public void CreateOrbit()
{
if (orbitData.randomized || WarpDrivers.WarpDrive.seedString == AstroUtils.KERBIN_SYSTEM_COORDS)
{
// Already randomized data
return;
}
orbitData = new OrbitData();
orbitData.randomized = true;
if (IsSun())
{
// Special case
orbitData.referenceBody = solarSystem.sun;
orbitData.semiMajorAxis = 0;
return;
}
#region Reference Body
CreateReferenceBody();
#endregion
#region Gravity
CreateGravity();
#endregion
#region Sphere of Influence
CreateSphereOfInfluence();
#endregion
#region Semi-Major Axis
double semiMajorAxis = AstroUtils.MAX_SEMI_MAJOR_AXIS;
if (referenceBodyData.IsSun())
{
semiMajorAxis = CreatePlanet();
}
else
{
// Planet is moon
semiMajorAxis = CreateMoon();
}
// Remove eccentricity from the semi-major axis
if (orbitData.eccentricity != 1.0f)
{
semiMajorAxis /= (1.0 - orbitData.eccentricity);
}
orbitData.semiMajorAxis = semiMajorAxis;
#endregion
#region Inclination
// New way uses normal distribution
double normalRNG = WarpRNG.GenerateNormalRandom();
double normalInc = normalRNG * 5.0;
orbitData.inclination = normalInc;
#endregion
#region Eccentricity
// Eccentricity must be a value between 0 and 0.99
// We prefer low values
normalRNG = WarpRNG.GenerateNormalRandom();
// We want to try to clamp the range somewhere between 0 and 0.1, since that produces results most similar to KSP
double eccentRNG = normalRNG * 0.01666667;
eccentRNG += 0.05;
if (eccentRNG < 0)
{
eccentRNG *= -1.0;
}
double eccentricity = eccentRNG;
orbitData.eccentricity = eccentricity;
#endregion
#region Longitude Ascending Node
int lan = WarpRNG.GenerateInt(0, 360);
orbitData.longitudeAscendingNode = lan;
#endregion
#region Argument Of Periapsis
int argumentOfPeriapsis = WarpRNG.GenerateInt(0, 360);
orbitData.argumentOfPeriapsis = argumentOfPeriapsis;
#endregion
#region Mean Anomaly at Epoch
float meanAnomalyAtEpoch = WarpRNG.GenerateFloat(0.0f, Mathf.PI * 2.0f);
if (orbitData.semiMajorAxis < 0)
{
meanAnomalyAtEpoch /= Mathf.PI;
meanAnomalyAtEpoch -= 1.0f;
meanAnomalyAtEpoch *= 5.0f;
}
orbitData.meanAnomalyAtEpoch = meanAnomalyAtEpoch;
#endregion
#region Period
double referenceMass = AstroUtils.MassInSolarMasses(referenceBody.Mass);
double usMass = AstroUtils.MassInSolarMasses(planet.Mass);
orbitData.period = AstroUtils.CalculatePeriodFromSemiMajorAxis(semiMajorAxis, referenceMass, usMass);
#endregion
}