shmodot/scripts/orbits/IOrbitalElementsExtensions.cs

13 lines
447 B
C#

using Vim.Math3d;
using static System.Math;
public static class IOrbitalElementsExtensions
{
/// <summary>
/// Get the Cartesian position on the orbit for a given mean anomaly.
/// </summary>
/// <param name="M">Mean anomaly</param>
/// <returns>Position</returns>
public static DVector2 GetEccentricPosition2D(this OrbitalElements elements, double M) =>
Kepler.GetEccentricPosition2D(elements.e, elements.a, M);
}