Date: Sun, 3 Dec 2017 21:26:18 +0000 (UTC) From: Rodrigo Osorio <rodrigo@FreeBSD.org> To: ports-committers@freebsd.org, svn-ports-all@freebsd.org, svn-ports-head@freebsd.org Subject: svn commit: r455488 - in head/science: . aircraft-datcom Message-ID: <201712032126.vB3LQIfN082718@repo.freebsd.org>
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Author: rodrigo Date: Sun Dec 3 21:26:18 2017 New Revision: 455488 URL: https://svnweb.freebsd.org/changeset/ports/455488 Log: Add new port science/aircraft-datcom aircraft-datcom is a modified version of USAF Aircraft DATCOM The goal of the project is to update the code and make it more usable by the end users PR: 207928 Submitted by: Michael Danilov <mike.d.ft402@gmail.com> Added: head/science/aircraft-datcom/ head/science/aircraft-datcom/Makefile (contents, props changed) head/science/aircraft-datcom/distinfo (contents, props changed) head/science/aircraft-datcom/pkg-descr (contents, props changed) head/science/aircraft-datcom/pkg-plist (contents, props changed) Modified: head/science/Makefile Modified: head/science/Makefile ============================================================================== --- head/science/Makefile Sun Dec 3 20:51:25 2017 (r455487) +++ head/science/Makefile Sun Dec 3 21:26:18 2017 (r455488) @@ -20,6 +20,7 @@ SUBDIR += R-cran-som SUBDIR += R-cran-udunits2 SUBDIR += afni + SUBDIR += aircraft-datcom SUBDIR += avogadro SUBDIR += bddsolve SUBDIR += bft Added: head/science/aircraft-datcom/Makefile ============================================================================== --- /dev/null 00:00:00 1970 (empty, because file is newly added) +++ head/science/aircraft-datcom/Makefile Sun Dec 3 21:26:18 2017 (r455488) @@ -0,0 +1,24 @@ +# $FreeBSD$ + +PORTNAME= aircraft-datcom +DISTVERSION= 0.0.20120723 +CATEGORIES= science + +MAINTAINER= mike.d.ft402@gmail.com +COMMENT= Modified USAF Aircraft Stability and Control Data Compendium + +LICENSE= GPLv3 + +USE_GITHUB= yes +GH_ACCOUNT= arktools +GH_TAGNAME= ed877bb + +USES= fortran cmake + +.include <bsd.port.pre.mk> + +post-install: + ${MKDIR} ${STAGEDIR}${DOCSDIR} + ${INSTALL_MAN} ${WRKSRC}/doc/* ${STAGEDIR}${DOCSDIR} + +.include <bsd.port.post.mk> Added: head/science/aircraft-datcom/distinfo ============================================================================== --- /dev/null 00:00:00 1970 (empty, because file is newly added) +++ head/science/aircraft-datcom/distinfo Sun Dec 3 21:26:18 2017 (r455488) @@ -0,0 +1,3 @@ +TIMESTAMP = 1484250474 +SHA256 (arktools-aircraft-datcom-0.0.20120723-ed877bb_GH0.tar.gz) = e9c8e5cf55f179bf3e3fa0aa27d238455822cc491afebe11b7548661c666f598 +SIZE (arktools-aircraft-datcom-0.0.20120723-ed877bb_GH0.tar.gz) = 38664179 Added: head/science/aircraft-datcom/pkg-descr ============================================================================== --- /dev/null 00:00:00 1970 (empty, because file is newly added) +++ head/science/aircraft-datcom/pkg-descr Sun Dec 3 21:26:18 2017 (r455488) @@ -0,0 +1,15 @@ +This computer program calculates static stability, high lift and control, and +dynamic derivative characteristics using the methods contained in the USAF +Stability and Control Datcom (Data Compendium). Configuration geometry, +attitude, and Mach range capabilities are consistent with those accommodated by +the Datcom. The program contains a trim option that computes control +deflections and aerodynamic increments for vehicle trim at subsonic Mach +numbers. + +WWW: http://www.pdas.com/datcom.html + +This project is a modified version of the publically released USAF aircraft +datcom. The goal of the project is to update the code and make it more usable +by the end user. + +WWW: https://github.com/arktools/aircraft-datcom Added: head/science/aircraft-datcom/pkg-plist ============================================================================== --- /dev/null 00:00:00 1970 (empty, because file is newly added) +++ head/science/aircraft-datcom/pkg-plist Sun Dec 3 21:26:18 2017 (r455488) @@ -0,0 +1,4 @@ +bin/aircraft-datcom +bin/aircraft-datcom-plot +%%PORTDOCS%%%%DOCSDIR%%/Users'_Manual Vol_1.pdf +%%PORTDOCS%%%%DOCSDIR%%/Users'_Manual Vol_2.pdf
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