From: kruland2607 <kruland2607@180e2498-e6e9-4542-8430-84ac67f01cd8>
Date: Sun, 8 Jan 2012 02:45:53 +0000 (+0000)
Subject: moving to core/
X-Git-Tag: upstream/12.03~1^2~163
X-Git-Url: https://git.gag.com/?a=commitdiff_plain;h=d59c3ed55dff40797c89853a34412efa8815b2b2;p=debian%2Fopenrocket

moving to core/

git-svn-id: https://openrocket.svn.sourceforge.net/svnroot/openrocket/trunk@308 180e2498-e6e9-4542-8430-84ac67f01cd8
---

diff --git a/core/fileformat.txt b/core/fileformat.txt
new file mode 100644
index 00000000..9e04dcff
--- /dev/null
+++ b/core/fileformat.txt
@@ -0,0 +1,41 @@
+
+The current OpenRocket file format is "documented" only as the
+reference implementation.  This will hopefully change in the future.
+
+
+The "version" attribute of the <openrocket> tag describes the file
+format version used, while the "creator" attribute MAY describe the
+software version used to write the document.
+
+The file format version is increased every time the format is
+changed.  The minor number is increased when changes are made that are
+mostly backward-compatible, meaning that older software versions
+should be able to read the design sans the new features.  The major
+number is increased when changes are made that render the design
+problematic or impossible to read for older software.  For maximum
+compatibility software should save a file in the oldest file format
+version that supports all the necessary design features.
+
+
+The following file format versions exist:
+
+
+0.9:  Used before the first public release of Openrocket; effectively
+      equivalent to 1.0.  Should not be used when writing documents.
+      OpenRocket accepts this version when reading files, but other
+      software need not.
+
+1.0:  File format version of the first public release (OpenRocket 0.9.0)
+
+1.1:  Introduced with OpenRocket 0.9.4.  Adds support for saving fin
+      tabs (<tabheight>, <tablength> and <tabposition> elements) and
+      allows attaching subcomponents to a tube coupler (previously
+      forbidden).
+
+1.2:  Introduced with OpenRocket 1.1.1.  Adds the <digest> tag to
+      motor definitions.  The digest uniquely identifies the
+      functional characteristics of a particular thrust curve motor.
+
+1.3:  Introduced with OpenRocket 1.1.9.  Adds the <launchlongitude> and
+      <geodeticmethod> parameters to the simulation conditions element.
+
diff --git a/fileformat.txt b/fileformat.txt
deleted file mode 100644
index 9e04dcff..00000000
--- a/fileformat.txt
+++ /dev/null
@@ -1,41 +0,0 @@
-
-The current OpenRocket file format is "documented" only as the
-reference implementation.  This will hopefully change in the future.
-
-
-The "version" attribute of the <openrocket> tag describes the file
-format version used, while the "creator" attribute MAY describe the
-software version used to write the document.
-
-The file format version is increased every time the format is
-changed.  The minor number is increased when changes are made that are
-mostly backward-compatible, meaning that older software versions
-should be able to read the design sans the new features.  The major
-number is increased when changes are made that render the design
-problematic or impossible to read for older software.  For maximum
-compatibility software should save a file in the oldest file format
-version that supports all the necessary design features.
-
-
-The following file format versions exist:
-
-
-0.9:  Used before the first public release of Openrocket; effectively
-      equivalent to 1.0.  Should not be used when writing documents.
-      OpenRocket accepts this version when reading files, but other
-      software need not.
-
-1.0:  File format version of the first public release (OpenRocket 0.9.0)
-
-1.1:  Introduced with OpenRocket 0.9.4.  Adds support for saving fin
-      tabs (<tabheight>, <tablength> and <tabposition> elements) and
-      allows attaching subcomponents to a tube coupler (previously
-      forbidden).
-
-1.2:  Introduced with OpenRocket 1.1.1.  Adds the <digest> tag to
-      motor definitions.  The digest uniquely identifies the
-      functional characteristics of a particular thrust curve motor.
-
-1.3:  Introduced with OpenRocket 1.1.9.  Adds the <launchlongitude> and
-      <geodeticmethod> parameters to the simulation conditions element.
-