CAAElementsPlanetaryOrbit_NeptuneEccentricity: CAAElementsPlanetaryOrbit_NeptuneEccentricity
In helixcn/skycalc: Computational Astronomy in R based on PJ Naughter's AA+ library
Description
Usage
Arguments
Value
Author(s)
References
Examples
View source: R/CAAElementsPlanetaryOrbit_NeptuneEccentricity.R
Description
CAAElementsPlanetaryOrbit_NeptuneEccentricity
Usage
1
Arguments
JD
The date in Dynamical time to calculate for.
Value
the eccentricity of the orbit.
Author(s)
C++ code by PJ Naughter, imported to R by Jinlong Zhang
References
Meeus, J. H. (1991). Astronomical algorithms. Willmann-Bell, Incorporated.
Examples
1
CAAElementsPlanetaryOrbit_NeptuneEccentricity(JD = 2456655.5)
helixcn/skycalc documentation built on March 31, 2021, 5:45 a.m.
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Description Usage Arguments Value Author(s) References Examples
View source: R/CAAElementsPlanetaryOrbit_NeptuneEccentricity.R
Description
CAAElementsPlanetaryOrbit_NeptuneEccentricity
Usage
1 |
Arguments
JD |
The date in Dynamical time to calculate for. |
Value
the eccentricity of the orbit.
Author(s)
C++ code by PJ Naughter, imported to R by Jinlong Zhang
References
Meeus, J. H. (1991). Astronomical algorithms. Willmann-Bell, Incorporated.
Examples
1 | CAAElementsPlanetaryOrbit_NeptuneEccentricity(JD = 2456655.5)
|
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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