Remove intlclock-applet, this has been superceeded by the new clock applet in GNOME 2.21/2.22

svn path=/; revision=55

3 files changed, 0 insertions, 562 deletions

diff --git a/gnome-extra/intlclock-applet/Manifest b/gnome-extra/intlclock-applet/Manifest
deleted file mode 100644
index d4b47d4..0000000
--- a/gnome-extra/intlclock-applet/Manifest
+++ /dev/null
@@ -1,12 +0,0 @@
-AUX intlclock-sunpos-gpl.patch 16071 RMD160 76a00b20a18a7b0d4dacf28bbfdf4f8ca00ffe7c SHA1 e69cd3cfc03a1d2d291e10f16450e7a466a0b892 SHA256 680a55ecd34ad2021c085d45f8255c514ef80a22d77bda2e6075141678c1d419
-MD5 2066ccd2e7bffad1203f2abbe7648888 files/intlclock-sunpos-gpl.patch 16071
-RMD160 76a00b20a18a7b0d4dacf28bbfdf4f8ca00ffe7c files/intlclock-sunpos-gpl.patch 16071
-SHA256 680a55ecd34ad2021c085d45f8255c514ef80a22d77bda2e6075141678c1d419 files/intlclock-sunpos-gpl.patch 16071
-DIST intlclock-1.0.tar.gz 605354 RMD160 d463895c794c2dc19f1bd6169903984063369f4b SHA1 29b61d0108a49b2e415aaeb2b71b58ef7804a47f SHA256 8848af9c052c45c5b6304143a22b9ef01d1249db66b30bf0cfdea499a13c7f3a
-EBUILD intlclock-applet-1.0.ebuild 993 RMD160 673891b1366c84c4a18d2cca0114a0c6144dfe44 SHA1 ef6b0fa8df7effdae5b95b710d349ec8d5770805 SHA256 42c4061d1f062d3339e1910e7443b79585de24eeb7e75b79c7aa9057a6d6990f
-MD5 8bc352f3075ac9fc64ac1dcabda384d2 intlclock-applet-1.0.ebuild 993
-RMD160 673891b1366c84c4a18d2cca0114a0c6144dfe44 intlclock-applet-1.0.ebuild 993
-SHA256 42c4061d1f062d3339e1910e7443b79585de24eeb7e75b79c7aa9057a6d6990f intlclock-applet-1.0.ebuild 993
-MD5 023771a1f08e7b1cfe6320a7496d9cb6 files/digest-intlclock-applet-1.0 241
-RMD160 3e6ac668649d3ee94e2a9b2e302c255b8590815e files/digest-intlclock-applet-1.0 241
-SHA256 9cffc1a24561f00c8181459d53b0153f76790d84fdc811a5f383354c7fc8f62d files/digest-intlclock-applet-1.0 241
diff --git a/gnome-extra/intlclock-applet/files/intlclock-sunpos-gpl.patch b/gnome-extra/intlclock-applet/files/intlclock-sunpos-gpl.patch
deleted file mode 100644
index 7e8178b..0000000
--- a/gnome-extra/intlclock-applet/files/intlclock-sunpos-gpl.patch
+++ /dev/null
@@ -1,508 +0,0 @@
---- src/intlclock-map.c
-+++ src/intlclock-map.c
-@@ -516,7 +516,7 @@
-         width = gdk_pixbuf_get_width (pixbuf);
-         height = gdk_pixbuf_get_height (pixbuf);
- 
--        sun_position (now, &sun_lat, &sun_lon);
-+        get_sun_position (now, &sun_lat, &sun_lon);
- 
-         for (y = 0; y < height; y++) {
-                 gdouble lat = (height / 2.0 - y) / (height / 2.0) * 90.0;
---- src/intlclock-sunpos.c
-+++ src/intlclock-sunpos.c
-@@ -1,348 +1,189 @@
- /*
-- * sunpos.c
-- * kirk johnson
-- * july 1993
-+ *  Copyright (C) 2007 Red Hat, Inc.
-  *
-- * includes revisions from Frank T. Solensky, february 1999
-+ *  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 2, 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.
-  *
-- * code for calculating the position on the earth's surface for which
-- * the sun is directly overhead (adapted from _practical astronomy
-- * with your calculator, third edition_, peter duffett-smith,
-- * cambridge university press, 1988.)
-- *
-- * Copyright (C) 1989, 1990, 1993-1995, 1999 Kirk Lauritz Johnson
-- *
-- * Parts of the source code (as marked) are:
-- *   Copyright (C) 1989, 1990, 1991 by Jim Frost
-- *   Copyright (C) 1992 by Jamie Zawinski <jwz@lucid.com>
-- *
-- * Permission to use, copy, modify and freely distribute xearth for
-- * non-commercial and not-for-profit purposes is hereby granted
-- * without fee, provided that both the above copyright notice and this
-- * permission notice appear in all copies and in supporting
-- * documentation.
-- *
-- * Unisys Corporation holds worldwide patent rights on the Lempel Zev
-- * Welch (LZW) compression technique employed in the CompuServe GIF
-- * image file format as well as in other formats. Unisys has made it
-- * clear, however, that it does not require licensing or fees to be
-- * paid for freely distributed, non-commercial applications (such as
-- * xearth) that employ LZW/GIF technology. Those wishing further
-- * information about licensing the LZW patent should contact Unisys
-- * directly at (lzw_info@unisys.com) or by writing to
-- *
-- *   Unisys Corporation
-- *   Welch Licensing Department
-- *   M/S-C1SW19
-- *   P.O. Box 500
-- *   Blue Bell, PA 19424
-- *
-- * The author makes no representations about the suitability of this
-- * software for any purpose. It is provided "as is" without express or
-- * implied warranty.
-- *
-- * THE AUTHOR DISCLAIMS ALL WARRANTIES WITH REGARD TO THIS SOFTWARE,
-- * INCLUDING ALL IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS,
-- * IN NO EVENT SHALL THE AUTHOR BE LIABLE FOR ANY SPECIAL, INDIRECT
-- * OR CONSEQUENTIAL DAMAGES OR ANY DAMAGES WHATSOEVER RESULTING FROM
-- * LOSS OF USE, DATA OR PROFITS, WHETHER IN AN ACTION OF CONTRACT,
-- * NEGLIGENCE OR OTHER TORTIOUS ACTION, ARISING OUT OF OR IN
-- * CONNECTION WITH THE USE OR PERFORMANCE OF THIS SOFTWARE.
-- */
--
--#include <assert.h>
--#include <math.h>
--#include <time.h>
--
--#include "intlclock-sunpos.h"
--
--#define TWOPI         (2*M_PI)
--#define DegsToRads(x) ((x)*(TWOPI/360))
--
--/*
-- * the epoch upon which these astronomical calculations are based is
-- * 1990 january 0.0, 631065600 seconds since the beginning of the
-- * "unix epoch" (00:00:00 GMT, Jan. 1, 1970)
-- *
-- * given a number of seconds since the start of the unix epoch,
-- * DaysSinceEpoch() computes the number of days since the start of the
-- * astronomical epoch (1990 january 0.0)
-+ * AUTHORS: Jonathan Blandford <jrb@redhat.com>, Matthias Clasen <mclasen@redhat.com>
-  */
- 
--#define EpochStart           (631065600)
--#define DaysSinceEpoch(secs) (((secs)-EpochStart)*(1.0/(24*3600)))
- 
--/*
-- * assuming the apparent orbit of the sun about the earth is circular,
-- * the rate at which the orbit progresses is given by RadsPerDay --
-- * TWOPI radians per orbit divided by 365.242191 days per year:
-- */
--
--#define RadsPerDay (TWOPI/365.242191)
-+#include <time.h>
-+#include <gtk/gtk.h>
-+#include <math.h>
- 
--/*
-- * details of sun's apparent orbit at epoch 1990.0 (after
-- * duffett-smith, table 6, section 46)
-- *
-- * Epsilon_g    (ecliptic longitude at epoch 1990.0) 279.403303 degrees
-- * OmegaBar_g   (ecliptic longitude of perigee)      282.768422 degrees
-- * Eccentricity (eccentricity of orbit)                0.016713
-+/* Calculated with the methods and figures from "Practical Astronomy With Your
-+ * Calculator, version 3" by Peter Duffet-Smith.
-  */
-+/* Table 6.  Details of the Sun's apparent orbit at epoch 1990.0 */
- 
--#define Epsilon_g    (DegsToRads(279.403303))
--#define OmegaBar_g   (DegsToRads(282.768422))
--#define Eccentricity (0.016713)
-+#define EPOCH          2447891.5  /* days */    /* epoch 1990 */
-+#define UNIX_EPOCH     2440586.5  /* days */    /* epoch 1970 */
-+#define EPSILON_G      279.403303 /* degrees */ /* ecliptic longitude at epoch 1990.0 */
-+#define PI_G           282.768422 /* degrees */ /* ecliptic longitude at perigree */
-+#define ECCENTRICITY   0.016713                 /* eccentricity of orbit */
-+#define R_0            149598500  /* km */      /* semi-major access */
-+#define THETA_0        0.533128   /* degrees */ /* angular diameter at r = r_0 */
-+#define MEAN_OBLIQUITY 23.440592  /* degrees */ /* mean obliquity of earths axis at epoch 1990.0 */
- 
--/*
-- * MeanObliquity gives the mean obliquity of the earth's axis at epoch
-- * 1990.0 (computed as 23.440592 degrees according to the method given
-- * in duffett-smith, section 27)
-- */
--#define MeanObliquity (23.440592*(TWOPI/360))
-+/* Constrain x to 0-360 degrees */
-+#define NORMALIZE(x) \
-+  while (x>360) x-=360; while (x<0) x+= 360;
- 
--/*
-- * Lunar parameters, epoch January 0, 1990.0
-- */
--#define MoonMeanLongitude        DegsToRads(318.351648)
--#define MoonMeanLongitudePerigee DegsToRads( 36.340410)
--#define MoonMeanLongitudeNode    DegsToRads(318.510107)
--#define MoonInclination          DegsToRads(  5.145396)
-+#define DEG_TO_RADS(x) \
-+  (x * G_PI/180.0)
- 
--#define SideralMonth (27.3217)
-+#define RADS_TO_DEG(x) \
-+  (x * 180.0/G_PI)
- 
--/*
-- * Force an angular value into the range [-PI, +PI]
-- */
--#define Normalize(x)                        \
--  do {                                      \
--    if ((x) < -M_PI)                        \
--      do (x) += TWOPI; while ((x) < -M_PI); \
--    else if ((x) > M_PI)                    \
--      do (x) -= TWOPI; while ((x) > M_PI);  \
--  } while (0)
--
--static double solve_keplers_equation (double);
--static double mean_sun (double);
--static double sun_ecliptic_longitude (time_t);
--static void   ecliptic_to_equatorial (double, double, double *, double *);
--static double julian_date (int, int, int);
--static double GST (time_t);
--
--/*
-- * solve Kepler's equation via Newton's method
-- * (after duffett-smith, section 47)
-+/* Calculate number of days since 4713BC.
-  */
--static double solve_keplers_equation(M)
--     double M;
-+static gdouble
-+unix_time_to_julian_date (gint unix_time)
- {
--  double E;
--  double delta;
--
--  E = M;
--  while (1)
--  {
--    delta = E - Eccentricity*sin(E) - M;
--    if (fabs(delta) <= 1e-10) break;
--    E -= delta / (1 - Eccentricity*cos(E));
--  }
--
--  return E;
-+  return UNIX_EPOCH + (double) unix_time / (60 * 60 * 24);
- }
- 
-+/* Finds an iterative solution for [ E - e sin (E) = M ] for values of e less
-+   than 0.1.  Page 90  */
- 
--/*
-- * Calculate the position of the mean sun: where the sun would
-- * be if the earth's orbit were circular instead of ellipictal.
-- */
-+#define ERROR_ACCURACY 1e-6 /* radians */
- 
--static double mean_sun (D)
--     double D;                  /* days since ephemeris epoch */
-+static gdouble
-+solve_keplers_equation (gdouble e,
-+			gdouble M)
- {
--  double N, M;
-+  gdouble d, E;
- 
--  N = RadsPerDay * D;
--  N = fmod(N, TWOPI);
--  if (N < 0) N += TWOPI;
--
--  M = N + Epsilon_g - OmegaBar_g;
--  if (M < 0) M += TWOPI;
--  return M;
--}
--
--/*
-- * compute ecliptic longitude of sun (in radians)
-- * (after duffett-smith, section 47)
-- */
--static double sun_ecliptic_longitude(ssue)
--     time_t ssue;               /* seconds since unix epoch */
--{
--  double D;
--  double M_sun, E;
--  double v;
--
--  D = DaysSinceEpoch(ssue);
--  M_sun = mean_sun(D);
-+  /* start with an initial estimate */
-+  E = M;
-+  
-+  d = E - e * sin (E) - M;
- 
--  E = solve_keplers_equation(M_sun);
--  v = 2 * atan(sqrt((1+Eccentricity)/(1-Eccentricity)) * tan(E/2));
-+  while (ABS (d) > ERROR_ACCURACY)
-+    {
-+      E = E - (d / (1 - e * cos (E)));
-+      d = E - e * sin (E) - M;
-+    }
- 
--  return (v + OmegaBar_g);
-+  return E;
- }
- 
-+  /* convert the ecliptic longitude to right ascension and declination.  Section 27.  */
-+static void
-+ecliptic_to_equatorial (gdouble  lambda,
-+			gdouble  beta,
-+			gdouble *ra,
-+			gdouble *dec)
-+{
-+  gdouble cos_mo;
-+  gdouble sin_mo;
-+
-+  g_assert (ra != NULL);
-+  g_assert (dec != NULL);
-+
-+  sin_mo = sin (DEG_TO_RADS (MEAN_OBLIQUITY));
-+  cos_mo = cos (DEG_TO_RADS (MEAN_OBLIQUITY));
-+
-+  *ra = atan2 (sin (lambda) * cos_mo - tan (beta) * sin_mo, cos (lambda));
-+  *dec = asin (sin (beta) * cos_mo + cos (beta) * sin_mo * sin (lambda));
-+}
-+
-+/* calculate GST.  Section 12  */
-+static gdouble
-+greenwich_sidereal_time (gdouble unix_time)
-+{
-+  gdouble u, JD, T, T0, UT;
-+
-+  u = fmod (unix_time, 24 * 60 * 60);
-+  JD = unix_time_to_julian_date (unix_time - u);
-+  T = (JD - 2451545) / 36525;
-+  T0 = 6.697374558 + (2400.051336 * T) + (0.000025862 * T * T);
-+  T0 = fmod (T0, 24);
-+  UT = u / (60 * 60);
-+  T0 = T0 + UT * 1.002737909;
-+  T0 = fmod (T0, 24);
- 
--/*
-- * convert from ecliptic to equatorial coordinates
-- * (after duffett-smith, section 27)
-- */
--static void ecliptic_to_equatorial(lambda, beta, alpha, delta)
--     double  lambda;            /* ecliptic longitude       */
--     double  beta;              /* ecliptic latitude        */
--     double *alpha;             /* (return) right ascension */
--     double *delta;             /* (return) declination     */
--{
--  double sin_e, cos_e;
--
--  sin_e = sin(MeanObliquity);
--  cos_e = cos(MeanObliquity);
--
--  *alpha = atan2(sin(lambda)*cos_e - tan(beta)*sin_e, cos(lambda));
--  *delta = asin(sin(beta)*cos_e + cos(beta)*sin_e*sin(lambda));
-+  return T0;
- }
- 
--
--/*
-- * computing julian dates (assuming gregorian calendar, thus this is
-- * only valid for dates of 1582 oct 15 or later)
-- * (after duffett-smith, section 4)
-- */
--static double julian_date(y, m, d)
--     int y;                     /* year (e.g. 19xx)          */
--     int m;                     /* month (jan=1, feb=2, ...) */
--     int d;                     /* day of month              */
-+/* Calulate the position of the sun at a given time.  pages 89-91 */
-+void
-+get_sun_position (gint unix_time, gdouble *latitude, gdouble *longitude)
- {
--  int    A, B, C, D;
--  double JD;
-+  gdouble jd, D, N, M, E, x, v, lambda;
-+  gdouble ra, dec, lat, lon;
-+  jd = unix_time_to_julian_date (unix_time);
- 
--  /* lazy test to ensure gregorian calendar */
--  assert(y >= 1583);
-+  /* Calculate number of days since the epoch */
-+  D = jd - EPOCH;
- 
--  if ((m == 1) || (m == 2))
--  {
--    y -= 1;
--    m += 12;
--  }
--
--  A = y / 100;
--  B = 2 - A + (A / 4);
--  C = 365.25 * y;
--  D = 30.6001 * (m + 1);
-+  N = D*360/365.242191;
- 
--  JD = B + C + D + d + 1720994.5;
-+  /* noramlize to 0 - 360 degrees */
-+  NORMALIZE (N);
- 
--  return JD;
--}
-+  /* Step 4: */
-+  M = N + EPSILON_G - PI_G;
-+  NORMALIZE (M);
- 
-+  /* Step 5: convert to radians */
-+  M = DEG_TO_RADS (M);
- 
--/*
-- * compute greenwich mean sidereal time (GST) corresponding to a given
-- * number of seconds since the unix epoch
-- * (after duffett-smith, section 12)
-- */
--static double GST(ssue)
--     time_t ssue;               /* seconds since unix epoch */
--{
--  double     JD;
--  double     T, T0;
--  double     UT;
--  struct tm *tm;
--
--  tm = gmtime(&ssue);
-+  /* Step 6: */
-+  E = solve_keplers_equation (ECCENTRICITY, M);
- 
--  JD = julian_date(tm->tm_year+1900, tm->tm_mon+1, tm->tm_mday);
--  T  = (JD - 2451545) / 36525;
-+  /* Step 7: */
-+  x = sqrt ((1 + ECCENTRICITY)/(1 - ECCENTRICITY)) * tan (E/2);
- 
--  T0 = ((T + 2.5862e-5) * T + 2400.051336) * T + 6.697374558;
-+  /* Step 8, 9 */
-+  v = 2 * RADS_TO_DEG (atan (x));
-+  NORMALIZE (v);
- 
--  T0 = fmod(T0, 24.0);
--  if (T0 < 0) T0 += 24;
-+  /* Step 10 */
-+  lambda = v + PI_G;
-+  NORMALIZE (lambda);
- 
--  UT = tm->tm_hour + (tm->tm_min + tm->tm_sec / 60.0) / 60.0;
-+  /* convert the ecliptic longitude to right ascension and declination */
-+  ecliptic_to_equatorial (DEG_TO_RADS (lambda), 0.0, &ra, &dec);
- 
--  T0 += UT * 1.002737909;
--  T0 = fmod(T0, 24.0);
--  if (T0 < 0) T0 += 24;
-+  ra = ra - (G_PI/12) * greenwich_sidereal_time (unix_time);
- 
--  return T0;
-+  *longitude = RADS_TO_DEG (ra);
-+  *latitude = RADS_TO_DEG (dec);
-+/*
-+  NORMALIZE (ra);
-+  NORMALIZE (dec);
-+*/
- }
- 
--
- /*
-- * given a particular time (expressed in seconds since the unix
-- * epoch), compute position on the earth (lat, lon) such that sun is
-- * directly overhead.
-- */
--void sun_position(ssue, lat, lon)
--     time_t  ssue;              /* seconds since unix epoch */
--     double *lat;               /* (return) latitude        */
--     double *lon;               /* (return) longitude       */
-+int
-+main (int argc, char *argv[])
- {
--  double lambda;
--  double alpha, delta;
--  double tmp;
--
--  lambda = sun_ecliptic_longitude(ssue);
--  ecliptic_to_equatorial(lambda, 0.0, &alpha, &delta);
--
--  tmp = alpha - (TWOPI/24)*GST(ssue);
--  Normalize(tmp);
--  *lon = tmp * (360/TWOPI);
--  *lat = delta * (360/TWOPI);
--}
-+  gint i;
-+  gint now;
-+  GTimeVal timeval;
- 
-+  gtk_init (&argc, &argv);
- 
--/*
-- * given a particular time (expressed in seconds since the unix
-- * epoch), compute position on the earth (lat, lon) such that the
-- * moon is directly overhead.
-- *
-- * Based on duffett-smith **2nd ed** section 61; combines some steps
-- * into single expressions to reduce the number of extra variables.
-- */
--void moon_position(ssue, lat, lon)
--     time_t  ssue;              /* seconds since unix epoch */
--     double *lat;               /* (return) latitude        */
--     double *lon;               /* (return) longitude       */
--{
--  double lambda, beta;
--  double D, L, Ms, Mm, N, Ev, Ae, Ec, alpha, delta;
-+  g_get_current_time (&timeval);
-+  now = timeval.tv_sec;
-+
-+  for (i = 0; i < now; i += 15 * 60)
-+    get_sun_position (i);
- 
--  D      = DaysSinceEpoch(ssue);
--  lambda = sun_ecliptic_longitude(ssue);
--  Ms     = mean_sun(D);
--
--  L = fmod(D/SideralMonth, 1.0)*TWOPI + MoonMeanLongitude;
--  Normalize(L);
--  Mm = L - DegsToRads(0.1114041*D) - MoonMeanLongitudePerigee;
--  Normalize(Mm);
--  N = MoonMeanLongitudeNode - DegsToRads(0.0529539*D);
--  Normalize(N);
--  Ev  = DegsToRads(1.2739) * sin(2.0*(L-lambda)-Mm);
--  Ae  = DegsToRads(0.1858) * sin(Ms);
--  Mm += Ev - Ae - DegsToRads(0.37)*sin(Ms);
--  Ec  = DegsToRads(6.2886) * sin(Mm);
--  L  += Ev + Ec - Ae + DegsToRads(0.214) * sin(2.0*Mm);
--  L  += DegsToRads(0.6583) * sin(2.0*(L-lambda));
--  N  -= DegsToRads(0.16) * sin(Ms);
--
--  L -= N;
--  lambda =(fabs(cos(L)) < 1e-12) ?
--    (N + sin(L) * cos(MoonInclination) * M_PI/2) :
--    (N + atan2(sin(L) * cos(MoonInclination), cos(L)));
--  Normalize(lambda);
--  beta = asin(sin(L) * sin(MoonInclination));
--  ecliptic_to_equatorial(lambda, beta, &alpha, &delta);
--  alpha -= (TWOPI/24)*GST(ssue);
--  Normalize(alpha);
--  *lon = alpha * (360/TWOPI);
--  *lat = delta * (360/TWOPI);
-+  return 0;
- }
-+*/
---- src/intlclock-sunpos.h
-+++ src/intlclock-sunpos.h
-@@ -1 +1,2 @@
--void sun_position(time_t ssue, double *lat, double *lon);
-+void
-+get_sun_position (gint unix_time, gdouble *latitude, gdouble *longitude);
diff --git a/gnome-extra/intlclock-applet/intlclock-applet-1.0.ebuild b/gnome-extra/intlclock-applet/intlclock-applet-1.0.ebuild
deleted file mode 100644
index 123bf4c..0000000
--- a/gnome-extra/intlclock-applet/intlclock-applet-1.0.ebuild
+++ /dev/null
@@ -1,42 +0,0 @@
-# Copyright 1999-2007 Gentoo Foundation
-# Distributed under the terms of the GNU General Public License v2
-# $Header: /var/cvsroot/gentoo-x86/gnome-extra/fast-user-switch-applet/fast-user-switch-applet-2.18.0.ebuild,v 1.8 2007/08/28 19:34:07 jer Exp $
-
-inherit eutils gnome2
-
-DESCRIPTION="Enhanced international Clock for the GNOME Panel"
-HOMEPAGE="http://www.gnome.org/"
-MY_PN="intlclock"
-MY_P="${MY_PN}-${PV}"
-SRC_URI="http://dev.gentoo.org/~suka/files/${MY_P}.tar.gz"
-S="${WORKDIR}/${MY_P}"
-
-LICENSE="GPL-2"
-SLOT="0"
-KEYWORDS="~x86"
-IUSE="eds"
-
-RDEPEND=">=dev-libs/glib-2
-	>=x11-libs/gtk+-2
-	>=gnome-base/librsvg-2
-	>=gnome-base/gconf-2
-	>=gnome-base/gnome-panel-2.0
-	>=gnome-base/libgnome-2
-	eds? ( >=gnome-extra/evolution-data-server-1.6 )"
-
-DEPEND="${RDEPEND}"
-
-DOCS="AUTHORS ChangeLog NEWS README"
-USE_DESTDIR="1"
-
-pkg_setup() {
-	GG2CONF="--disable-scrollkeeper $(use_enable eds)"
-}
-
-src_unpack() {
-	unpack ${A}
-	cd ${S}
-	epatch ${FILESDIR}/${MY_PN}-sunpos-gpl.patch
-
-	gnome2_omf_fix
-}