revDay2radMin

This function converts a rotation rate in revolutions per day to radians per
minute. This conversion is useful since values in TLEs are given in revolutions
per day, but the SGP4 and SDP4 propagators require the mean motion to be provided
in radians per minute.

Provides basic functionalities to calculate the position of
satellites given a known state vector. The package includes implementations
of the SGP4 and SDP4 simplified perturbation models to propagate orbital
state vectors, as well as utilities to read TLE files and convert coordinates
between different frames of reference. Several of the functionalities of the
package (including the high-precision numerical orbit propagator) require
the coefficients and data included in the 'asteRiskData' package, available
in a 'drat' repository. To install this data package, run
'install.packages("asteRiskData", repos="https://rafael-ayala.github.io/drat/")'.
Felix R. Hoots, Ronald L. Roehrich and T.S. Kelso (1988) <https://celestrak.org/NORAD/documentation/spacetrk.pdf>.
David Vallado, Paul Crawford, Richard Hujsak and T.S. Kelso (2012) <doi:10.2514/6.2006-6753>.
Felix R. Hoots, Paul W. Schumacher Jr. and Robert A. Glover (2014) <doi:10.2514/1.9161>.

Rafael Ayala

asteRisk

Computation of Satellite Position

Daniel Ayala

David Ruiz

Lara Selles Vidal

revDay2radMin function

<dl> <dt>revPerDay</dt>
<dd>Value of the rotation rate in revolutions per day.</dd></dl>

Arguments

Converts revolutions per day to radians per minute — revDay2radMin

<dl>

 <dt>revPerDay</dt>
<dd>Value of the rotation rate in revolutions per day.</dd>

</dl>

revDay2radMin: Converts revolutions per day to radians per minute

Description

Usage

Value

Arguments

Examples