public Orbit(double semiMajorAxis, double eccentricity, double argumentOfPeriapsis, double gravParameter, double meanAnomaly, bool prograde)
{
_semiMajorAxis = semiMajorAxis;
_eccentricity = eccentricity;
_argumentOfPeriapsis = argumentOfPeriapsis;
this.gravParameter = gravParameter;
_prograde = prograde;
this.meanAnomaly = meanAnomaly;
_trueAnomaly = OrbitMath.ConvertMeanToTrueElliptic(this.meanAnomaly, _eccentricity);
meanMotion = System.Math.Sqrt(gravParameter / System.Math.Pow(_semiMajorAxis, 3));
_periapsis = _semiMajorAxis * (1 - _eccentricity);
_apoapsis = _semiMajorAxis * (1 + _eccentricity);
_radius = OrbitMath.CalculateRadius(_semiMajorAxis, _eccentricity, _trueAnomaly);
flightPathAngle = OrbitMath.CalculateFlightpathAngle(_eccentricity, _trueAnomaly);
_velocity = OrbitMath.CalculateVelocity(this.gravParameter, _radius, _semiMajorAxis);
}
public DVector2[] GetSubsets(int count, bool includeFirst = true)
{
DVector2[] subsets = new DVector2[count];
double step = 2 * Math.PI / ((double)count - (includeFirst?1:0));
for (int i = 0; i < count - (includeFirst ? 1 : 0); i++)
{
DVector2 pos = new DVector2(OrbitMath.CalculateRadius(_semiMajorAxis, _eccentricity, step * (double)i), 0).Rotate(OrbitMath.ReduceAngle(_argumentOfPeriapsis + step * (double)i));
subsets[i] = pos;
}
if (includeFirst)
{
subsets[--count] = subsets[0];
}
return(subsets);
}
