/// <summary>
/// Gets the UT for the equatorial AN.
/// </summary>
/// <returns>The equatorial AN UT.</returns>
/// <param name="o">The Orbit to calculate the UT from.</param>
internal static double getEquatorialANUT(this Orbit o)
{
//TODO: Add safeguards for bad UTs, may need to be refactored to NodeManager
return(o.GetUTforTrueAnomaly(o.GetTrueAnomalyOfZupVector(o.GetANVector()), 2));
}
/// <summary>
///
/// </summary>
/// <param name="o">O.</param>
private static void Print_Orbit_info(Orbit o)
{
if (o == null) {
Debug.Log("Orbit is null");
return;
}
string Output = "";
Output += "Orbit Info \n";
Output += "\n activePatch:" + o.activePatch ;
Output += "\n altitude:"+ o.altitude ;
//Output += "\n an:"+ o.an ;
//Output += "\n ApA:"+ o.ApA ;
//Output += "\n ApR:"+ o.ApR ;
Output += "\n argumentOfPeriapsis:"+ o.argumentOfPeriapsis ;
//Output += "\n ClAppr:"+ o.ClAppr ;
//Output += "\n ClEctr1:"+ o.ClEctr1 ;
//Output += "\n ClEctr2:"+ o.ClEctr2 ;
Output += "\n closestEncounterBody:"+ o.closestEncounterBody ;
Output += "\n closestEncounterLevel:"+ o.closestEncounterLevel ;
Output += "\n closestEncounterPatch:"+ o.closestEncounterPatch ;
Output += "\n closestTgtApprUT:"+ o.closestTgtApprUT ;
//Output += "\n CrAppr:"+ o.CrAppr ;
//Output += "\n debugAN:"+ o.debugAN ;
//Output += "\n debugEccVec:"+ o.debugEccVec ;
//Output += "\n debugH:"+ o.debugH ;
//Output += "\n debugPos:"+ o.debugPos ;
//Output += "\n debugVel:"+ o.debugVel ;
//Output += "\n debug_returnFullEllipseTrajectory:"+ o.debug_returnFullEllipseTrajectory ;
//Output += "\n E:"+ o.E ;
//Output += "\n eccentricAnomaly:"+ o.eccentricAnomaly ;
//Output += "\n eccentricity:"+ o.eccentricity ;
//Output += "\n eccVec:"+ o.eccVec ;
//Output += "\n EndUT:"+ o.EndUT ;
Output += "\n epoch:"+ o.epoch ;
//Output += "\n FEVp:"+ o.FEVp;
//Output += "\n FEVs:"+ o.FEVs ;
//Output += "\n fromE:"+ o.fromE ;
//Output += "\n fromV:"+ o.fromV ;
//Output += "\n h:"+ o.h ;
//Output += "\n inclination:"+ o.inclination ;
//Output += "\n LAN:"+ o.LAN ;
//Output += "\n mag:"+ o.mag ;
//Output += "\n meanAnomaly:"+ o.meanAnomaly ;
//Output += "\n meanAnomalyAtEpoch:"+ o.meanAnomalyAtEpoch ;
Output += "\n nearestTT:"+ o.nearestTT ;
Output += "\n nextPatch:"+ o.nextPatch ;
Output += "\n nextTT:"+ o.nextTT ;
//Output += "\n ObT:"+ o.ObT ;
Output += "\n ObTAtEpoch :"+ o.ObTAtEpoch ;
//Output += "\n orbitalEnergy :"+ o.orbitalEnergy ;
//Output += "\n orbitalSpeed:"+ o.orbitalSpeed ;
//Output += "\n orbitPercent :"+ o.orbitPercent ;
Output += "\n patchEndTransition :"+ o.patchEndTransition ;
Output += "\n patchStartTransition :"+ o.patchStartTransition ;
//Output += "\n period :"+ o.period ;
//Output += "\n pos :"+ o.pos ;
Output += "\n previousPatch :"+ o.previousPatch ;
//Output += "\n radius :"+ o.radius ;
Output += "\n referenceBody :"+ o.referenceBody ;
//Output += "\n sampleInterval :"+ o.sampleInterval ;
Output += "\n secondaryPosAtTransition1 :"+ o.secondaryPosAtTransition1 ;
Output += "\n secondaryPosAtTransition2 :"+ o.secondaryPosAtTransition2 ;
//Output += "\n semiLatusRectum :"+ o.semiLatusRectum ;
//Output += "\n semiMajorAxis :"+ o.semiMajorAxis ;
//Output += "\n semiMinorAxis :"+ o.semiMinorAxis ;
//Output += "\n SEVp :"+ o.SEVp ;
//Output += "\n SEVs :"+ o.SEVs ;
//Output += "\n StartUT :"+ o.StartUT ;
Output += "\n timeToAp :"+ o.timeToAp ;
Output += "\n timeToPe :"+ o.timeToPe ;
Output += "\n timeToTransition1 :"+ o.timeToTransition1 ;
Output += "\n timeToTransition2 :"+ o.timeToTransition2 ;
//Output += "\n toE :"+ o.toE ;
//Output += "\n toV :"+ o.toV ;
//Output += "\n trueAnomaly :"+ o.trueAnomaly ;
//Output += "\n UTappr :"+ o.UTappr ;
//Output += "\n UTsoi :"+ o.UTsoi ;
//Output += "\n V :"+ o.V ;
//Output += "\n vel :"+ o.vel ;
Debug.Log(Output);
if (!o.activePatch) {
return;
}
try{
//Functions
Output = "Orbit Functions: \n";
Output += "\n PeA :"+ o.PeA ;
Output += "\n PeR :"+ o.PeR ;
Output += "\n GetANVector:"+ o.GetANVector() ;
Output += "\n GetEccVector:"+ o.GetEccVector() ;
Output += "\n GetFrameVel:"+ o.GetFrameVel() ;
Output += "\n GetHashCode:"+ o.GetHashCode() ;
Output += "\n GetOrbitNormal:"+ o.GetOrbitNormal() ;
Output += "\n GetRelativeVel:"+ o.GetRelativeVel() ;
Output += "\n GetType:"+ o.GetType() ;
Output += "\n GetVel:"+ o.GetVel() ;
Output += "\n GetWorldSpaceVel:"+ o.GetWorldSpaceVel() ;
//Unused Funtion (Tests?)
// Output += "\n :"+ o.DrawOrbit;
// Output += "\n :"+ o.Equals ;
// Output += "\n :"+ o.GetDTforTrueAnomaly() ;
// Output += "\n :"+ o.GetEccentricAnomaly ;
// Output += "\n :"+ o.GetFrameVelAtUT ;
// Output += "\n :"+ o.GetMeanAnomaly ;
// Output += "\n :"+ o.getObTAtMeanAnomaly ;
// Output += "\n :"+ o.getObtAtUT ;
// Output += "\n :"+ o.getOrbitalSpeedAt ;
// Output += "\n :"+ o.getOrbitalSpeedAtDistance ;
// Output += "\n :"+ o.getOrbitalSpeedAtPos ;
// Output += "\n :"+ o.getOrbitalSpeedAtRelativePos ;
// Output += "\n :"+ o.getOrbitalVelocityAtObT ;
// Output += "\n :"+ o.getOrbitalVelocityAtUT ;
// Output += "\n :"+ o.GetPatchTrajectory ;
// Output += "\n :"+ o.getPositionAtT ;
// Output += "\n :"+ o.getPositionAtUT ;
// Output += "\n :"+ o.getPositionFromEccAnomaly ;
// Output += "\n :"+ o.getPositionFromMeanAnomaly ;
// Output += "\n :"+ o.getPositionFromTrueAnomaly ;
// Output += "\n :"+ o.getRelativePositionAtT ;
// Output += "\n :"+ o.getRelativePositionAtUT ;
// Output += "\n :"+ o.getRelativePositionFromEccAnomaly ;
// Output += "\n :"+ o.getRelativePositionFromMeanAnomaly ;
// Output += "\n :"+ o.getRelativePositionFromTrueAnomaly ;
// Output += "\n :"+ o.GetRotFrameVel ;
// Output += "\n :"+ o.getTrueAnomaly ;
// Output += "\n :"+ o.GetTrueAnomalyOfZupVector ;
// Output += "\n :"+ o.getTruePositionAtUT ;
// Output += "\n :"+ o.GetUTforTrueAnomaly ;
// Output += "\n :"+ o.Init() ;
// Output += "\n :"+ o.RadiusAtTrueAnomaly ;
// Output += "\n :"+ o.solveEccentricAnomaly ;
// Output += "\n :"+ o.TrueAnomalyAtRadius ;
// Output += "\n :"+ o.TrueAnomalyAtT ;
// Output += "\n :"+ o.TrueAnomalyAtUT;
// Output += "\n :"+ o.UpdateFromOrbitAtUT;
// Output += "\n :"+ o.UpdateFromStateVectors;
// Output += "\n :"+ o.UpdateFromUT;
}
catch(Exception ex) {
Debug.Log("Could not orbit functions. Exception:" + ex);
//no catch exception for now.
}
Debug.Log(Output);
Debug.Log("Patch from o.nextPatch");
Print_Orbit_info (o.nextPatch);
Debug.Log("Patch from o.closestEncounterPatch");
Print_Orbit_info (o.closestEncounterPatch);
Output = "";
}
/// <summary>
///
/// </summary>
/// <param name="o">O.</param>
private static void Print_Orbit_info(Orbit o)
{
if (o == null)
{
Debug.Log("Orbit is null");
return;
}
string Output = "";
Output += "Orbit Info \n";
Output += "\n activePatch:" + o.activePatch;
Output += "\n altitude:" + o.altitude;
//Output += "\n an:"+ o.an ;
//Output += "\n ApA:"+ o.ApA ;
//Output += "\n ApR:"+ o.ApR ;
Output += "\n argumentOfPeriapsis:" + o.argumentOfPeriapsis;
//Output += "\n ClAppr:"+ o.ClAppr ;
//Output += "\n ClEctr1:"+ o.ClEctr1 ;
//Output += "\n ClEctr2:"+ o.ClEctr2 ;
Output += "\n closestEncounterBody:" + o.closestEncounterBody;
Output += "\n closestEncounterLevel:" + o.closestEncounterLevel;
Output += "\n closestEncounterPatch:" + o.closestEncounterPatch;
Output += "\n closestTgtApprUT:" + o.closestTgtApprUT;
//Output += "\n CrAppr:"+ o.CrAppr ;
//Output += "\n debugAN:"+ o.debugAN ;
//Output += "\n debugEccVec:"+ o.debugEccVec ;
//Output += "\n debugH:"+ o.debugH ;
//Output += "\n debugPos:"+ o.debugPos ;
//Output += "\n debugVel:"+ o.debugVel ;
//Output += "\n debug_returnFullEllipseTrajectory:"+ o.debug_returnFullEllipseTrajectory ;
//Output += "\n E:"+ o.E ;
//Output += "\n eccentricAnomaly:"+ o.eccentricAnomaly ;
//Output += "\n eccentricity:"+ o.eccentricity ;
//Output += "\n eccVec:"+ o.eccVec ;
//Output += "\n EndUT:"+ o.EndUT ;
Output += "\n epoch:" + o.epoch;
//Output += "\n FEVp:"+ o.FEVp;
//Output += "\n FEVs:"+ o.FEVs ;
//Output += "\n fromE:"+ o.fromE ;
//Output += "\n fromV:"+ o.fromV ;
//Output += "\n h:"+ o.h ;
//Output += "\n inclination:"+ o.inclination ;
//Output += "\n LAN:"+ o.LAN ;
//Output += "\n mag:"+ o.mag ;
//Output += "\n meanAnomaly:"+ o.meanAnomaly ;
//Output += "\n meanAnomalyAtEpoch:"+ o.meanAnomalyAtEpoch ;
Output += "\n nearestTT:" + o.nearestTT;
Output += "\n nextPatch:" + o.nextPatch;
Output += "\n nextTT:" + o.nextTT;
//Output += "\n ObT:"+ o.ObT ;
Output += "\n ObTAtEpoch :" + o.ObTAtEpoch;
//Output += "\n orbitalEnergy :"+ o.orbitalEnergy ;
//Output += "\n orbitalSpeed:"+ o.orbitalSpeed ;
//Output += "\n orbitPercent :"+ o.orbitPercent ;
Output += "\n patchEndTransition :" + o.patchEndTransition;
Output += "\n patchStartTransition :" + o.patchStartTransition;
//Output += "\n period :"+ o.period ;
//Output += "\n pos :"+ o.pos ;
Output += "\n previousPatch :" + o.previousPatch;
//Output += "\n radius :"+ o.radius ;
Output += "\n referenceBody :" + o.referenceBody;
//Output += "\n sampleInterval :"+ o.sampleInterval ;
Output += "\n secondaryPosAtTransition1 :" + o.secondaryPosAtTransition1;
Output += "\n secondaryPosAtTransition2 :" + o.secondaryPosAtTransition2;
//Output += "\n semiLatusRectum :"+ o.semiLatusRectum ;
//Output += "\n semiMajorAxis :"+ o.semiMajorAxis ;
//Output += "\n semiMinorAxis :"+ o.semiMinorAxis ;
//Output += "\n SEVp :"+ o.SEVp ;
//Output += "\n SEVs :"+ o.SEVs ;
//Output += "\n StartUT :"+ o.StartUT ;
Output += "\n timeToAp :" + o.timeToAp;
Output += "\n timeToPe :" + o.timeToPe;
Output += "\n timeToTransition1 :" + o.timeToTransition1;
Output += "\n timeToTransition2 :" + o.timeToTransition2;
//Output += "\n toE :"+ o.toE ;
//Output += "\n toV :"+ o.toV ;
//Output += "\n trueAnomaly :"+ o.trueAnomaly ;
//Output += "\n UTappr :"+ o.UTappr ;
//Output += "\n UTsoi :"+ o.UTsoi ;
//Output += "\n V :"+ o.V ;
//Output += "\n vel :"+ o.vel ;
Debug.Log(Output);
if (!o.activePatch)
{
return;
}
try{
//Functions
Output = "Orbit Functions: \n";
Output += "\n PeA :" + o.PeA;
Output += "\n PeR :" + o.PeR;
Output += "\n GetANVector:" + o.GetANVector();
Output += "\n GetEccVector:" + o.GetEccVector();
Output += "\n GetFrameVel:" + o.GetFrameVel();
Output += "\n GetHashCode:" + o.GetHashCode();
Output += "\n GetOrbitNormal:" + o.GetOrbitNormal();
Output += "\n GetRelativeVel:" + o.GetRelativeVel();
Output += "\n GetType:" + o.GetType();
Output += "\n GetVel:" + o.GetVel();
Output += "\n GetWorldSpaceVel:" + o.GetWorldSpaceVel();
//Unused Funtion (Tests?)
// Output += "\n :"+ o.DrawOrbit;
// Output += "\n :"+ o.Equals ;
// Output += "\n :"+ o.GetDTforTrueAnomaly() ;
// Output += "\n :"+ o.GetEccentricAnomaly ;
// Output += "\n :"+ o.GetFrameVelAtUT ;
// Output += "\n :"+ o.GetMeanAnomaly ;
// Output += "\n :"+ o.getObTAtMeanAnomaly ;
// Output += "\n :"+ o.getObtAtUT ;
// Output += "\n :"+ o.getOrbitalSpeedAt ;
// Output += "\n :"+ o.getOrbitalSpeedAtDistance ;
// Output += "\n :"+ o.getOrbitalSpeedAtPos ;
// Output += "\n :"+ o.getOrbitalSpeedAtRelativePos ;
// Output += "\n :"+ o.getOrbitalVelocityAtObT ;
// Output += "\n :"+ o.getOrbitalVelocityAtUT ;
// Output += "\n :"+ o.GetPatchTrajectory ;
// Output += "\n :"+ o.getPositionAtT ;
// Output += "\n :"+ o.getPositionAtUT ;
// Output += "\n :"+ o.getPositionFromEccAnomaly ;
// Output += "\n :"+ o.getPositionFromMeanAnomaly ;
// Output += "\n :"+ o.getPositionFromTrueAnomaly ;
// Output += "\n :"+ o.getRelativePositionAtT ;
// Output += "\n :"+ o.getRelativePositionAtUT ;
// Output += "\n :"+ o.getRelativePositionFromEccAnomaly ;
// Output += "\n :"+ o.getRelativePositionFromMeanAnomaly ;
// Output += "\n :"+ o.getRelativePositionFromTrueAnomaly ;
// Output += "\n :"+ o.GetRotFrameVel ;
// Output += "\n :"+ o.getTrueAnomaly ;
// Output += "\n :"+ o.GetTrueAnomalyOfZupVector ;
// Output += "\n :"+ o.getTruePositionAtUT ;
// Output += "\n :"+ o.GetUTforTrueAnomaly ;
// Output += "\n :"+ o.Init() ;
// Output += "\n :"+ o.RadiusAtTrueAnomaly ;
// Output += "\n :"+ o.solveEccentricAnomaly ;
// Output += "\n :"+ o.TrueAnomalyAtRadius ;
// Output += "\n :"+ o.TrueAnomalyAtT ;
// Output += "\n :"+ o.TrueAnomalyAtUT;
// Output += "\n :"+ o.UpdateFromOrbitAtUT;
// Output += "\n :"+ o.UpdateFromStateVectors;
// Output += "\n :"+ o.UpdateFromUT;
}
catch (Exception ex) {
Debug.Log("Could not orbit functions. Exception:" + ex);
//no catch exception for now.
}
Debug.Log(Output);
Debug.Log("Patch from o.nextPatch");
Print_Orbit_info(o.nextPatch);
Debug.Log("Patch from o.closestEncounterPatch");
Print_Orbit_info(o.closestEncounterPatch);
Output = "";
}
/// <summary>
/// Gets the UT for the equatorial AN.
/// </summary>
/// <returns>The equatorial AN UT.</returns>
/// <param name="o">The Orbit to calculate the UT from.</param>
public static double getEquatorialANUT(Orbit o)
{
//TODO: Add safeguards for bad UTs, may need to be refactored to NodeManager
return o.GetUTforTrueAnomaly(o.GetTrueAnomalyOfZupVector(o.GetANVector()), 2);
}
