CAAElliptical_VelocityAtAphelion: CAAElliptical_VelocityAtAphelion
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/CAAElliptical_VelocityAtAphelion.R
Description
CAAElliptical_VelocityAtAphelion
Usage
1
Arguments
e
e The eccentricity of the orbit.
a
a The semi major axis of the orbit in astronomical units.
Value
The velocity of the object in kilometres per second at aphelion.
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
CAAElliptical_VelocityAtAphelion(e = 0.22, a = 2.1)
helixcn/skycalc documentation built on March 31, 2021, 5:45 a.m.
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.
Description Usage Arguments Value Author(s) References Examples
View source: R/CAAElliptical_VelocityAtAphelion.R
Description
CAAElliptical_VelocityAtAphelion
Usage
1 |
Arguments
e |
e The eccentricity of the orbit. |
a |
a The semi major axis of the orbit in astronomical units. |
Value
The velocity of the object in kilometres per second at aphelion.
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 | CAAElliptical_VelocityAtAphelion(e = 0.22, a = 2.1)
|
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.
Embedding an R snippet on your website
Add the following code to your website.
For more information on customizing the embed code, read Embedding Snippets.