diff options
author | Andreas Proschofsky <suka@gentoo.org> | 2008-02-19 08:53:43 +0000 |
---|---|---|
committer | Andreas Proschofsky <suka@gentoo.org> | 2008-02-19 08:53:43 +0000 |
commit | d050c7578c2ccee805247bc51790e1da472d4edf (patch) | |
tree | f932261fe6f75636c617b6b5aae0960d62e570b6 /gnome-extra | |
parent | Add ebuilds for the shiny new application launcher gnome-do and the correspon... (diff) | |
download | suka-d050c7578c2ccee805247bc51790e1da472d4edf.tar.gz suka-d050c7578c2ccee805247bc51790e1da472d4edf.tar.bz2 suka-d050c7578c2ccee805247bc51790e1da472d4edf.zip |
Remove intlclock-applet, this has been superceeded by the new clock applet in GNOME 2.21/2.22
svn path=/; revision=55
Diffstat (limited to 'gnome-extra')
-rw-r--r-- | gnome-extra/intlclock-applet/Manifest | 12 | ||||
-rw-r--r-- | gnome-extra/intlclock-applet/files/intlclock-sunpos-gpl.patch | 508 | ||||
-rw-r--r-- | gnome-extra/intlclock-applet/intlclock-applet-1.0.ebuild | 42 |
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 -} |