CalcE.m
版本 1.0.0.0 (1.4 KB) 作者:
Richard Rieber
Calculates eccentric anomaly given mean anomaly and eccentricity of an elliptical orbit.
Since the eccentric anomaly cannot be directly calculated from certain given values, this function performs a simple Newton-Raphson iteration to solve for the eccentric anomaly within a given tolerance (default 10^-8 radians).
引用格式
Richard Rieber (2024). CalcE.m (https://www.mathworks.com/matlabcentral/fileexchange/6779-calce-m), MATLAB Central File Exchange. 检索来源 .
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Start Hunting!版本 | 已发布 | 发行说明 | |
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1.0.0.0 | Didn't notice that MatLab already had a function entitled calce.m, so the file has been renamed to CalcEA.m. |