http://arxiv.org/abs/2108.03215
The manuscripts provides a novel starting guess for the solution of Kepler’s equation for unknown eccentric anomaly E given the eccentricity e and mean anomaly M of an elliptical orbit.
R. Mathar
Mon, 9 Aug 21
18/51
Comments: 5 pages. C++ source code in anc directory
You must be logged in to post a comment.