/// <summary>
/// In Meters!
/// </summary>
/// <param name="parent"></param>
/// <param name="myMass"></param>
/// <param name="parentMass"></param>
/// <param name="sgp_m"></param>
/// <param name="position_m"></param>
/// <param name="velocity_m"></param>
/// <param name="atDateTime"></param>
/// <returns></returns>
/// <exception cref="Exception"></exception>
public static OrbitDB FromVector(Entity parent, double myMass, double parentMass, double sgp_m, Vector3 position_m, Vector3 velocity_m, DateTime atDateTime)
{
if (position_m.Length() > OrbitProcessor.GetSOI_AU(parent))
{
throw new Exception("Entity not in target SOI");
}
//var sgp = GameConstants.Science.GravitationalConstant * (myMass + parentMass) / 3.347928976e33;
var ke = OrbitMath.KeplerFromPositionAndVelocity(sgp_m, position_m, velocity_m, atDateTime);
OrbitDB orbit = new OrbitDB(parent)
{
SemiMajorAxis = ke.SemiMajorAxis,
Eccentricity = ke.Eccentricity,
Inclination = ke.Inclination,
LongitudeOfAscendingNode = ke.LoAN,
ArgumentOfPeriapsis = ke.AoP,
MeanAnomalyAtEpoch = ke.MeanAnomalyAtEpoch,
Epoch = atDateTime,
_parentMass = parent.GetDataBlob <MassVolumeDB>().Mass,
_myMass = myMass
};
orbit.CalculateExtendedParameters();
var pos = OrbitProcessor.GetAbsolutePosition_m(orbit, atDateTime);
return(orbit);
}
/// <summary>
/// Gets a future position for this entity, regarless of wheter it's orbit or newtonion trajectory
/// </summary>
/// <param name="entity"></param>
/// <param name="atDateTime"></param>
/// <param name="ralitive"></param>
/// <returns>In Meters</returns>
/// <exception cref="Exception"></exception>
public static Vector3 GetPosition_m(Entity entity, DateTime atDateTime, bool ralitive = true)
{
if (entity.HasDataBlob<OrbitDB>())
{
if (ralitive)
return OrbitProcessor.GetPosition_m(entity.GetDataBlob<OrbitDB>(), atDateTime);
else
return OrbitProcessor.GetAbsolutePosition_m(entity.GetDataBlob<OrbitDB>(), atDateTime);
}
else if (entity.HasDataBlob<NewtonMoveDB>())
{
if (ralitive)
return NewtonionMovementProcessor.GetPositon_m(entity, entity.GetDataBlob<NewtonMoveDB>(), atDateTime).pos;
else
return NewtonionMovementProcessor.GetAbsulutePositon_m(entity, entity.GetDataBlob<NewtonMoveDB>(), atDateTime).pos;
}
else if (entity.HasDataBlob<PositionDB>())
{
if(ralitive)
return entity.GetDataBlob<PositionDB>().RelativePosition_m;
else
return entity.GetDataBlob<PositionDB>().AbsolutePosition_m;
}
else
{
throw new Exception("Entity is positionless");
}
}
/// <summary>
/// Gets a future position for this entity, regarless of wheter it's orbit or newtonion trajectory
/// </summary>
/// <param name="entity"></param>
/// <param name="atDateTime"></param>
/// <returns>In Meters</returns>
/// <exception cref="Exception"> if entity doesn't have one of the correct datablobs</exception>
public static Vector3 GetAbsoluteFuturePosition(Entity entity, DateTime atDateTime)
{
if (entity.HasDataBlob <OrbitDB>())
{
return(OrbitProcessor.GetAbsolutePosition_m(entity.GetDataBlob <OrbitDB>(), atDateTime));
}
else if (entity.HasDataBlob <OrbitUpdateOftenDB>())
{
return(OrbitProcessor.GetAbsolutePosition_m(entity.GetDataBlob <OrbitUpdateOftenDB>(), atDateTime));
}
else if (entity.HasDataBlob <NewtonMoveDB>())
{
return(NewtonionMovementProcessor.GetAbsoluteState(entity, entity.GetDataBlob <NewtonMoveDB>(), atDateTime).pos);
}
else if (entity.HasDataBlob <PositionDB>())
{
return(entity.GetDataBlob <PositionDB>().AbsolutePosition_m);
}
else
{
throw new Exception("Entity is positionless");
}
}
/// <summary>
/// creates an asteroid that will collide with the given entity on the given date.
/// </summary>
/// <param name="starSys"></param>
/// <param name="target"></param>
/// <param name="collisionDate"></param>
/// <returns></returns>
public static Entity CreateAsteroid(StarSystem starSys, Entity target, DateTime collisionDate, double asteroidMass = -1.0)
{
//todo rand these a bit.
double radius = Distance.KmToAU(0.5);
double mass;
if (asteroidMass < 0)
{
mass = 1.5e+12; //about 1.5 billion tonne
}
else
{
mass = asteroidMass;
}
var speed = 40000;
Vector3 velocity = new Vector3(speed, 0, 0);
var massVolume = MassVolumeDB.NewFromMassAndRadius_AU(mass, radius);
var planetInfo = new SystemBodyInfoDB();
var name = new NameDB("Ellie");
var AsteroidDmg = new AsteroidDamageDB();
AsteroidDmg.FractureChance = new PercentValue(0.75f);
var dmgPfl = EntityDamageProfileDB.AsteroidDamageProfile(massVolume.Volume_km3, massVolume.Density, massVolume.RadiusInM, 50);
var sensorPfil = new SensorProfileDB();
planetInfo.SupportsPopulations = false;
planetInfo.BodyType = BodyType.Asteroid;
Vector3 targetPos = OrbitProcessor.GetAbsolutePosition_m(target.GetDataBlob <OrbitDB>(), collisionDate);
TimeSpan timeToCollision = collisionDate - StaticRefLib.CurrentDateTime;
var parent = target.GetDataBlob <OrbitDB>().Parent;
var parentMass = parent.GetDataBlob <MassVolumeDB>().Mass;
var myMass = massVolume.Mass;
double sgp = OrbitMath.CalculateStandardGravityParameterInM3S2(myMass, parentMass);
OrbitDB orbit = OrbitDB.FromVector(parent, myMass, parentMass, sgp, targetPos, velocity, collisionDate);
var currentpos = OrbitProcessor.GetAbsolutePosition_AU(orbit, StaticRefLib.CurrentDateTime);
var posDB = new PositionDB(currentpos.X, currentpos.Y, currentpos.Z, parent.Manager.ManagerGuid, parent);
var planetDBs = new List <BaseDataBlob>
{
posDB,
massVolume,
planetInfo,
name,
orbit,
AsteroidDmg,
dmgPfl,
sensorPfil
};
Entity newELE = new Entity(starSys, planetDBs);
return(newELE);
}
/// <summary>
///
/// </summary>
/// <param name="moverAbsolutePos"></param>
/// <param name="speed"></param>
/// <param name="targetOrbit"></param>
/// <param name="atDateTime"></param>
/// <param name="offsetPosition">position ralitive to the target object we wish to stop warp.</param>
/// <returns></returns>
public static (Vector3 position, DateTime etiDateTime) GetInterceptPosition_m(Vector3 moverAbsolutePos, double speed, OrbitDB targetOrbit, DateTime atDateTime, Vector3 offsetPosition = new Vector3())
{
var pos = moverAbsolutePos;
double tim = 0;
var pl = new obit()
{
position = moverAbsolutePos,
T = targetOrbit.OrbitalPeriod.TotalSeconds,
};
double a = targetOrbit.SemiMajorAxis * 2;
Vector3 p;
int i;
double tt, t, dt, a0, a1, T;
// find orbital position with min error (coarse)
a1 = -1.0;
dt = 0.01 * pl.T;
for (t = 0; t < pl.T; t += dt)
{
p = OrbitProcessor.GetAbsolutePosition_m(targetOrbit, atDateTime + TimeSpan.FromSeconds(t)); //pl.position(sim_t + t); // try time t
p += offsetPosition;
tt = Vector3.Magnitude(p - pos) / speed; //length(p - pos) / speed;
a0 = tt - t; if (a0 < 0.0)
{
continue; // ignore overshoots
}
a0 /= pl.T; // remove full periods from the difference
a0 -= Math.Floor(a0);
a0 *= pl.T;
if ((a0 < a1) || (a1 < 0.0))
{
a1 = a0;
tim = tt;
} // remember best option
}
// find orbital position with min error (fine)
for (i = 0; i < 10; i++) // recursive increase of accuracy
{
for (a1 = -1.0, t = tim - dt, T = tim + dt, dt *= 0.1; t < T; t += dt)
{
p = OrbitProcessor.GetAbsolutePosition_m(targetOrbit, atDateTime + TimeSpan.FromSeconds(t)); //p = pl.position(sim_t + t); // try time t
p += offsetPosition;
tt = Vector3.Magnitude(p - pos) / speed; //tt = length(p - pos) / speed;
a0 = tt - t; if (a0 < 0.0)
{
continue; // ignore overshoots
}
a0 /= pl.T; // remove full periods from the difference
a0 -= Math.Floor(a0);
a0 *= pl.T;
if ((a0 < a1) || (a1 < 0.0))
{
a1 = a0;
tim = tt;
} // remember best option
}
}
// direction
p = OrbitProcessor.GetAbsolutePosition_m(targetOrbit, atDateTime + TimeSpan.FromSeconds(tim));//pl.position(sim_t + tim);
p += offsetPosition;
//dir = normalize(p - pos);
return(p, atDateTime + TimeSpan.FromSeconds(tim));
}