void DrawGUIPrediction()
{
ReentrySimulation.Result result = predictor.GetResult();
if (result != null)
{
switch (result.outcome)
{
case ReentrySimulation.Outcome.LANDED:
GUILayout.Label("Landing Predictions:");
GUILayout.Label(Coordinates.ToStringDMS(result.endPosition.latitude, result.endPosition.longitude) + "\nASL:" + MuUtils.ToSI(result.endASL, -1, 4) + "m");
GUILayout.Label(ScienceUtil.GetExperimentBiome(result.body, result.endPosition.latitude, result.endPosition.longitude));
double error = Vector3d.Distance(mainBody.GetRelSurfacePosition(result.endPosition.latitude, result.endPosition.longitude, 0),
mainBody.GetRelSurfacePosition(core.target.targetLatitude, core.target.targetLongitude, 0));
GUILayout.Label("Target difference = " + MuUtils.ToSI(error, 0) + "m"
+ "\nMax drag: " + result.maxDragGees.ToString("F1") + "g"
+ "\nDelta-v needed: " + result.deltaVExpended.ToString("F1") + "m/s"
+ "\nTime to land: " + GuiUtils.TimeToDHMS(result.endUT - Planetarium.GetUniversalTime(), 1));
break;
case ReentrySimulation.Outcome.AEROBRAKED:
GUILayout.Label("Predicted orbit after aerobraking:");
Orbit o = result.EndOrbit();
if (o.eccentricity > 1)
{
GUILayout.Label("Hyperbolic, eccentricity = " + o.eccentricity.ToString("F2"));
}
else
{
GUILayout.Label(MuUtils.ToSI(o.PeA, 3) + "m x " + MuUtils.ToSI(o.ApA, 3) + "m");
}
GUILayout.Label("Max drag: " + result.maxDragGees.ToString("F1") + "g"
+ "\nExit atmosphere in: " + GuiUtils.TimeToDHMS(result.endUT - Planetarium.GetUniversalTime(), 1));
break;
case ReentrySimulation.Outcome.NO_REENTRY:
GUILayout.Label("Orbit does not reenter:\n"
+ MuUtils.ToSI(orbit.PeA, 3) + "m Pe > " + MuUtils.ToSI(mainBody.RealMaxAtmosphereAltitude(), 3) + "m atmosphere height");
break;
case ReentrySimulation.Outcome.TIMED_OUT:
GUILayout.Label("Reentry simulation timed out.");
break;
}
}
}
void DrawGUIPrediction()
{
ReentrySimulation.Result result = predictor.GetResult();
if (result != null)
{
switch (result.outcome)
{
case ReentrySimulation.Outcome.LANDED:
GUILayout.Label("Predicted landing site:");
GUILayout.Label(Coordinates.ToStringDMS(result.endPosition.latitude, result.endPosition.longitude));
double error = Vector3d.Distance(mainBody.GetRelSurfacePosition(result.endPosition.latitude, result.endPosition.longitude, 0),
mainBody.GetRelSurfacePosition(core.target.targetLatitude, core.target.targetLongitude, 0));
GUILayout.Label("Difference from target = " + MuUtils.ToSI(error, 0) + "m");
if (result.maxDragGees > 0)
{
GUILayout.Label("Predicted max drag gees: " + result.maxDragGees.ToString("F1"));
}
break;
case ReentrySimulation.Outcome.AEROBRAKED:
GUILayout.Label("Predicted orbit after aerobraking:");
Orbit o = result.EndOrbit();
if (o.eccentricity > 1)
{
GUILayout.Label("Hyperbolic, eccentricity = " + o.eccentricity.ToString("F2"));
}
else
{
GUILayout.Label(MuUtils.ToSI(o.PeA, 3) + "m x " + MuUtils.ToSI(o.ApA, 3) + "m");
}
break;
case ReentrySimulation.Outcome.NO_REENTRY:
GUILayout.Label("Orbit does not reenter:");
GUILayout.Label(MuUtils.ToSI(orbit.PeA, 3) + "m Pe > " + MuUtils.ToSI(mainBody.RealMaxAtmosphereAltitude(), 3) + "m atmosphere height");
break;
case ReentrySimulation.Outcome.TIMED_OUT:
GUILayout.Label("Reentry simulation timed out.");
break;
}
}
}
