calcE: Calculate the Eccentricity anomaly
In EarthSystemDiagnostics/orbitalforcing: Orbital Forcing from Insolation
calcE R Documentation
Calculate the Eccentricity anomaly
Description
Calculate the Eccentricity anomaly E from the mean anomaly M, iteratively
inversion of Keplers formula: E-e*sin(E)=M
based on Grossman, N.: Orbits under the Inverse Square Law, in
The Sheer Joy of Celestial Mechanics, edited by N. Grossman, pp. 41–61,
Birkhäuser Boston, Boston, MA., 1996.
Usage
calcE(M, e, tol = 1e-08)
Arguments
M
mean anomaly
tol
tolerance
Value
Eccentricity anomaly E
Author(s)
Thomas Laepple
EarthSystemDiagnostics/orbitalforcing documentation built on March 24, 2022, 11:25 a.m.
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| calcE | R Documentation |
Calculate the Eccentricity anomaly
Description
Calculate the Eccentricity anomaly E from the mean anomaly M, iteratively inversion of Keplers formula: E-e*sin(E)=M based on Grossman, N.: Orbits under the Inverse Square Law, in The Sheer Joy of Celestial Mechanics, edited by N. Grossman, pp. 41–61, Birkhäuser Boston, Boston, MA., 1996.
Usage
calcE(M, e, tol = 1e-08)
Arguments
M |
mean anomaly |
tol |
tolerance |
Value
Eccentricity anomaly E
Author(s)
Thomas Laepple
R Package Documentation
Browse R Packages
We want your feedback!
Note that we can't provide technical support on individual packages. You should contact the package authors for that.
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