public void HyperOmegaLNoInclNoPhase()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
const float orbitPeri = 15f;
GameObject planet = TestSetupUtils.CreatePlanetInHyper(star, 1f);
OrbitHyper orbitHyper = planet.GetComponent <OrbitHyper>();
orbitHyper.ecc = 1.4f;
orbitHyper.perihelion = orbitPeri;
orbitHyper.r_initial = orbitPeri;
// Try some values of om
float[] omegaValues = { 30f, 45f, 60f, 90f, 135f, 180f, 0f };
foreach (float omega in omegaValues)
{
orbitHyper.omega_lc = omega;
orbitHyper.Init();
orbitHyper.InitNBody(1f, 1f);
orbitHyper.Log(System.Reflection.MethodBase.GetCurrentMethod().Name);
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("omega = " + omega + " od.omega_l=" + od.omega_lc);
// Need a bit of leeway at 0 with error
Assert.IsTrue(FloatEqual(omega, od.omega_lc, 0.05));
TestRV(od, planet, star);
}
}
/// <summary>
/// Raise a circular orbit by the specified percent
/// - only on-rail is implemented
/// </summary>
/// <param name="percentRaise"></param>
private void NewCircularOrbit(float percentRaise)
{
if (onRails)
{
KeplerSequence keplerSeq = spaceship.GetComponent <KeplerSequence>();
OrbitUniversal orbitU = keplerSeq.GetCurrentOrbit();
// check orbit is circular
if (orbitU.eccentricity < 1E-2)
{
// circular, ok to proceed
OrbitData fromOrbit = new OrbitData(orbitU);
OrbitData toOrbit = new OrbitData(fromOrbit);
toOrbit.a = percentRaise * fromOrbit.a;
const bool rendezvous = false;
OrbitTransfer hohmannXfer = new HohmannXfer(fromOrbit, toOrbit, rendezvous);
keplerSeq.RemoveFutureSegments();
keplerSeq.AddManeuvers(hohmannXfer.GetManeuvers());
}
}
else
{
// assume we're in orbit around the moon
OrbitData orbitData = new OrbitData();
orbitData.SetOrbitForVelocity(spaceship, moonBody);
OrbitData toOrbit = new OrbitData(orbitData);
toOrbit.a = percentRaise * orbitData.a;
const bool rendezvous = false;
OrbitTransfer hohmannXfer = new HohmannXfer(orbitData, toOrbit, rendezvous);
ge.AddManeuvers(hohmannXfer.GetManeuvers());
}
}
public void HyperOmegaUInclNoPhase()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
GameObject planet = TestSetupUtils.CreatePlanetInHyper(star, 1f);
OrbitHyper orbitHyper = planet.GetComponent <OrbitHyper>();
orbitHyper.ecc = 1.4f;
orbitHyper.perihelion = 20f;
orbitHyper.r_initial = 20f;
orbitHyper.inclination = 35f;
// Try some values of om
float[] omegaValues = { 30f, 45f, 60f, 90f, 135f, 180f, 210f, 275f, 355f };
foreach (float omega in omegaValues)
{
orbitHyper.omega_uc = omega;
TestSetupUtils.SetupGravityEngine(star, planet);
orbitHyper.Log(System.Reflection.MethodBase.GetCurrentMethod().Name);
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("omega = " + omega + " od.omega_uc=" + od.omega_uc);
// Need a bit of leeway at 0 with error
Assert.IsTrue(FloatEqualMod360(omega, od.omega_uc, 0.05));
}
}
// Update is called once per frame
void Update()
{
if (xferRequested)
{
return;
}
if (Input.GetKeyUp(KeyCode.T))
{
OrbitData od1 = new OrbitData();
od1.SetOrbitForVelocity(orbit1, centerBody);
OrbitData od2 = new OrbitData();
od2.SetOrbitForVelocity(orbit2, centerBody);
OrbitTransfer transfer = new CircularInclinationAndAN(od1, od2);
// Update for as many markers as provided
List <Maneuver> maneuvers = transfer.GetManeuvers();
for (int i = 0; i < commonPointMarker.Length; i++)
{
commonPointMarker[i].transform.position = maneuvers[i].physPosition.ToVector3();
}
GravityEngine.instance.AddManeuvers(transfer.GetManeuvers());
xferRequested = true;
}
}
public void PhaseRetrogradeEllipse()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
const float orbitRadius = 10f;
GameObject planet = TestSetupUtils.CreatePlanetInOrbit(star, 1f, orbitRadius);
OrbitEllipse orbitEllipse = planet.GetComponent <OrbitEllipse>();
orbitEllipse.ecc = 0.4f;
orbitEllipse.inclination = 180f;
// Try some values of om
float[] phaseValues = { 30f, 45f, 60f, 90f, 135f, 180f, 0f };
foreach (float phase in phaseValues)
{
orbitEllipse.phase = phase;
orbitEllipse.Init();
orbitEllipse.ApplyScale(1f);
orbitEllipse.InitNBody(1f, 1f);
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("phase = " + phase + " od.phase=" + od.phase);
// Need a bit of leeway at 0 with error
Assert.IsTrue(FloatEqual(phase, od.phase, 0.02));
TestRV(od, planet, star, orbitRadius);
}
}
// Update is called once per frame
void Update()
{
if (Input.GetKeyUp(KeyCode.C))
{
OrbitData currentOrbit = new OrbitData();
currentOrbit.SetOrbitForVelocity(shipNbody, centerNbody);
// circularize the orbit
OrbitTransfer t = new CircularizeXfer(currentOrbit);
// If this is a ship with a Kepler sequence take the maneuvers and add them as KeplerSequence elements
// This allows the transfer to be time-reversible if the whole scene is on rails.
if (keplerSeq != null)
{
keplerSeq.AddManeuvers(t.GetManeuvers());
}
else
{
// Nbody evolution (or plain onRails w/o KeplerSequence) use maneuvers
GravityEngine.Instance().AddManeuver(t.GetManeuvers()[0]);
}
}
else if (Input.GetKeyDown(KeyCode.R))
{
// return orbit to GravityEngine control (go Off-Rails)
if (keplerSeq != null)
{
keplerSeq.AppendReturnToGE(GravityEngine.Instance().GetPhysicalTime(), shipNbody);
}
}
else if (Input.GetKeyDown(KeyCode.W))
{
// return orbit to GravityEngine control (go Off-Rails)
GravityEngine.Instance().ApplyImpulse(shipNbody, Vector3.up);
}
}
public void HyperInclOmega()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
GameObject planet = TestSetupUtils.CreatePlanetInHyper(star, 1f);
OrbitHyper orbitHyper = planet.GetComponent <OrbitHyper>();
orbitHyper.r_initial = 20f;
orbitHyper.ecc = 2.5f;
// Try some values of phase
float[] inclinationValues = { 0f, 30f, 45f, 60f, 90f, 135f, 180f };
float[] omegaUValues = { 0f, 30f, 45f, 60f, 90f, 135f, 180f, 210f, 320f };
foreach (float incl in inclinationValues)
{
foreach (float omegau in omegaUValues)
{
orbitHyper.inclination = incl;
orbitHyper.omega_uc = omegau;
orbitHyper.Init();
orbitHyper.InitNBody(1f, 1f);
orbitHyper.Log("Initial circle:");
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("incl = " + incl + " od.incl=" + od.inclination);
Debug.Log("omegaU = " + omegau + " od.omegau=" + od.omega_uc);
TestRV(od, planet, star);
}
}
}
public void HyperInclination()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
GameObject planet = TestSetupUtils.CreatePlanetInHyper(star, 1f);
OrbitHyper orbitHyper = planet.GetComponent <OrbitHyper>();
orbitHyper.ecc = 1.4f;
orbitHyper.r_initial = 20f;
// Try some values of om
float[] inclValues = { 30f, 45f, 60f, 90f, 135f, 180f, 0f };
foreach (float incl in inclValues)
{
orbitHyper.inclination = incl;
TestSetupUtils.SetupGravityEngine(star, planet);
orbitHyper.Log(System.Reflection.MethodBase.GetCurrentMethod().Name);
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("incl = " + incl + " od.incl=" + od.inclination);
// Need a bit of leeway at 0 with error
Assert.IsTrue(FloatEqual(incl, od.inclination, 0.02));
}
}
public void HyperPhaseNoIncl()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
const float orbitPeri = 15f;
GameObject planet = TestSetupUtils.CreatePlanetInHyper(star, 1f);
OrbitHyper orbitHyper = planet.GetComponent <OrbitHyper>();
orbitHyper.ecc = 1.4f;
orbitHyper.perihelion = orbitPeri;
orbitHyper.r_initial = orbitPeri;
// Try some values of om
float[] rinit_values = { orbitPeri, orbitPeri + 2f, orbitPeri + 5f, orbitPeri + 10f, orbitPeri + 20f };
foreach (float rinit in rinit_values)
{
orbitHyper.r_initial = rinit;
TestSetupUtils.SetupGravityEngine(star, planet);
orbitHyper.Log(System.Reflection.MethodBase.GetCurrentMethod().Name);
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("rinit = " + rinit + " od.r_initial=" + od.r_initial);
// Need a bit of leeway at 0 with error
TestRV(od, planet, star);
}
}
public void OmegaUCircleInclination()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
NBody starNbody = star.GetComponent <NBody>();
const float orbitRadius = 10f;
GameObject planet = TestSetupUtils.CreatePlanetInOrbitUniversal(starNbody, 1f, orbitRadius);
OrbitUniversal orbitU = planet.GetComponent <OrbitUniversal>();
orbitU.eccentricity = 0.0f;
orbitU.inclination = 5;
orbitU.SetMajorAxisInspector(orbitRadius);
// Try some values of om
float[] omegaValues = { 0f, 30f, 45f, 60f, 90f, 135f, 180f, 210f, 320f };
foreach (float omega in omegaValues)
{
orbitU.omega_uc = omega;
TestSetupUtils.SetupGravityEngine(star, planet);
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("Omega = " + omega + " od.omega_lc=" + od.omega_lc + " od:" + od.LogString());
Assert.IsTrue(GEUnit.FloatEqual(omega, od.omega_uc, 0.1));
}
}
public void OmegasEllipseInclination()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
const float orbitRadius = 10f;
GameObject planet = TestSetupUtils.CreatePlanetInOrbit(star, 1f, orbitRadius);
OrbitEllipse orbitEllipse = planet.GetComponent <OrbitEllipse>();
orbitEllipse.InitNBody(1f, 1f);
orbitEllipse.inclination = 35f;
orbitEllipse.ecc = 0.25f;
orbitEllipse.Init();
orbitEllipse.ApplyScale(1f);
orbitEllipse.InitNBody(1f, 1f);
// Try some values of om
float[] omegaValues = { 0f, 30f, 45f, 60f, 90f, 135f, 180f };
foreach (float omega in omegaValues)
{
orbitEllipse.omega_uc = omega;
orbitEllipse.Init();
orbitEllipse.InitNBody(1f, 1f);
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
TestRV(od, planet, star, orbitRadius);
}
}
public void OmegaULEllipseInclined()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
const float orbitRadius = 10f;
GameObject planet = TestSetupUtils.CreatePlanetInOrbit(star, 1f, orbitRadius);
OrbitEllipse orbitEllipse = planet.GetComponent <OrbitEllipse>();
orbitEllipse.InitNBody(1f, 1f);
orbitEllipse.inclination = 30f;
orbitEllipse.ecc = 0.2f;
orbitEllipse.Init();
orbitEllipse.ApplyScale(1f);
orbitEllipse.InitNBody(1f, 1f);
// Try some values of om
float[] omegaUValues = { 0f, 30f, 45f, 60f, 90f, 135f, 180f, 210f, 310f };
float[] omegaLValues = { 0f, 30f, 45f, 60f, 90f, 135f, 180f, 210f, 310f };
foreach (float omegaU in omegaUValues)
{
foreach (float omegaL in omegaLValues)
{
orbitEllipse.omega_uc = omegaU;
orbitEllipse.omega_lc = omegaL;
TestSetupUtils.SetupGravityEngine(star, planet);
orbitEllipse.Log("OmegaUL inclined:");
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("omegaU = " + omegaU + "omegaL = " + omegaL + " OD:=" + od.LogString());
TestRV(od, planet, star, orbitRadius);
}
}
}
// Update is called once per frame
void Update()
{
if (Input.GetKeyUp(KeyCode.H))
{
OrbitData shipOrbit = new OrbitData();
shipOrbit.SetOrbitForVelocity(shipNbody, centerNbody);
OrbitData targetOrbit = new OrbitData();
targetOrbit.SetOrbitForVelocity(targetNbody, centerNbody);
// determine the transfer
orbitTransfer = new HohmannXfer(shipOrbit, targetOrbit, rendezvous);
// If this is a ship with a Kepler sequence take the maneuvers and add them as KeplerSequence elements
// This allows the transfer to be time-reversible if the whole scene is on rails.
if (keplerSeq != null)
{
keplerSeq.AddManeuvers(orbitTransfer.GetManeuvers());
}
else
{
// Nbody evolution (or plain onRails w/o KeplerSequence) use maneuvers
foreach (Maneuver m in orbitTransfer.GetManeuvers())
{
GravityEngine.Instance().AddManeuver(m);
}
}
// Maneuver markers
if (markerPrefab != null)
{
foreach (Maneuver m in orbitTransfer.GetManeuvers())
{
// set maneuver position marker
GameObject marker = Instantiate(markerPrefab, centerNbody.gameObject.transform, true);
marker.transform.position = m.physPosition.ToVector3();
markers.Add(marker);
m.onExecuted = RemoveMarker;
}
}
}
if (Input.GetKeyUp(KeyCode.C))
{
// clear maneuvers
GravityEngine.Instance().ClearManeuvers();
// delete on rails maneuvers
if (keplerSeq != null)
{
keplerSeq.RemoveManeuvers(orbitTransfer.GetManeuvers());
}
foreach (GameObject marker in markers)
{
Destroy(marker);
}
markers.Clear();
}
// optionally report time to next maneuver
// for now just do first maneuver
if ((timeToManeuverText != null) && (orbitTransfer != null))
{
double time = orbitTransfer.GetManeuvers()[0].worldTime - GravityEngine.Instance().GetPhysicalTime();
timeToManeuverText.text = string.Format("Time to Next Maneuver = {0:0.00}", time);
}
}
public void CirclePhaseOmegaInclined()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
const float orbitRadius = 10f;
GameObject planet = TestSetupUtils.CreatePlanetInOrbit(star, 1f, orbitRadius);
OrbitEllipse orbitEllipse = planet.GetComponent <OrbitEllipse>();
orbitEllipse.inclination = 20f;
// Try some values of phase
// omegaU for a circle does not make sense, no axis to relate it to.
float[] phaseValues = { 0f, 30f, 45f, 60f, 90f, 135f, 180f, 210f, 320f };
foreach (float phase in phaseValues)
{
orbitEllipse.phase = phase;
orbitEllipse.omega_uc = 0;
TestSetupUtils.SetupGravityEngine(star, planet);
Debug.LogFormat("Test for phase={0} omegau={1}", phase, 0);
orbitEllipse.Log("Initial circle:");
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("OrbitData: " + od.LogString());
Assert.IsTrue(FloatEqualMod360(phase, od.phase, 0.05));
Assert.IsTrue(FloatEqualMod360(0, od.omega_uc, 0.05));
TestRV(od, planet, star, orbitRadius);
}
}
public void PhaseNoInclinationEllipse()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
const float orbitRadius = 20f;
GameObject planet = TestSetupUtils.CreatePlanetInOrbit(star, 1f, orbitRadius);
OrbitEllipse orbitEllipse = planet.GetComponent <OrbitEllipse>();
orbitEllipse.ecc = 0.2f;
// Try some values of om
float[] phaseValues = { 30f, 45f, 60f, 90f, 135f, 180f, 225f, 270f, 325f, 0f };
foreach (float phase in phaseValues)
{
orbitEllipse.phase = phase;
TestSetupUtils.SetupGravityEngine(star, planet);
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
orbitEllipse.Log("PhaseNoInclinationEllipse:");
Debug.Log(od.LogString());
// Need a bit of leeway at 0 with error
Assert.IsTrue(FloatEqualMod360(phase, od.phase, 0.02));
Assert.IsTrue(FloatEqualMod360(0f, od.omega_lc, 0.02));
Assert.IsTrue(FloatEqualMod360(0f, od.omega_uc, 0.02));
TestRV(od, planet, star, orbitRadius);
}
}
// Check eccentricity and inclination
public void EllipseInclination()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
const float orbitRadius = 10f;
GameObject planet = TestSetupUtils.CreatePlanetInOrbit(star, 1f, orbitRadius);
OrbitEllipse orbitEllipse = planet.GetComponent <OrbitEllipse>();
float eccentricity = 0.3f;
orbitEllipse.ecc = eccentricity;
TestSetupUtils.SetupGravityEngine(star, planet);
// take the velocity and check
OrbitData orbitData = new OrbitData();
orbitData.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Assert.IsTrue(FloatEqual(orbitRadius, orbitData.a));
Assert.IsTrue(FloatEqual(eccentricity, orbitData.ecc));
// Try some values of inclination
float[] inclinationValues = { 0f, 30f, 45f, 60f, 90f, 135f, 180f };
foreach (float inc in inclinationValues)
{
Debug.Log("====EclipseInclination==== inc=" + inc);
orbitEllipse.inclination = inc;
TestSetupUtils.SetupGravityEngine(star, planet);
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("TEST: incl = " + orbitEllipse.inclination + " ecc=" + orbitEllipse.ecc + " od:" + od.LogString());
Assert.IsTrue(FloatEqual(inc, od.inclination));
TestRV(od, planet, star, orbitRadius);
}
}
public void CirclePhaseOmegaInclined()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
const float orbitRadius = 10f;
GameObject planet = TestSetupUtils.CreatePlanetInOrbit(star, 1f, orbitRadius);
OrbitEllipse orbitEllipse = planet.GetComponent <OrbitEllipse>();
orbitEllipse.inclination = 20f;
// Try some values of phase
float[] phaseValues = { 0f, 30f, 45f, 60f, 90f, 135f, 180f, 210f, 320f };
float[] omegaUValues = { 0f, 30f, 45f, 60f, 90f, 135f, 180f, 210f, 320f };
foreach (float phase in phaseValues)
{
foreach (float omegau in omegaUValues)
{
orbitEllipse.phase = phase;
orbitEllipse.omega_uc = omegau;
orbitEllipse.Init();
orbitEllipse.ApplyScale(1f);
orbitEllipse.InitNBody(1f, 1f);
orbitEllipse.Log("Initial circle:");
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("TEST: phase = " + phase + " od.phase=" + od.phase +
" omegaU = " + omegau + " od.omegau=" + od.omega_uc);
TestRV(od, planet, star, orbitRadius);
}
}
}
/// <summary>
/// Circularize around Moon
/// - currently only onRails is implemented
/// </summary>
private void CircularizeAroundMoon()
{
// check ship is on segment where it near Moon
if (onRails)
{
KeplerSequence keplerSeq = spaceship.GetComponent <KeplerSequence>();
OrbitUniversal orbitU = keplerSeq.GetCurrentOrbit();
if (orbitU.centerNbody == moonBody)
{
// in orbit around the moon - do circularization
OrbitData orbitData = new OrbitData(orbitU);
OrbitTransfer circularizeXfer = new CircularizeXfer(orbitData);
keplerSeq.RemoveFutureSegments();
keplerSeq.AddManeuvers(circularizeXfer.GetManeuvers());
}
}
else
{
// assume we're in orbit around the moon
OrbitData orbitData = new OrbitData();
orbitData.SetOrbitForVelocity(spaceship, moonBody);
OrbitTransfer circularizeXfer = new CircularizeXfer(orbitData);
ge.AddManeuvers(circularizeXfer.GetManeuvers());
}
}
public void OmegaUNoInclination()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
const float orbitRadius = 10f;
GameObject planet = TestSetupUtils.CreatePlanetInOrbit(star, 1f, orbitRadius);
OrbitEllipse orbitEllipse = planet.GetComponent <OrbitEllipse>();
orbitEllipse.InitNBody(1f, 1f);
orbitEllipse.ecc = 0.1f;
// Try some values of om
float[] omegaValues = { 0f, 30f, 45f, 60f, 90f, 135f, 180f, 210f, 320f };
foreach (float omega in omegaValues)
{
orbitEllipse.omega_uc = omega;
orbitEllipse.Init();
orbitEllipse.ApplyScale(1f);
orbitEllipse.InitNBody(1f, 1f);
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("omega = " + omega + " od.omega_lc=" + od.omega_lc);
Assert.IsTrue(FloatEqual(omega, od.omega_lc, 0.4));
}
}
private void ComputeTransfer()
{
shipData = new OrbitData();
shipData.centralMass = starNBody;
shipData.SetOrbitForVelocity(spaceshipNBody, starNBody);
targetData = new OrbitData(targetEllipses[selectedEllipse].orbitData);
targetData.phase = targetEllipses[selectedEllipse].manueverPhase;
// compute the min energy path (this will be in the short path direction)
lambertU = new LambertUniversal(shipData, targetData, shortPath);
// apply any time of flight change
transferTime = tflightFactor * lambertU.GetTMin();
bool reverse = !shortPath;
// recompute with updated time
const bool df = false;
const int nrev = 0;
int error = lambertU.ComputeXfer(reverse, df, nrev, transferTime);
if (error != 0)
{
Debug.LogWarning("Lambert failed to find solution.");
maneuverSegment.gameObject.SetActive(false);
return;
}
Vector3 vel = lambertU.GetTransferVelocity();
maneuverOrbitPredictor.SetVelocity(vel);
maneuverSegment.SetVelocity(vel);
maneuverOrbitPredictor.gameObject.SetActive(true);
maneuverSegment.gameObject.SetActive(true);
}
private void ComputeTransfer()
{
Vector3d r_from = GravityEngine.Instance().GetPositionDoubleV3(spaceship);
Vector3d r_to = new Vector3d(targetPoint.transform.position);
OrbitData shipOrbit = new OrbitData();
shipOrbit.SetOrbitForVelocity(spaceship, centralMass);
// compute the min energy path (this will be in the short path direction)
lambertU = new LambertUniversal(shipOrbit, r_from, r_to, shortPath);
// apply any time of flight change
double t_flight = tflightFactor * lambertU.GetTMin();
bool reverse = !shortPath;
const bool df = false;
const int nrev = 0;
int error = lambertU.ComputeXfer(reverse, df, nrev, t_flight);
if (error != 0)
{
Debug.LogWarning("Lambert failed to find solution.");
maneuverSegment.gameObject.SetActive(false);
return;
}
Vector3 dv = lambertU.GetTransferVelocity() - GravityEngine.Instance().GetVelocity(spaceship);
dvText.text = string.Format("dV = {0:00.00} Time={1:00.00}", dv.magnitude, t_flight);
maneuverOrbitPredictor.SetVelocity(lambertU.GetTransferVelocity());
maneuverSegment.gameObject.SetActive(true);
maneuverSegment.SetDestination(r_to.ToVector3());
maneuverSegment.SetVelocity(lambertU.GetTransferVelocity());
}
public OrbitTransfer Circularize()
{
OrbitData shipOrbit = new OrbitData();
shipOrbit.SetOrbitForVelocity(ship, centralMass);
return(new CircularizeXfer(shipOrbit));
}
// Create an NBody and check it's mass
public void CircleA()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
const float orbitRadius = 10f;
GameObject planet = TestSetupUtils.CreatePlanetInOrbit(star, 1f, orbitRadius);
// confirm planet is in correct location
Assert.AreEqual(Vector3.Distance(planet.transform.position, new Vector3(10f, 0f, 0)), 0);
// take the velocity and check
OrbitData orbitData = new OrbitData();
orbitData.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Assert.AreEqual(orbitData.a, orbitRadius);
Assert.AreEqual(orbitData.omega_uc, 0f);
}
// Update is called once per frame
void Update()
{
if (Input.GetKey(KeyCode.A))
{
fromPhase += PHASE_PER_KEY;
}
else if (Input.GetKey(KeyCode.S))
{
fromPhase -= PHASE_PER_KEY;
}
else if (Input.GetKey(KeyCode.Q))
{
toPhase += PHASE_PER_KEY;
}
else if (Input.GetKey(KeyCode.W))
{
toPhase -= PHASE_PER_KEY;
}
fromPhase = NUtils.DegreesMod360(fromPhase);
toPhase = NUtils.DegreesMod360(toPhase);
SetMarkers();
shipOrbitData.SetOrbitForVelocity(spaceshipNBody, shipOrbit.centerNbody);
// Determine TOF
Vector3d from = new Vector3d(shipOrbitData.GetPhysicsPositionforEllipse(fromPhase));
Vector3d to = new Vector3d(shipOrbitData.GetPhysicsPositionforEllipse(toPhase));
Vector3d shipPos = GravityEngine.instance.GetPositionDoubleV3(spaceshipNBody);
double tPeri = shipOrbit.TimeOfFlight(shipPos, new Vector3d(shipOrbitData.GetPhysicsPositionforEllipse(0f)));
double tApo = shipOrbit.TimeOfFlight(shipPos, new Vector3d(shipOrbitData.GetPhysicsPositionforEllipse(180f)));
double tof = shipOrbit.TimeOfFlight(from, to);
// Scale to game time
//tApo = GravityScaler.ScaleToGameSeconds((float) tApo);
//tPeri = GravityScaler.ScaleToGameSeconds((float)tPeri);
//tof = GravityScaler.ScaleToGameSeconds((float)tof);
//tofText.text = string.Format("Time of Flight = {0:#.#}\nTime to Apoapsis = {1:#.#}\nTime to Periapsis = {2:#.#}\ntau = {3}",
// tof, tApo, tPeri, shipOrbitData.tau);
GravityScaler.Units units = GravityEngine.instance.units;
tofText.text = string.Format("Time of Flight = {0}\nTime to Apoapsis = {1}\nTime to Periapsis = {2}\ntau = {3}",
GravityScaler.GetWorldTimeFormatted(tof, units),
GravityScaler.GetWorldTimeFormatted(tApo, units),
GravityScaler.GetWorldTimeFormatted(tPeri, units),
GravityScaler.GetWorldTimeFormatted(shipOrbitData.tau, units));
}
// Check eccentricity and inclination
public void EccentricityInclTest()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
NBody starNbody = star.GetComponent <NBody>();
const float orbitRadius = 10f;
GameObject planet = TestSetupUtils.CreatePlanetInOrbitUniversal(starNbody, 1f, orbitRadius);
OrbitUniversal orbitU = planet.GetComponent <OrbitUniversal>();
float eccentricity = 0.3f;
// MUST reset the scale after ecc is changed, since -> p
orbitU.eccentricity = eccentricity;
orbitU.SetMajorAxisInspector(orbitRadius);
TestSetupUtils.SetupGravityEngine(star, planet);
// Try some values of inclination and ecc
float[] eccValues = { 0f, .1f, .2f, 0.5f, 0.9f };
float[] inclinationValues = { 0f, 30f, 45f, 60f, 90f, 135f, 180f };
foreach (float inc in inclinationValues)
{
foreach (float ecc in eccValues)
{
Debug.Log("====EccentricityInclTest==== ecc=" + ecc + " incl = " + inc);
orbitU.inclination = inc;
orbitU.eccentricity = ecc;
orbitU.SetMajorAxisInspector(orbitRadius); // can only use for ellipses
TestSetupUtils.SetupGravityEngine(star, planet);
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), starNbody);
Debug.Log("TEST: incl = " + orbitU.inclination + " ecc=" + orbitU.eccentricity + " od:" + od.LogString());
Debug.LogFormat("Check ecc: {0} vs {1}", ecc, od.ecc);
Assert.IsTrue(GEUnit.FloatEqual(ecc, od.ecc, 1E-3));
float axis = (float)orbitU.GetMajorAxisInspector();
Debug.LogFormat("Check axis: {0} vs {1}", axis, od.a);
Assert.IsTrue(GEUnit.FloatEqual(axis, od.a, 1E-3));
Debug.LogFormat("Check incl: {0} vs {1}", inc, od.inclination);
Assert.IsTrue(GEUnit.FloatEqual(inc, od.inclination, 1E-3));
// TestRV(od, planet, starNbody, orbitRadius);
}
}
}
public void HyperBasic()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
GameObject planet = TestSetupUtils.CreatePlanetInHyper(star, 1f);
OrbitHyper orbitHyper = planet.GetComponent <OrbitHyper>();
// Try some values of om
float[] eccValues = { 1.1f, 1.3f, 2f, 2.2f, 3f, 10f };
foreach (float ecc in eccValues)
{
orbitHyper.ecc = ecc;
orbitHyper.Init();
orbitHyper.InitNBody(1f, 1f);
orbitHyper.Log(System.Reflection.MethodBase.GetCurrentMethod().Name);
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("ecc = " + ecc + " od.ecc=" + od.ecc);
// Need a bit of leeway at 0 with error
Assert.IsTrue(FloatEqual(ecc, od.ecc, 0.02));
}
}
public void HyperInclOmega()
{
const float mass = 1000f;
GameObject star = TestSetupUtils.CreateNBody(mass, new Vector3(0, 0, 0));
GameObject planet = TestSetupUtils.CreatePlanetInHyper(star, 1f);
OrbitHyper orbitHyper = planet.GetComponent <OrbitHyper>();
orbitHyper.r_initial = 20f;
orbitHyper.ecc = 2.5f;
// Try some values of phase (incl=0 covered by another test)
float[] inclinationValues = { 30f, 45f, 60f, 90f, 135f, 180f };
float[] omegaUValues = { 0f, 30f, 45f, 60f, 90f, 135f, 180f, 210f, 320f };
foreach (float incl in inclinationValues)
{
foreach (float omegau in omegaUValues)
{
orbitHyper.inclination = incl;
orbitHyper.omega_uc = omegau;
TestSetupUtils.SetupGravityEngine(star, planet);
Debug.LogFormat("Test for i={0} omegaU={1}", incl, omegau);
orbitHyper.Log("Initial circle:");
OrbitData od = new OrbitData();
od.SetOrbitForVelocity(planet.GetComponent <NBody>(), star.GetComponent <NBody>());
Debug.Log("OrbitData: " + od.LogString());
TestRV(od, planet, star);
Debug.Log("incl = " + incl + " od.incl=" + od.inclination);
Debug.Log("omegaU = " + omegau + " od.omegau=" + od.omega_uc + " od.omega_lc=" + od.omega_lc);
if (incl != 180f)
{
// 180 comes back as omegaL = omegaU = 180, but TestRV is ok
Assert.IsTrue(FloatEqual(incl, od.inclination, 0.02));
Assert.IsTrue(FloatEqualMod360(omegau, od.omega_uc, 0.02));
}
}
}
}
// Update is called once per frame
void Update()
{
if (initOk)
{
// velocities not normally updated in NBody (to reduce CPU). Need to ask
// object to update its velocity from Gravity Engine if engine is running
if (GravityEngine.instance.GetEvolve())
{
nbody.UpdateVelocity();
}
orbitData.SetOrbitForVelocity(nbody, aroundNBody);
// Is the resulting orbit and ellipse or hyperbola?
if (orbitData.ecc < 1f)
{
ellipseBase.InitFromOrbitData(orbitData);
lineR.SetPositions(ellipseBase.OrbitPositions(numPoints));
}
else
{
orbitHyper.InitFromOrbitData(orbitData);
lineR.SetPositions(orbitHyper.OrbitPositions(numPoints));
}
}
}
//============================================================================================
// Console commands: If there is a GEConsole in the scene, these commands will be available
//============================================================================================
// In-class console method
// Quick and Dirty implementation for testing LambertUniversal code.
private string LambertUniversal(float time)
{
OrbitData shipData = new OrbitData();
shipData.SetOrbitForVelocity(spaceshipNBody, starNBody);
OrbitData targetData = targetEllipses[selectedEllipse].orbitData;
targetData.phase = targetEllipses[selectedEllipse].manueverPhase;
// get time and try universal
LambertUniversal lu = new LambertUniversal(shipData, targetData, true);
const bool reverse = false;
const bool df = false;
const int nrev = 0;
int error = lu.ComputeXfer(reverse, df, nrev, time);
if (error != 0)
{
return(string.Format("Error: LambertUniversal rc=" + error));
}
spaceshipNBody.vel_phys = lu.GetTransferVelocity();
return(string.Format("time={0} univ={1}", time, lu.GetTransferVelocity()));
}
/// <summary>
/// Computes the transfer with the moon on the +X axis without accounting for the moon motion during
/// transit. (That is accounted for in the ExecuteTransfer routine).
///
/// This allows a co-rotating visualization of the orbit.
/// </summary>
/// <returns></returns>
private Vector3 ComputeTransfer()
{
OrbitData shipOrbit = new OrbitData();
shipOrbit.SetOrbitForVelocity(spaceship, planet);
// compute the min energy path (this will be in the short path direction)
lambertU = new LambertUniversal(shipOrbit, startPoint, targetPoint, shortPath);
// apply any time of flight change
double t_flight = tflightFactor * lambertU.GetTMin();
bool reverse = !shortPath;
const bool df = false;
const int nrev = 0;
int error = lambertU.ComputeXfer(reverse, df, nrev, t_flight);
if (error != 0)
{
Debug.LogWarning("Lambert failed to find solution.");
aroundMoonSegment.gameObject.SetActive(false);
return(Vector3.zero);
}
// Check Lambert is going in the correct direction
Vector3 shipOrbitAxis = Vector3.Cross(ge.GetVelocity(spaceship), ge.GetPhysicsPosition(spaceship)).normalized;
Vector3 tliOrbitAxis = Vector3.Cross(lambertU.GetTransferVelocity(), startPoint.ToVector3());
if (Vector3.Dot(shipOrbitAxis, tliOrbitAxis) < 0)
{
error = lambertU.ComputeXfer(!reverse, df, nrev, t_flight);
if (error != 0)
{
Debug.LogWarning("Lambert failed to find solution for reverse path. error=" + error);
return(Vector3.zero);
}
}
Vector3 tliVelocity = lambertU.GetTransferVelocity();
toMoonOrbit.SetVelocity(tliVelocity);
toMoonSegment.SetVelocity(tliVelocity);
aroundMoonSegment.gameObject.SetActive(true);
// Set velocity for orbit around moon
Vector3 soiEnterVel = lambertU.GetFinalVelocity();
aroundMoonSegment.SetVelocity(soiEnterVel);
// update shipEnterSOI object
ge.UpdatePositionAndVelocity(shipEnterSOI, targetPoint.ToVector3(), soiEnterVel);
// Find the orbit around the moon. By using the mirror position we're assuming it's
// a hyperbola (since there is no course correction at SOI this is true).
// (Moon is in correct position for these calcs so can use world positions, relativePos=false)
Vector3d soiEnterV = new Vector3d(lambertU.GetFinalVelocity());
OrbitUtils.OrbitElements oe = OrbitUtils.RVtoCOE(targetPoint, soiEnterV, moonBody, false);
Vector3d soiExitR = new Vector3d();
Vector3d soiExitV = new Vector3d();
OrbitUtils.COEtoRVMirror(oe, moonBody, ref soiExitR, ref soiExitV, false);
// Set position and vel for exit ship, so exit orbit predictor can run. Moon offset/vel already added.
ge.SetPositionDoubleV3(shipExitSOI, soiExitR);
ge.SetVelocityDoubleV3(shipExitSOI, soiExitV);
aroundMoonSegment.UpdateOrbit();
return(tliVelocity);
}
