/// <summary>
/// Add an element to the sequence using r0/v0/t0 initial conditions.
///
/// Position and velocity are with respect to the center body (NOT world/physics space!).
///
/// Orbit segements must be added in increasing time order.
/// </summary>
/// <param name="r0"></param>
/// <param name="v0"></param>
/// <param name="time"></param>
/// <param name="relativePos"></param>
/// <param name="body"></param>
/// <param name="centerBody"></param>
/// <param name="callback">(Optional) Method to call when sequence starts</param>
/// <returns></returns>
public OrbitUniversal AppendElementRVT(Vector3d r0,
Vector3d v0,
double time,
bool relativePos,
NBody body,
NBody centerBody,
ElementStarted callback)
{
if (BadTime(time))
{
return(null);
}
KeplerElement ke = new KeplerElement
{
timeStart = time,
callback = callback,
returnToGE = false
};
OrbitUniversal orbit = orbitsGO.AddComponent <OrbitUniversal>();
orbit.centerNbody = centerBody;
orbit.SetNBody(body);
orbit.InitFromRVT(r0, v0, time, centerBody, relativePos);
orbit.evolveMode = OrbitUniversal.EvolveMode.KEPLERS_EQN;
ke.orbit = orbit;
keplerElements.Add(ke);
return(orbit);
}
/// <summary>
/// Add an element to the sequence that begins at time and evolves based on the orbit data provided.
///
/// Orbit elements must be added in increasing time order.
/// </summary>
/// <param name="time"></param>
/// <param name="orbitData"></param>
/// <param name="body"></param>
/// <param name="centerBody"></param>
/// <param name="callback">(Optional) Method to call when sequence starts</param>
/// <returns></returns>
public OrbitUniversal AppendElementOrbitData(double time,
OrbitData orbitData,
NBody body,
NBody centerBody,
ElementStarted callback)
{
if (BadTime(time))
{
return(null);
}
KeplerElement ke = new KeplerElement
{
timeStart = time,
returnToGE = false,
callback = callback
};
OrbitUniversal orbit = orbitsGO.AddComponent <OrbitUniversal>();
orbit.centerNbody = centerBody;
orbit.SetNBody(body);
orbit.InitFromOrbitData(orbitData, time);
orbit.evolveMode = OrbitUniversal.EvolveMode.KEPLERS_EQN;
ke.orbit = orbit;
keplerElements.Add(ke);
return(orbit);
}
public void AppendReturnToGE(double time, NBody body)
{
KeplerElement ke = new KeplerElement();
ke.timeStart = time;
ke.returnToGE = true;
keplerElements.Add(ke);
}
/// <summary>
/// Add an element using an existing OrbitUniversal instance
///
/// Orbit elements must be added in increasing time order.
/// </summary>
/// <param name="orbitU"></param>
/// <param name="callback">(Optional) Method to call when sequence starts</param>
public void AppendElementExistingOrbitU(OrbitUniversal orbitU, ElementStarted callback)
{
if (BadTime(orbitU.GetStartTime()))
{
return;
}
KeplerElement ke = new KeplerElement
{
timeStart = orbitU.GetStartTime(),
returnToGE = false
};
ke.orbit = orbitU;
ke.callback = callback;
keplerElements.Add(ke);
}
/// <summary>
/// Add orbit segements for each of the maneuvers. The maneuvers must have been created by transfer code
/// that populated the fields: relativeTo, relativePos, relativeVel and time fields.
///
/// </summary>
/// <param name="list"></param>
public void AddManeuvers(List <Maneuver> maneuverList)
{
foreach (Maneuver m in maneuverList)
{
if (m.relativeTo != null)
{
Debug.LogFormat("Maneuver: relPos={0} phyPos={1} t={2}", m.relativePos, m.physPosition, m.worldTime);
AppendElementRVT(m.relativePos, m.relativeVel, m.worldTime, true, m.nbody, m.relativeTo, null);
// add the maneuver to the KE so callback can be used
KeplerElement ke = keplerElements[keplerElements.Count - 1];
ke.maneuver = m;
}
else
{
Debug.LogError("Could not add maneuver. Missing relativeTo information. Skipped.");
}
}
}
public void Evolve(double physicsTime, ref double[] r)
{
if ((activeElement < keplerElements.Count - 1) &&
(physicsTime > keplerElements[activeElement + 1].timeStart))
{
// Advance to next element
activeElement++;
GravityEngine ge = GravityEngine.Instance();
KeplerElement activeKE = keplerElements[activeElement];
if (activeKE.returnToGE)
{
#pragma warning disable 162 // disable unreachable code warning
if (GravityEngine.DEBUG)
{
Debug.Log("return to GE:" + gameObject.name);
}
#pragma warning restore 162
KeplerElement priorKE = keplerElements[activeElement - 1];
priorKE.orbit.Evolve(physicsTime, ref r);
Vector3d pos = priorKE.orbit.GetPositionDouble();
Vector3d vel = priorKE.orbit.GetVelocityDouble();
ge.BodyOffRails(nbody, pos, vel);
return;
}
else
{
// if the center object of the orbit changes, need to recompute the KeplerDepth and update
if (keplerElements[activeElement - 1].orbit.centerNbody != activeKE.orbit.centerNbody)
{
NewCenter(activeKE.orbit);
}
// move on to the next orbit in the sequence
activeKE.orbit.PreEvolve(ge.physToWorldFactor, ge.massScale);
if (activeKE.callback != null)
{
activeKE.callback(activeKE.orbit);
}
if ((activeKE.maneuver != null) && (activeKE.maneuver.onExecuted != null))
{
activeKE.maneuver.onExecuted(activeKE.maneuver);
}
}
#pragma warning disable 162 // disable unreachable code warning
if (GravityEngine.DEBUG)
{
Debug.LogFormat("Changed to segment {0} tnow={1} tseg={2} ", activeElement, physicsTime,
keplerElements[activeElement].timeStart);
}
#pragma warning restore 162
}
else if (physicsTime < keplerElements[activeElement].timeStart)
{
// Use an earlier element (happens if time set to earlier)
int lastElement = activeElement;
while (physicsTime < keplerElements[activeElement].timeStart && (activeElement >= 0))
{
activeElement--;
// if the center object of the orbit changes, need to recompute the KeplerDepth and update
if (keplerElements[lastElement].orbit.centerNbody != keplerElements[activeElement].orbit.centerNbody)
{
NewCenter(keplerElements[activeElement].orbit);
}
}
}
if (!keplerElements[activeElement].returnToGE)
{
// time for evolve is absolute - up to OrbitUniversal to make it relative to their time0
keplerElements[activeElement].orbit.Evolve(physicsTime, ref r);
}
}
