Description: Gives the solution of transcendental equation using Newton' s method, for solving elliptic orbit and the hyperbolic orbits Kepler equation Eccentric anomaly of the source code and examples universal equation are given to understand the function and examples, is to study the orbital theory of the important functions, are based on the matlab programming
File list (Check if you may need any files):
20090826_kepler_solver
......................\Example_kepler_E.m
......................\Example_kepler_H.m
......................\Example_kepler_U.m
......................\kepler_E.m
......................\kepler_H.m
......................\kepler_U.m
......................\stumpC.m
......................\stumpS.m
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