NAME

Astro::Coords::Elements - Specify astronomical coordinates using orbital elements

SYNOPSIS

$c = new Astro::Coords::Elements( elements => \%elements );

DESCRIPTION

This class is used by Astro::Coords for handling coordinates specified as orbital elements.

METHODS

Constructor

new

Instantiate a new object using the supplied options.

$c = new Astro::Coords::Elements( elements => \%elements );
$c = new Astro::Coords::Elements( elements => \@array );

Returns undef on error.

The elements can be specified either by using a reference to an array returned by the array() method of another elements object or in a reference to a hash containing the following keys:

suitable for the major planets:

EPOCH 		 =  epoch of elements t0 (TT MJD)
ORBINC          =  inclination i (radians)
ANODE 		 =  longitude of the ascending node  [$\Omega$] (radians)
PERIH 		 =  longitude of perihelion  [$\varpi$] (radians)
AORQ 		 =  mean distance a (AU)
E 		 =  eccentricity e 
AORL 		 =  mean longitude L (radians)
DM 		 =  daily motion n (radians)

suitable for minor planets:

EPOCH 		 =  epoch of elements t0 (TT MJD)
ORBINC        	 =  inclination i (radians)
ANODE 		 =  longitude of the ascending node  [$\Omega$] (radians)
PERIH 		 =  argument of perihelion  [$\omega$] (radians)
AORQ 		 =  mean distance a (AU)
E 		 =  eccentricity e
AORL 		 =  mean anomaly M (radians)

suitable for comets:

EPOCH 		 =  epoch of elements t0 (TT MJD)
ORBINC        	 =  inclination i (radians)
ANODE 		 =  longitude of the ascending node  [$\Omega$] (radians)
PERIH 		 =  argument of perihelion  [$\omega$] (radians)
AORQ 		 =  perihelion distance q (AU)
E 		 =  eccentricity e
EPOCHPERIH      =  epoch of perihelion T (TT MJD)

See the documentation to slaPlante() and slaPertel() for more information. Keys must be upper case.

For comets if the only one epoch is specified it is assumed that the epochs are identical. This may cause problems if the epochs are not really close to each other.

In order to better match normal usage, EPOCH can also be specified as a string of the form 'YYYY mmm D.frac' (e.g. '1997 Apr 1.567'). (no decimal place after the month). This is the format used by JPL.

Accessor Methods

elements

Returns the hash containing the elements.

%el = $c->elements;

General Methods

array

Return back 11 element array with first element containing the string "ELEMENTS", the next two elements as undef and up to 8 following elements containing the orbital elements in the order presented in the documentation of the constructor.

This method returns a standardised set of elements across all types of coordinates.

Note that for JFORM=3 (Comet) case the epoch of perihelion is stored as the 8th element (the epoch of the elements is still returned as the first element) [corresponding to array index 10]. This usage of the final element can be determined by noting that the element before it (AORL) will be undefined in the case of JFORM=3. If AORL is defined then the Epoch of perihelion will not be written even if it is defined.

type

Returns the generic type associated with the coordinate system. For this class the answer is always "RADEC".

This is used to aid construction of summary tables when using mixed coordinates.

It could be done using isa relationships.

stringify

Stringify overload. Returns comma-separated list of the elements.

summary

Return a one line summary of the coordinates. In the future will accept arguments to control output.

$summary = $c->summary();

apparent

Return the apparent RA and Dec (as two Astro::Coords::Angle objects) for the current coordinates and time. Includes perterbation corrections to convert the elements to the required epoch.

Returns empty list on error.

rv

Radial velocity of the planet relative to the Earth geocentre.

vdefn

Velocity definition. Always 'RADIO'.

vframe

Velocity reference frame. Always 'GEO'.

NOTES

Usually called via Astro::Coords.

LINKS

Useful sources of orbital elements can be found at http://ssd.jpl.nasa.gov and http://cfa-www.harvard.edu/iau/Ephemerides/

REQUIREMENTS

Astro::SLA is used for all internal astrometric calculations.

AUTHOR

Tim Jenness <tjenness@cpan.org>

COPYRIGHT

Copyright (C) 2001-2005 Particle Physics and Astronomy Research Council. All Rights Reserved.

This program is free software; you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation; either version 3 of the License, or (at your option) any later version.

This program is distributed in the hope that it will be useful,but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details.

You should have received a copy of the GNU General Public License along with this program; if not, write to the Free Software Foundation, Inc., 59 Temple Place,Suite 330, Boston, MA 02111-1307, USA