Description Usage Arguments Value Author(s) References Examples
View source: R/CAAKepler_Calculate.R
CAAKepler_Calculate
1 | CAAKepler_Calculate(M, e, nIterations)
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M |
M The mean anomaly in degrees. |
e |
e The eccentricity of the orbit |
nIterations |
nIterations The method uses the third method to solve the equation. This uses a binary chop to find the solution. The default value of 53 is the number of iterations required to obtain the accuracy of the standard Visual C "double". |
The Eccentric anomaly in degrees (i.e. the solution to Kepler's equation).
C++ code by PJ Naughter, imported to R by Jinlong Zhang
Meeus, J. H. (1991). Astronomical algorithms. Willmann-Bell, Incorporated.
1 | CAAKepler_Calculate(M = 120, e = 0.22, nIterations = 40)
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