CAAElliptical_VelocityAtPerihelion: CAAElliptical_VelocityAtPerihelion
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_VelocityAtPerihelion.R
Description
CAAElliptical_VelocityAtPerihelion
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 perihelion.
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_VelocityAtPerihelion(e = 0.21, a = 1.5)
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/CAAElliptical_VelocityAtPerihelion.R
Description
CAAElliptical_VelocityAtPerihelion
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 perihelion.
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_VelocityAtPerihelion(e = 0.21, a = 1.5)
|
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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