aboutsummaryrefslogtreecommitdiff
path: root/ham
diff options
context:
space:
mode:
authorAndrea Sacchetti Picchio <andrea.sacchettipicchio@gmail.com>2023-12-15 22:50:24 +0900
committerWilly Sudiarto Raharjo <willysr@slackbuilds.org>2023-12-16 08:56:03 +0700
commitaac1cf55b3d7dc360ec79e83aff20d1fdaeab514 (patch)
treec7a23267bd55b4fa252c33b95fd870d21dc5e130 /ham
parent7c7dd7439ae1e287bfdf70f4e473b64ccbca56e3 (diff)
ham/sgp4: Added (Simplified perturbations models).
Signed-off-by: Andrew Clemons <andrew.clemons@gmail.com> Signed-off-by: Willy Sudiarto Raharjo <willysr@slackbuilds.org>
Diffstat (limited to 'ham')
-rw-r--r--ham/sgp4/README6
-rw-r--r--ham/sgp4/sgp4.SlackBuild111
-rw-r--r--ham/sgp4/sgp4.info10
-rw-r--r--ham/sgp4/slack-desc19
4 files changed, 146 insertions, 0 deletions
diff --git a/ham/sgp4/README b/ham/sgp4/README
new file mode 100644
index 0000000000000..d746144f42dce
--- /dev/null
+++ b/ham/sgp4/README
@@ -0,0 +1,6 @@
+Simplified perturbations models are a set of five mathematical models
+(SGP, SGP4, SDP4, SGP8 and SDP8) used to calculate orbital state
+vectors of satellites and space debris relative to the Earth-centered
+inertial coordinate system. This set of models is often referred to
+collectively as SGP4 due to the frequency of use of that model
+particularly with two-line element sets produced by NORAD and NASA.
diff --git a/ham/sgp4/sgp4.SlackBuild b/ham/sgp4/sgp4.SlackBuild
new file mode 100644
index 0000000000000..a9f9bc2f4dca8
--- /dev/null
+++ b/ham/sgp4/sgp4.SlackBuild
@@ -0,0 +1,111 @@
+#!/bin/bash
+
+# Slackware build script for sgp4
+
+# Copyright 2023 Andrea Sacchetti Picchio Italy
+# All rights reserved.
+#
+# Redistribution and use of this script, with or without modification, is
+# permitted provided that the following conditions are met:
+#
+# 1. Redistributions of this script must retain the above copyright
+# notice, this list of conditions and the following disclaimer.
+#
+# THIS SOFTWARE IS PROVIDED BY THE AUTHOR "AS IS" AND ANY EXPRESS OR IMPLIED
+# WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE IMPLIED WARRANTIES OF
+# MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO
+# EVENT SHALL THE AUTHOR BE LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL,
+# SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO,
+# PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS;
+# OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY,
+# WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR
+# OTHERWISE) ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF
+# ADVISED OF THE POSSIBILITY OF SUCH DAMAGE.
+
+cd $(dirname $0) ; CWD=$(pwd)
+
+PRGNAM=sgp4
+VERSION=${VERSION:-20231211.6a448b48}
+SRCVERSION=${SRCVERSION:-6a448b4850e5fbf8c1ca03bb5f6013a9fdc1fd91}
+BUILD=${BUILD:-1}
+TAG=${TAG:-_SBo}
+PKGTYPE=${PKGTYPE:-tgz}
+
+if [ -z "$ARCH" ]; then
+ case "$( uname -m )" in
+ i?86) ARCH=i586 ;;
+ arm*) ARCH=arm ;;
+ *) ARCH=$( uname -m ) ;;
+ esac
+fi
+
+if [ ! -z "${PRINT_PACKAGE_NAME}" ]; then
+ echo "$PRGNAM-$VERSION-$ARCH-$BUILD$TAG.$PKGTYPE"
+ exit 0
+fi
+
+TMP=${TMP:-/tmp/SBo}
+PKG=$TMP/package-$PRGNAM
+OUTPUT=${OUTPUT:-/tmp}
+
+if [ "$ARCH" = "i586" ]; then
+ SLKCFLAGS="-O2 -march=i586 -mtune=i686"
+ LIBDIRSUFFIX=""
+elif [ "$ARCH" = "i686" ]; then
+ SLKCFLAGS="-O2 -march=i686 -mtune=i686"
+ LIBDIRSUFFIX=""
+elif [ "$ARCH" = "x86_64" ]; then
+ SLKCFLAGS="-O2 -fPIC"
+ LIBDIRSUFFIX="64"
+elif [ "$ARCH" = "aarch64" ]; then
+ SLKCFLAGS="-O2 -fPIC"
+ LIBDIRSUFFIX="64"
+else
+ SLKCFLAGS="-O2"
+ LIBDIRSUFFIX=""
+fi
+
+set -e
+
+rm -rf $PKG
+mkdir -p $TMP $PKG $OUTPUT
+cd $TMP
+
+rm -rf $PRGNAM-$SRCVERSION
+unzip $CWD/$PRGNAM-$SRCVERSION.zip
+cd $PRGNAM-$SRCVERSION
+
+chown -R root:root .
+find -L . \
+ \( -perm 777 -o -perm 775 -o -perm 750 -o -perm 711 -o -perm 555 \
+ -o -perm 511 \) -exec chmod 755 {} \; -o \
+ \( -perm 666 -o -perm 664 -o -perm 640 -o -perm 600 -o -perm 444 \
+ -o -perm 440 -o -perm 400 \) -exec chmod 644 {} \;
+
+mkdir -p build
+cd build
+ cmake \
+ -DCMAKE_C_FLAGS:STRING="$SLKCFLAGS -lserialdv" \
+ -DCMAKE_CXX_FLAGS:STRING="$SLKCFLAGS -lserialdv" \
+ -DCMAKE_INSTALL_PREFIX=/usr \
+ -DLIB_SUFFIX=${LIBDIRSUFFIX} \
+ -DMAN_INSTALL_DIR=/usr/man \
+ -DCMAKE_BUILD_TYPE=Release ..
+ make
+ make install/strip DESTDIR=$PKG
+cd ..
+
+# Fix (it seems that LIB_SUFFIX is not taken into account)
+[ -d $PKG/usr/lib -a ! -e $PKG/usr/lib$LIBDIRSUFFIX ] && mv $PKG/usr/lib $PKG/usr/lib$LIBDIRSUFFIX
+
+mkdir -p $PKG/usr/doc/$PRGNAM-$VERSION
+cp -a \
+ LICENSE README.md \
+ $PKG/usr/doc/$PRGNAM-$VERSION
+cat $CWD/$PRGNAM.SlackBuild > $PKG/usr/doc/$PRGNAM-$VERSION/$PRGNAM.SlackBuild
+
+mkdir -p $PKG/install
+cat $CWD/slack-desc > $PKG/install/slack-desc
+
+cd $PKG
+/sbin/makepkg -l y -c n $OUTPUT/$PRGNAM-$VERSION-$ARCH-$BUILD$TAG.$PKGTYPE
diff --git a/ham/sgp4/sgp4.info b/ham/sgp4/sgp4.info
new file mode 100644
index 0000000000000..4f1ce6b7ed916
--- /dev/null
+++ b/ham/sgp4/sgp4.info
@@ -0,0 +1,10 @@
+PRGNAM="sgp4"
+VERSION="20231211.6a448b48"
+HOMEPAGE="https://github.com/dnwrnr/sgp4/"
+DOWNLOAD="https://github.com/dnwrnr/sgp4/archive/6a448b48/sgp4-6a448b4850e5fbf8c1ca03bb5f6013a9fdc1fd91.zip"
+MD5SUM="90b246600ec54eaeb35f414accc020d4"
+DOWNLOAD_x86_64=""
+MD5SUM_x86_64=""
+REQUIRES="serialDV"
+MAINTAINER="Andrea Sacchetti Picchio"
+EMAIL="andrea dot sacchettipicchio at gmail dot com"
diff --git a/ham/sgp4/slack-desc b/ham/sgp4/slack-desc
new file mode 100644
index 0000000000000..7b42e4636a69a
--- /dev/null
+++ b/ham/sgp4/slack-desc
@@ -0,0 +1,19 @@
+# HOW TO EDIT THIS FILE:
+# The "handy ruler" below makes it easier to edit a package description.
+# Line up the first '|' above the ':' following the base package name, and
+# the '|' on the right side marks the last column you can put a character in.
+# You must make exactly 11 lines for the formatting to be correct. It's also
+# customary to leave one space after the ':' except on otherwise blank lines.
+
+ |-----handy-ruler------------------------------------------------------|
+sgp4: sgp4 (Satellites Tracking library)
+sgp4:
+sgp4: SGP4 is mathematical model used to calculate orbital state vectors of
+sgp4: satellites and space debris relative to the Earth-centered inertial
+sgp4: coordinate system.
+sgp4:
+sgp4:
+sgp4:
+sgp4:
+sgp4: Homepage: https://github.com/dnwrnr/sgp4/
+sgp4: