulsion = mover.GetDataBlob <PropulsionAbilityDB>();
Vector3 targetPosInKM = Distance.AuToKm((OrbitProcessor.GetAbsolutePosition_AU(targetOrbit, atDateTime)));
int speed = 25000;//moverPropulsion.MaximumSpeed * 100; //299792458;
(Vector3, TimeSpan)intercept = (new Vector3(), TimeSpan.Zero);
TimeSpan eti = new TimeSpan();
TimeSpan eti_prev = new TimeSpan();
DateTime edi = atDateTime;
DateTime edi_prev = atDateTime;
Vector3 predictedPosKM = Distance.AuToKm(OrbitProcessor.GetAbsolutePosition_AU(targetOrbit, edi_prev));
double distance = (predictedPosKM - moverPosInKM).Length();
eti = TimeSpan.FromSeconds((distance * 1000) / speed);
int steps = 0;
if (eti < targetOrbit.OrbitalPeriod)
{
double timeDifference = double.MaxValue;
double distanceDifference = timeDifference * speed;
while (distanceDifference >= 1000)
{
eti_prev = eti;
edi_prev = edi;
predictedPosKM = Distance.AuToKm(OrbitProcessor.GetAbsolutePosition_AU(targetOrbit, edi_prev));
distance = (predictedPosKM - moverPosInKM).Length();
eti = TimeSpan.FromSeconds((distance * 1000) / speed);
edi = atDateTime + eti;
timeDifference = Math.Abs(eti.TotalSeconds - eti_prev.TotalSeconds);
distanceDifference = timeDifference * speed;
steps++;
}
}
return(intercept);
}
/// <summary>
/// Creates on Orbit at current location from a given velocity
/// </summary>
/// <returns>The Orbit Does not attach the OrbitDB to the entity!</returns>
/// <param name="parent">Parent.</param>
/// <param name="entity">Entity.</param>
/// <param name="velocityAU">Velocity.</param>
public static OrbitDB FromVector(Entity parent, Entity entity, Vector3 velocityAU, DateTime atDateTime)
{
var parentMass = parent.GetDataBlob <MassVolumeDB>().Mass;
var myMass = entity.GetDataBlob <MassVolumeDB>().Mass;
var epoch1 = parent.Manager.ManagerSubpulses.StarSysDateTime; //getting epoch from here is incorrect as the local datetime doesn't change till after the subpulse.
var parentPos = OrbitProcessor.GetAbsolutePosition_AU(parent.GetDataBlob <OrbitDB>(), atDateTime); //need to use the parent position at the epoch
var posdb = entity.GetDataBlob <PositionDB>();
posdb.SetParent(parent);
var ralitivePos = posdb.RelativePosition_AU;//entity.GetDataBlob<PositionDB>().AbsolutePosition_AU - parentPos;
if (ralitivePos.Length() > OrbitProcessor.GetSOI(parent))
{
throw new Exception("Entity not in target SOI");
}
var sgp = GameConstants.Science.GravitationalConstant * (myMass + parentMass) / 3.347928976e33;
var ke = OrbitMath.KeplerFromPositionAndVelocity(sgp, ralitivePos, velocityAU, atDateTime);
var epoch = atDateTime;// - TimeSpan.FromSeconds(ke.Epoch); //ke.Epoch is seconds from periapsis.
OrbitDB orbit = new OrbitDB(parent, parentMass, myMass,
Math.Abs(ke.SemiMajorAxis),
ke.Eccentricity,
Angle.ToDegrees(ke.Inclination),
Angle.ToDegrees(ke.LoAN),
Angle.ToDegrees(ke.AoP),
Angle.ToDegrees(ke.MeanAnomalyAtEpoch),
epoch);
var pos = OrbitProcessor.GetPosition_AU(orbit, atDateTime);
var d = Distance.AuToKm(pos - ralitivePos).Length();
if (d > 1)
{
var e = new Event(atDateTime, "Positional difference of " + d + "Km when creating orbit from velocity");
e.Entity = entity;
e.SystemGuid = entity.Manager.ManagerGuid;
e.EventType = EventType.Opps;
//e.Faction = entity.FactionOwner;
StaticRefLib.EventLog.AddEvent(e);
//other info:
var keta = Angle.ToDegrees(ke.TrueAnomalyAtEpoch);
var obta = Angle.ToDegrees(OrbitProcessor.GetTrueAnomaly(orbit, atDateTime));
var tadif = Angle.ToDegrees(Angle.DifferenceBetweenRadians(keta, obta));
var pos1 = OrbitProcessor.GetPosition_AU(orbit, atDateTime);
var pos2 = OrbitProcessor.GetPosition_AU(orbit, ke.TrueAnomalyAtEpoch);
var d2 = Distance.AuToKm(pos1 - pos2).Length();
}
return(orbit);
}
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);
}
}
/// <summary>
/// Creates orbit here using the current distance between the two entites as aphelion(furthest distance) and a given semiMajorAxis
/// *NOTE BUG* this only returns a correct orbit DB if the position is y=0 and is +x (ie the position is in the reference direction)
/// </summary>
/// <returns>An OrbitDB. Does Not set DB to Entity.</returns>
/// <param name="shipEntity">Ship entity.</param>
/// <param name="parentEntity">The Entity to orbit</param>
/// <param name="semiMajorAxsis">Largest Radius</param>
public static OrbitDB CreateOrbitHereWithSemiMajAxis(Entity shipEntity, Entity parentEntity, double semiMajAxsisKM, DateTime time)
{
PositionDB parentPosition = parentEntity.GetDataBlob <PositionDB>();
PositionDB myPosition = shipEntity.GetDataBlob <PositionDB>();
double parentMass = parentEntity.GetDataBlob <MassVolumeDB>().Mass;
double myMass = shipEntity.GetDataBlob <MassVolumeDB>().Mass;
double aphelionAU = PositionDB.GetDistanceBetween(parentPosition, myPosition);
double semiMajAxisAU = semiMajAxsisKM / GameConstants.Units.KmPerAu;
double linierEcentricity = aphelionAU - semiMajAxisAU;
double semiMinorAxsis = Math.Sqrt(Math.Pow(semiMajAxisAU, 2) - Math.Pow(linierEcentricity, 2));
double ecentricity = linierEcentricity / semiMajAxisAU;
Vector3 ralitivePos = myPosition.RelativePosition_AU;
double angle = Math.Atan2(ralitivePos.Y, ralitivePos.X);
var theta = Angle.ToDegrees(angle);
OrbitDB newOrbit = OrbitDB.FromAsteroidFormat(parentEntity, parentMass, myMass, semiMajAxisAU, ecentricity, 0, 0, angle, angle, time);
var pos = OrbitProcessor.GetPosition_AU(newOrbit, time);
var pos2 = Distance.AuToKm(pos);
return(newOrbit);
}
/// <summary>
/// Calculates volume in Km^3 from a radius in Au.
/// </summary>
/// <param name="radius">Radius in AU</param>
/// <returns>Volume_km3 in Km^3</returns>
public static double CalculateVolume_Km3(double radius_au)
{
return((4.0 / 3.0) * Math.PI * Math.Pow(Distance.AuToKm(radius_au), 3));
}
public static Entity CreateShip(Entity classEntity, EntityManager systemEntityManager, Entity ownerFaction, Entity parent, StarSystem starsys, string shipName = null)
{
Vector3 position = parent.GetDataBlob <PositionDB>().AbsolutePosition_AU;
var distanceFromParent = parent.GetDataBlob <MassVolumeDB>().Radius * 2;
position.X += distanceFromParent;
Entity ship = CreateShip(classEntity, systemEntityManager, ownerFaction, position, starsys, shipName);
ship.GetDataBlob <PositionDB>().SetParent(parent);
var orbitDB = ShipMovementProcessor.CreateOrbitHereWithSemiMajAxis(ship, parent, Distance.AuToKm(distanceFromParent), systemEntityManager.ManagerSubpulses.StarSysDateTime);
ship.SetDataBlob(orbitDB);
return(ship);
}
/// <summary>
/// This was designed so that fast moving objects will get interpolated a lot more than slow moving objects
/// so fast moving objects shouldn't loose positional acuracy when close to a planet,
/// and slow moving objects won't have processor time wasted on them by calulcating too often.
/// However this seems to be unstable and looses energy, unsure why. currently set it to just itterate/interpolate every second.
/// so currently will be using more time to get through this than neccisary.
/// </summary>
/// <param name="entity">Entity.</param>
/// <param name="deltaSeconds">Delta seconds.</param>
public static void NewtonMove(Entity entity, int deltaSeconds)
{
NewtonMoveDB newtonMoveDB = entity.GetDataBlob <NewtonMoveDB>();
PositionDB positionDB = entity.GetDataBlob <PositionDB>();
double Mass_Kg = entity.GetDataBlob <MassVolumeDB>().Mass;
double ParentMass_kg = newtonMoveDB.ParentMass;
var manager = entity.Manager;
DateTime dateTimeFrom = newtonMoveDB.LastProcessDateTime;
DateTime dateTimeNow = manager.ManagerSubpulses.StarSysDateTime;
DateTime dateTimeFuture = dateTimeNow + TimeSpan.FromSeconds(deltaSeconds);
double deltaT = (dateTimeFuture - dateTimeFrom).TotalSeconds;
double secondsToItterate = deltaT;
while (secondsToItterate > 0)
{
double speed_kms = newtonMoveDB.CurrentVector_kms.Length();
//double timeStep = Math.Max(secondsToItterate / speed_kms, 1);
//timeStep = Math.Min(timeStep, secondsToItterate);
double timeStep = 1;//because the above seems unstable and looses energy.
double distanceToParent_m = Distance.AuToMt(positionDB.GetDistanceTo(newtonMoveDB.SOIParent.GetDataBlob <PositionDB>()));
distanceToParent_m = Math.Max(distanceToParent_m, 0.1); //don't let the distance be 0 (once collision is in this will likely never happen anyway)
double gravForce = GameConstants.Science.GravitationalConstant * (Mass_Kg * ParentMass_kg / Math.Pow(distanceToParent_m, 2));
Vector3 gravForceVector = gravForce * -Vector3.Normalise(positionDB.RelativePosition_AU);
double distance = Distance.AuToKm(positionDB.RelativePosition_AU).Length();
Vector3 totalForce = gravForceVector + newtonMoveDB.ThrustVector;
Vector3 acceleration_mps = totalForce / Mass_Kg;
Vector3 newVelocity = (acceleration_mps * timeStep * 0.001) + newtonMoveDB.CurrentVector_kms;
newtonMoveDB.CurrentVector_kms = newVelocity;
Vector3 deltaPos = (newtonMoveDB.CurrentVector_kms + newVelocity) / 2 * timeStep;
//Vector4 deltaPos = newtonMoveDB.CurrentVector_kms * timeStep;
positionDB.RelativePosition_AU += Distance.KmToAU(deltaPos);
double sOIRadius_AU = OrbitProcessor.GetSOI(newtonMoveDB.SOIParent);
if (positionDB.RelativePosition_AU.Length() >= sOIRadius_AU)
{
Entity newParent;
Vector3 parentRalitiveVector;
//if our parent is a regular kepler object (normaly this is the case)
if (newtonMoveDB.SOIParent.HasDataBlob <OrbitDB>())
{
var orbitDB = newtonMoveDB.SOIParent.GetDataBlob <OrbitDB>();
newParent = orbitDB.Parent;
var parentVelocity = OrbitProcessor.InstantaneousOrbitalVelocityVector(orbitDB, entity.Manager.ManagerSubpulses.StarSysDateTime);
parentRalitiveVector = Distance.KmToAU(newtonMoveDB.CurrentVector_kms) + parentVelocity;
var pvlen = Distance.AuToKm(parentVelocity.Length());
var vlen = newtonMoveDB.CurrentVector_kms.Length();
var rvlen = Distance.AuToKm(parentRalitiveVector.Length());
}
else //if (newtonMoveDB.SOIParent.HasDataBlob<NewtonMoveDB>())
{ //this will pretty much never happen.
newParent = newtonMoveDB.SOIParent.GetDataBlob <NewtonMoveDB>().SOIParent;
var parentVelocity = newtonMoveDB.SOIParent.GetDataBlob <NewtonMoveDB>().CurrentVector_kms;
parentRalitiveVector = Distance.KmToAU(newtonMoveDB.CurrentVector_kms + parentVelocity);
}
double newParentMass = newParent.GetDataBlob <MassVolumeDB>().Mass;
double sgp = GameConstants.Science.GravitationalConstant * (newParentMass + Mass_Kg) / 3.347928976e33;
Vector3 posRalitiveToNewParent = positionDB.AbsolutePosition_AU - newParent.GetDataBlob <PositionDB>().AbsolutePosition_AU;
var dateTime = dateTimeNow + TimeSpan.FromSeconds(deltaSeconds - secondsToItterate);
var kE = OrbitMath.KeplerFromPositionAndVelocity(sgp, posRalitiveToNewParent, parentRalitiveVector, dateTime);
if (kE.Eccentricity < 1) //if we're going to end up in a regular orbit around our new parent
{
/*
* var newOrbit = OrbitDB.FromKeplerElements(
* newParent,
* newParentMass,
* Mass_Kg,
* kE,
* dateTime);
*/
var newOrbit = OrbitDB.FromVector(newParent, entity, parentRalitiveVector, dateTime);
entity.RemoveDataBlob <NewtonMoveDB>();
entity.SetDataBlob(newOrbit);
positionDB.SetParent(newParent);
var currentPos = Distance.AuToKm(positionDB.RelativePosition_AU);
var newPos = OrbitProcessor.GetPosition_AU(newOrbit, dateTime);
var newPosKM = Distance.AuToKm(newPos);
positionDB.RelativePosition_AU = newPos;
break;
}
else //else we're in a hyperbolic trajectory around our new parent, so just coninue the newtonion move.
{
positionDB.SetParent(newParent);
newtonMoveDB.ParentMass = newParentMass;
newtonMoveDB.SOIParent = newParent;
}
}
secondsToItterate -= timeStep;
}
newtonMoveDB.LastProcessDateTime = dateTimeFuture;
}
// sets the speed of the ship to the maximum speed allowed in the direction of the target.
// Returns true if the destination has been reached or the target no longer exists.
public override bool processOrder()
{
double speedMultiplier = 1.0; //was this just for debugging? if so we should remove it, if not, then maybe move it to game settings?
double minimumDistance = 1000.0;
PositionDB currentPosition = Owner.GetDataBlob <PositionDB>();
PositionDB targetPosition = null;
double AUSpeed, kmSpeed;
kmSpeed = Owner.GetDataBlob <PropulsionDB>().MaximumSpeed *speedMultiplier;
AUSpeed = Distance.KmToAU(kmSpeed);
currentPosition.SetParent(null);
if (PositionTarget != null)
{
// just head straight towards the target position
targetPosition = PositionTarget;
// Assume that 1000 is extremely close,
if (Distance.AuToKm(distanceBetweenPositions(currentPosition, targetPosition)) <= minimumDistance)
{
setPositionToTarget(Owner, targetPosition);
Owner.GetDataBlob <PropulsionDB>().CurrentSpeed = new Vector4(0, 0, 0, 0);
return(true);
}
else
{
Owner.GetDataBlob <PropulsionDB>().CurrentSpeed = getSpeed(currentPosition, targetPosition, kmSpeed);
return(false);
}
}
else if (Target == null || Target == Entity.InvalidEntity) // Target no longer exists
{
return(true);
}
else
{
targetPosition = Target.GetDataBlob <PositionDB>();
// Assume that 1000 is extremely close,
if (Distance.AuToKm(distanceBetweenPositions(currentPosition, targetPosition)) <= minimumDistance)
{
setPositionToTarget(Owner, targetPosition);
currentPosition.SetParent(Target);
return(true);
}
if (Target.HasDataBlob <OrbitDB>())
{
if (Target.GetDataBlob <OrbitDB>().IsStationary)
{
// just head straight towards the target position
targetPosition = Target.GetDataBlob <PositionDB>();
Owner.GetDataBlob <PropulsionDB>().CurrentSpeed = getSpeed(currentPosition, targetPosition, kmSpeed);
}
else
{
// TODO: Figure out an intercept based on OrbitProcessor.GetPosition
// for now, just head straight towards the target position
targetPosition = Target.GetDataBlob <PositionDB>();
Owner.GetDataBlob <PropulsionDB>().CurrentSpeed = getSpeed(currentPosition, targetPosition, kmSpeed);
return(false);
}
}
else if (Target.HasDataBlob <PropulsionDB>())
{
if (Target.GetDataBlob <PropulsionDB>().MaximumSpeed >= Owner.GetDataBlob <PropulsionDB>().MaximumSpeed)
// Target is faster than our ship, and cannot intercept
{
// Just head in a straight line
targetPosition = Target.GetDataBlob <PositionDB>();
Owner.GetDataBlob <PropulsionDB>().CurrentSpeed = getSpeed(currentPosition, targetPosition, kmSpeed);
}
else
{
// Calculate an intercept
targetPosition = Target.GetDataBlob <PositionDB>();
Vector4 targetPos = new Vector4(targetPosition.X, targetPosition.Y, targetPosition.Z, 0);
Vector4 currentPos = new Vector4(currentPosition.X, currentPosition.Y, currentPosition.Z, 0);
targetPos = Find_collision_point(targetPos, Target.GetDataBlob <PropulsionDB>().CurrentSpeed, currentPos, AUSpeed);
targetPosition = new PositionDB(targetPos, targetPosition.SystemGuid);
Owner.GetDataBlob <PropulsionDB>().CurrentSpeed = getSpeed(currentPosition, targetPosition, kmSpeed);
}
}
}
return(false);
}