From fa080de7afc95aa1c19a6e6fc0e0708ced2eadc4 Mon Sep 17 00:00:00 2001
From: Joseph Hunkeler <jhunkeler@gmail.com>
Date: Wed, 8 Jul 2015 20:46:52 -0400
Subject: Initial commit

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+.help planel Jun99 "Slalib Package"
+.nf
+
+      SUBROUTINE slPLNE (DATE, JFORM, EPOCH, ORBINC, ANODE, PERIH,
+     :                       AORQ, E, AORL, DM, PV, JSTAT)
+
+     - - - - - - -
+      P L N L
+     - - - - - - -
+
+  Heliocentric position and velocity of a planet, asteroid or comet,
+  starting from orbital elements.
+
+  Given:
+     DATE      d      date, Modified Julian Date (JD - 2400000.5)
+     JFORM     i      choice of element set (1-3; Note 3)
+     EPOCH     d      epoch of elements (TT MJD)
+     ORBINC    d      inclination (radians)
+     ANODE     d      longitude of the ascending node (radians)
+     PERIH     d      longitude or argument of perihelion (radians)
+     AORQ      d      mean distance or perihelion distance (AU)
+     E         d      eccentricity
+     AORL      d      mean anomaly or longitude (radians, JFORM=1,2 only)
+     DM        d      daily motion (radians, JFORM=1 only)
+
+  Returned:
+     PV        d(6)   heliocentric x,y,z,xdot,ydot,zdot of date,
+                                       J2000 equatorial triad (AU,AU/s)
+     JSTAT     i      status:  0 = OK
+                              -1 = illegal JFORM
+                              -2 = illegal E
+                              -3 = illegal AORQ
+                              -4 = illegal DM
+                              -5 = numerical error
+
+  Called:  slELUE, slUEPV
+
+  Notes
+
+  1  DATE is the instant for which the prediction is required.  It is
+     in the TT timescale (formerly Ephemeris Time, ET) and is a
+     Modified Julian Date (JD-2400000.5).
+
+  2  The elements are with respect to the J2000 ecliptic and equinox.
+
+  3  Three different element-format options are available:
+
+     Option JFORM=1, suitable for the major planets:
+
+     EPOCH  = epoch of elements (TT MJD)
+     ORBINC = inclination i (radians)
+     ANODE  = longitude of the ascending node, big omega (radians)
+     PERIH  = longitude of perihelion, curly pi (radians)
+     AORQ   = mean distance, a (AU)
+     E      = eccentricity, e (range 0 to <1)
+     AORL   = mean longitude L (radians)
+     DM     = daily motion (radians)
+
+     Option JFORM=2, suitable for minor planets:
+
+     EPOCH  = epoch of elements (TT MJD)
+     ORBINC = inclination i (radians)
+     ANODE  = longitude of the ascending node, big omega (radians)
+     PERIH  = argument of perihelion, little omega (radians)
+     AORQ   = mean distance, a (AU)
+     E      = eccentricity, e (range 0 to <1)
+     AORL   = mean anomaly M (radians)
+
+     Option JFORM=3, suitable for comets:
+
+     EPOCH  = epoch of perihelion (TT MJD)
+     ORBINC = inclination i (radians)
+     ANODE  = longitude of the ascending node, big omega (radians)
+     PERIH  = argument of perihelion, little omega (radians)
+     AORQ   = perihelion distance, q (AU)
+     E      = eccentricity, e (range 0 to 10)
+
+  4  Unused elements (DM for JFORM=2, AORL and DM for JFORM=3) are
+     not accessed.
+
+  5  The reference frame for the result is with respect to the mean
+     equator and equinox of epoch J2000.
+
+  6  The algorithm was originally adapted from the EPHSLA program of
+     D.H.P.Jones (private communication, 1996).  The method is based
+     on Stumpff's Universal Variables.
+
+  Reference:  Everhart, E. & Pitkin, E.T., Am.J.Phys. 51, 712, 1983.
+
+  P.T.Wallace   Starlink   18 March 1999
+
+  Copyright (C) 1999 Rutherford Appleton Laboratory
+  Copyright (C) 1995 Association of Universities for Research in Astronomy Inc.
+
+.fi
+.endhelp
-- 
cgit 

