calcf: Calculate the true anomaly
In EarthSystemDiagnostics/orbitalforcing: Orbital Forcing from Insolation
calcf R Documentation
Calculate the true anomaly
Description
Calculate the true anomaly f (theta) from the eccentricity
anomaly true anomaly = angle between the point and perihelion
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
calcf(E, e)
Value
true anomaly f (theta)
Author(s)
Thomas Laepple
EarthSystemDiagnostics/orbitalforcing documentation built on March 24, 2022, 11:25 a.m.
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| calcf | R Documentation |
Calculate the true anomaly
Description
Calculate the true anomaly f (theta) from the eccentricity anomaly true anomaly = angle between the point and perihelion 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
calcf(E, e)
Value
true anomaly f (theta)
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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