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f16b52.xml
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f16b52.xml
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<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<fdm_config name="General Dynamics YF-16" version="2.0" release="ALPHA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader>
<author> Erik Hofman, Nikolai V. Chr. </author>
<filecreationdate> 2001-12-28 </filecreationdate>
<version> $Revision: 1.93 $ </version>
<license>
<licenseName>GPL (General Public License)</licenseName>
<licenseURL>http://www.gnu.org/licenses/gpl.html</licenseURL>
</license>
<description> Models an F-16 </description>
<note>
This model was created using data that is, or has been, publically
available by means of technical reports, textbooks, image graphs or
published code. This aircraft description file is in no way related
to the manufacturer of the real aircraft.
Neither the name of (any of) the authors nor the names of (any of) the
manufacturers may be used to endorse or promote products derived from
this file.
The data is provided ''as is'' and any express or implied
warranties, including, but not limitted to the implied warranties of
merchantability and fitness for a particular purpose are disclaimed.
</note>
<reference refID="ISBN 0-7232-3458-2" author="William Green" title="General Dynamics F-16 Dash-1" date="1987"/>
<reference refID="NASA TP-1538" author="Nguyen, L. T.; Ogburn, M. E.; Gilbert, W. P.; Kibler, K. S.; Brown, P. W.; Deal, P. L."
title="Simulator study of stall/post-stall characteristics of a fighter airplane with relaxed longitudinal static stability." date="12/1979"/>
<reference refID="AD A 055417" author="Marchand,Michael A" title="Pitch Rate Flight Control for the F-16 Aircraft to Improve Air-To-Air Combat" date="Dec 1977"/>
<reference refID="AD A 189675" author="Kassan, Mark W" title="F-16 Simulator for Man-in-the-Loop Testing of Aircraft Control Systems (SIMTACS)" date="Dec 1987"/>
<reference refID="AFD-070827-032" author="Goddard and Lemm" title="Simulation of the F-16 Lantirn Automatic Terrain Avoidance System" date="Aug 1986"/>
<reference refID="NASA TN-D-8176" author="Gilbert, W. P.; Nguyen, L. T.; Vangunst, R. W."
title="Simulator study of the effectiveness of an automatic control system designed to improve the high-angle-of-attack characteristics of a fighter airplane" date="1976"/>
<reference refID="NASA TP-2857" author="Dale A. Mackall" title="Development and flight test experiences with a flight-crucial digital control system" date="1988"/>
<reference refID="PW-100 Engine" author="Elodie Roux" title="Turbofan and Turbojet Engines: Database Handbook" date="2007"/>
<reference refID="Manual" author="Lockheed Martin" title="F-16C/D Block 50 Flight Manual" date="2 December 1996"/>
<reference refID="Youtube video showing speed brake actuation time (2 secs)" author="MultiplyLeadership's channel"
title="Air-to-air chase video of F-16 AB light off FTT" date="Oct 20, 2010"/>
<reference refID="None" author="Richard Murray" title="http://www.cds.caltech.edu/~murray/projects/afosr95-vehicles/models/f16/" date="n/a"/>
<reference refID="H-1999" author="NASA" title="Dynamic ground effects flight test of an F-15 aircraft" date="n/a"/>
<reference refID="H-2177" author="NASA" title="Dynamic ground effect for a Cranked Arrow Wing Airplane" date="n/a"/>
<reference refID="None" author="n/a" title="http://www.codeonemagazine.com/archives/1991/articles/jul_91/july2a_91.html" date="n/a"/>
</fileheader>
<system file="jsb-hook"/>
<system file="jsb-hydraulics"/>
<system file="jsb-electrical"/>
<system file="jsb-misc"/>
<ground_reactions file="Systems/jsb-ground-reactions"/>
<external_reactions file="Systems/jsb-external-reactions"/>
<system file="jsb-pushback"/>
<metrics file="Systems/jsb-metrics"/>
<mass_balance file="Systems/jsb-mass-52"/>
<flight_control file="Systems/jsb-controls"/>
<system file="autoflight"/>
<propulsion file="Systems/jsb-propulsion-block52"/>
<aerodynamics file="Systems/jsb-aerodynamics-block15-subtle.xml"/>
<!--
<output name="c:/users/nikolai/documents/f16_datalog.csv" type="CSV" rate="120">
<property> fcs/fly-by-wire/pitch/q-washout </property>
<property> velocities/q-aero-deg_sec </property>-->
<!--<property> attitude/phi-rad </property>
<property> position/h-sl-ft </property>
<property> velocities/vc-kts </property>
<property> fcs/throttle-cmd-norm </property>
<property> fcs/elevator-cmd-norm </property>
<property> fcs/pitch-trim-cmd-norm </property>
<property> propulsion/total-fuel-lbs </property>
<property> flight-path/gamma-rad </property>
<property> accelerations/n-pilot-z-norm </property>
<rates> ON </rates>
<velocities> ON </velocities>
<forces> ON </forces>
<moments> ON </moments>
<position> ON </position>
<fcs> ON </fcs>
<propulsion> OFF </propulsion>
<aerosurfaces> ON </aerosurfaces>
<fcs> ON </fcs>
<ground_reactions> ON </ground_reactions>-->
<!--</output>-->
</fdm_config>