923 lines
37 KiB
XML
923 lines
37 KiB
XML
<?xml version="1.0"?>
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<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
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<fdm_config name="c172" version="2.0" release="BETA"
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xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
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xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
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<fileheader>
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<author> Unknown </author>
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<filecreationdate> 2002-01-01 </filecreationdate>
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<version> $Id$ </version>
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<description> Cessna C-172 </description>
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</fileheader>
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<metrics>
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<wingarea unit="FT2"> 174 </wingarea>
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<wingspan unit="FT"> 35.8 </wingspan>
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<chord unit="FT"> 4.9 </chord>
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<htailarea unit="FT2"> 21.9 </htailarea>
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<htailarm unit="FT"> 15.7 </htailarm>
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<vtailarea unit="FT2"> 16.5 </vtailarea>
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<vtailarm unit="FT"> 0 </vtailarm>
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<location name="AERORP" unit="IN">
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<x> 43.2 </x>
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<y> 0 </y>
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<z> 59.4 </z>
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</location>
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<location name="EYEPOINT" unit="IN">
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<x> 37 </x>
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<y> 0 </y>
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<z> 48 </z>
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</location>
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<location name="VRP" unit="IN">
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<x> 42.6 </x>
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<y> 0 </y>
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<z> 38.5 </z>
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</location>
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</metrics>
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<mass_balance>
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<ixx unit="SLUG*FT2"> 948 </ixx>
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<iyy unit="SLUG*FT2"> 1346 </iyy>
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<izz unit="SLUG*FT2"> 1967 </izz>
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<ixy unit="SLUG*FT2"> -0 </ixy>
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<ixz unit="SLUG*FT2"> -0 </ixz>
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<iyz unit="SLUG*FT2"> -0 </iyz>
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<emptywt unit="LBS"> 1500 </emptywt>
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<location name="CG" unit="IN">
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<x> 41 </x>
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<y> 0 </y>
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<z> 36.5 </z>
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</location>
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<pointmass name="Pilot">
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<weight unit="LBS"> 180 </weight>
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<location name="POINTMASS" unit="IN">
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<x> 36 </x>
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<y> -14 </y>
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<z> 24 </z>
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</location>
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</pointmass>
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<pointmass name="Co-Pilot">
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<weight unit="LBS"> 0 </weight>
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<location name="POINTMASS" unit="IN">
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<x> 36 </x>
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<y> 14 </y>
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<z> 24 </z>
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</location>
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</pointmass>
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<pointmass name="Left Passenger">
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<weight unit="LBS"> 0 </weight>
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<location name="POINTMASS" unit="IN">
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<x> 70 </x>
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<y> -14 </y>
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<z> 24 </z>
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</location>
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</pointmass>
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<pointmass name="Right Passenger">
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<weight unit="LBS"> 0 </weight>
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<location name="POINTMASS" unit="IN">
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<x> 70 </x>
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<y> 14 </y>
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<z> 24 </z>
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</location>
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</pointmass>
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<pointmass name="Baggage">
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<weight unit="LBS"> 0 </weight>
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<location name="POINTMASS" unit="IN">
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<x> 95 </x>
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<y> 0 </y>
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<z> 24 </z>
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</location>
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</pointmass>
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</mass_balance>
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<ground_reactions>
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<contact type="BOGEY" name="NOSE">
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<location unit="IN">
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<x> -6.8 </x>
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<y> 0 </y>
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<z> -19.5</z>
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</location>
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<static_friction> 0.8 </static_friction>
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<dynamic_friction> 0.5 </dynamic_friction>
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<rolling_friction> 0.02 </rolling_friction>
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<spring_coeff unit="LBS/FT"> 1800 </spring_coeff>
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<damping_coeff unit="LBS/FT/SEC"> 600 </damping_coeff>
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<max_steer unit="DEG"> 10 </max_steer>
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<brake_group> NONE </brake_group>
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<retractable>0</retractable>
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</contact>
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<contact type="BOGEY" name="LEFT_MAIN">
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<location unit="IN">
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<x> 58.2 </x>
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<y> -43 </y>
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<z> -15.5 </z>
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</location>
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<static_friction> 0.8 </static_friction>
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<dynamic_friction> 0.5 </dynamic_friction>
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<rolling_friction> 0.02 </rolling_friction>
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<spring_coeff unit="LBS/FT"> 5400 </spring_coeff>
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<damping_coeff unit="LBS/FT/SEC"> 1600 </damping_coeff>
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<max_steer unit="DEG"> 0.0 </max_steer>
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<brake_group> LEFT </brake_group>
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<retractable>0</retractable>
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</contact>
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<contact type="BOGEY" name="RIGHT_MAIN">
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<location unit="IN">
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<x> 58.2 </x>
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<y> 43 </y>
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<z> -15.5 </z>
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</location>
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<static_friction> 0.8 </static_friction>
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<dynamic_friction> 0.5 </dynamic_friction>
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<rolling_friction> 0.02 </rolling_friction>
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<spring_coeff unit="LBS/FT"> 5400 </spring_coeff>
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<damping_coeff unit="LBS/FT/SEC"> 1600 </damping_coeff>
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<max_steer unit="DEG"> 0.0 </max_steer>
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<brake_group> RIGHT </brake_group>
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<retractable>0</retractable>
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</contact>
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<contact type="BOGEY" name="TAIL_SKID">
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<location unit="IN">
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<x> 188 </x>
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<y> 0 </y>
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<z> 8 </z>
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</location>
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<static_friction> 0.2 </static_friction>
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<dynamic_friction> 0.2 </dynamic_friction>
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<rolling_friction> 0.2 </rolling_friction>
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<spring_coeff unit="LBS/FT"> 20000 </spring_coeff>
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<damping_coeff unit="LBS/FT/SEC"> 1000 </damping_coeff>
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<max_steer unit="DEG"> 0.0 </max_steer>
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<brake_group> NONE </brake_group>
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<retractable>0</retractable>
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</contact>
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<contact type="BOGEY" name="LEFT_TIP">
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<location unit="IN">
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<x> 43.2 </x>
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<y> -214.8 </y>
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<z> 59.4 </z>
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</location>
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<static_friction> 0.2 </static_friction>
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<dynamic_friction> 0.2 </dynamic_friction>
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<rolling_friction> 0.2 </rolling_friction>
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<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
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<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
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<max_steer unit="DEG"> 0.0 </max_steer>
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<brake_group> NONE </brake_group>
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<retractable>0</retractable>
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</contact>
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<contact type="BOGEY" name="RIGHT_TIP">
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<location unit="IN">
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<x> 43.2 </x>
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<y> 214.8 </y>
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<z> 59.4 </z>
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</location>
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<static_friction> 0.2 </static_friction>
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<dynamic_friction> 0.2 </dynamic_friction>
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<rolling_friction> 0.2 </rolling_friction>
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<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
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<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
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<max_steer unit="DEG"> 0.0 </max_steer>
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<brake_group> NONE </brake_group>
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<retractable>0</retractable>
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</contact>
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</ground_reactions>
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<propulsion>
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<engine file="eng_io320">
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<location unit="IN">
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<x> -19.7 </x>
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<y> 0 </y>
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<z> 26.6 </z>
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</location>
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<orient unit="DEG">
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<roll> 0.0 </roll>
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<pitch> 0 </pitch>
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<yaw> 0 </yaw>
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</orient>
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<feed>0</feed>
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<feed>1</feed>
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<thruster file="prop_75in2f">
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<location unit="IN">
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<x> -37.7 </x>
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<y> 0 </y>
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<z> 26.6 </z>
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</location>
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<orient unit="DEG">
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<roll> 0.0 </roll>
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<pitch> 0.0 </pitch>
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<yaw> 0.0 </yaw>
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</orient>
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<sense> 1 </sense>
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<p_factor> 5 </p_factor>
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</thruster>
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</engine>
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<tank type="FUEL"> <!-- Tank number 0 -->
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<location unit="IN">
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<x> 56 </x>
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<y> -112 </y>
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<z> 59.4 </z>
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</location>
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<capacity unit="LBS"> 185 </capacity>
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<contents unit="LBS"> 100 </contents>
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</tank>
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<tank type="FUEL"> <!-- Tank number 1 -->
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<location unit="IN">
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<x> 56 </x>
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<y> 112 </y>
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<z> 59.4 </z>
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</location>
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<capacity unit="LBS"> 185 </capacity>
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<contents unit="LBS"> 100 </contents>
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</tank>
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</propulsion>
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<flight_control name="FCS: c172">
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<channel name="Pitch">
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<summer name="Pitch Trim Sum">
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<input>fcs/elevator-cmd-norm</input>
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<input>fcs/pitch-trim-cmd-norm</input>
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<clipto>
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<min>-1</min>
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<max>1</max>
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</clipto>
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</summer>
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<aerosurface_scale name="Elevator Control">
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<input>fcs/pitch-trim-sum</input>
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<gain>0.01745</gain>
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<range>
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<min>-28</min>
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<max>23</max>
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</range>
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<output>fcs/elevator-pos-rad</output>
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</aerosurface_scale>
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<aerosurface_scale name="Elevator Position Normalized">
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<input>fcs/elevator-pos-deg</input>
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<domain>
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<min>-28</min>
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<max>23</max>
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</domain>
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<range>
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<min>-1</min>
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<max>1</max>
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</range>
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<output>fcs/elevator-pos-norm</output>
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</aerosurface_scale>
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</channel>
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<channel name="Roll">
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<summer name="Roll Trim Sum">
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<input>fcs/aileron-cmd-norm</input>
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<input>fcs/roll-trim-cmd-norm</input>
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<clipto>
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<min>-1</min>
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<max>1</max>
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</clipto>
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</summer>
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<aerosurface_scale name="Left Aileron Control">
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<input>fcs/roll-trim-sum</input>
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<gain>0.01745</gain>
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<range>
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<min>-20</min>
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<max>15</max>
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</range>
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<output>fcs/left-aileron-pos-rad</output>
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</aerosurface_scale>
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<aerosurface_scale name="Left Aileron Position Normalized">
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<input>fcs/left-aileron-pos-deg</input>
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<domain>
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<min>-20</min>
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<max>15</max>
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</domain>
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<range>
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<min>-1</min>
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<max>1</max>
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</range>
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<output>fcs/left-aileron-pos-norm</output>
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</aerosurface_scale>
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<aerosurface_scale name="Right Aileron Control">
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<input>fcs/roll-trim-sum</input>
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<gain>-0.01745</gain>
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<range>
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<min>-20</min>
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<max>15</max>
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</range>
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<output>fcs/right-aileron-pos-rad</output>
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</aerosurface_scale>
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<aerosurface_scale name="Right Aileron Position Normalized">
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<input>fcs/right-aileron-pos-deg</input>
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<domain>
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<min>-15</min>
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<max>20</max>
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</domain>
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<range>
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<min>1</min>
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<max>-1</max>
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</range>
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<output>fcs/right-aileron-pos-norm</output>
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</aerosurface_scale>
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</channel>
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<channel name="Yaw">
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<summer name="Yaw Trim Sum">
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<input>fcs/rudder-cmd-norm</input>
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<input>fcs/yaw-trim-cmd-norm</input>
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<clipto>
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<min>-1</min>
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<max>1</max>
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</clipto>
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</summer>
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<aerosurface_scale name="Rudder Control">
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<input>fcs/yaw-trim-sum</input>
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<gain>0.01745</gain>
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<range>
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<min>-16</min>
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<max>16</max>
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</range>
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<output>fcs/rudder-pos-rad</output>
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</aerosurface_scale>
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<aerosurface_scale name="Rudder Position Normalized">
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<input>fcs/rudder-pos-deg</input>
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<domain>
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<min>-16</min>
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<max>16</max>
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</domain>
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<range>
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<min>-1</min>
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<max>1</max>
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</range>
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<output>fcs/rudder-pos-norm</output>
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</aerosurface_scale>
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</channel>
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<channel name="Flaps">
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<kinematic name="Flaps Control">
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<input>fcs/flap-cmd-norm</input>
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<traverse>
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<setting>
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<position>0</position>
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<time>0</time>
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</setting>
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<setting>
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<position>10</position>
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<time>2</time>
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</setting>
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<setting>
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<position>20</position>
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<time>1</time>
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</setting>
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<setting>
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<position>30</position>
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<time>1</time>
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</setting>
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</traverse>
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<output>fcs/flap-pos-deg</output>
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</kinematic>
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<aerosurface_scale name="Flap Position Normalizer">
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<input>fcs/flap-pos-deg</input>
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<domain>
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<min>0</min> <!-- Flaps actual minimum position -->
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<max>30</max> <!-- Flaps actual maximum position -->
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</domain>
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<range>
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<min>0</min> <!-- Flaps normalized minimum position -->
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<max>1</max> <!-- Flaps normalized maximum position -->
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</range>
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<output>fcs/flap-pos-norm</output>
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</aerosurface_scale>
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</channel>
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</flight_control>
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<aerodynamics>
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<alphalimits unit="RAD">
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<min>-0.087</min>
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<max>0.28</max>
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</alphalimits>
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|
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<hysteresis_limits unit="RAD">
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<min>0.09</min>
|
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<max>0.36</max>
|
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</hysteresis_limits>
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|
|
|
<function name="aero/function/kCDge">
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<description>Change_in_drag_due_to_ground_effect</description>
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|
<product>
|
|
<table>
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|
<independentVar>aero/h_b-mac-ft</independentVar>
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|
<tableData>
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|
0.0000 0.4800
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|
0.1000 0.5150
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|
0.1500 0.6290
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|
0.2000 0.7090
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|
0.3000 0.8150
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|
0.4000 0.8820
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|
0.5000 0.9280
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|
0.6000 0.9620
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|
0.7000 0.9880
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|
0.8000 1.0000
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|
0.9000 1.0000
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|
1.0000 1.0000
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|
1.1000 1.0000
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</tableData>
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</table>
|
|
</product>
|
|
</function>
|
|
|
|
<function name="aero/function/kCLge">
|
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<description>Change_in_lift_due_to_ground_effect</description>
|
|
<product>
|
|
<table>
|
|
<independentVar>aero/h_b-mac-ft</independentVar>
|
|
<tableData>
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|
0.0000 1.2030
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|
0.1000 1.1270
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|
0.1500 1.0900
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|
0.2000 1.0730
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|
0.3000 1.0460
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|
0.4000 1.0550
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|
0.5000 1.0190
|
|
0.6000 1.0130
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|
0.7000 1.0080
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|
0.8000 1.0060
|
|
0.9000 1.0030
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|
1.0000 1.0020
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|
1.1000 1.0000
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|
</tableData>
|
|
</table>
|
|
</product>
|
|
</function>
|
|
|
|
<axis name="DRAG">
|
|
<function name="aero/coefficient/CDo">
|
|
<description>Drag_at_zero_lift</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<value>0.027</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/CDDf">
|
|
<description>Delta_drag_due_to_flap_deflection</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>aero/function/kCDge</property>
|
|
<table>
|
|
<independentVar>fcs/flap-pos-deg</independentVar>
|
|
<tableData>
|
|
0.0000 0.0000
|
|
10.0000 0.0070
|
|
20.0000 0.0120
|
|
30.0000 0.0180
|
|
</tableData>
|
|
</table>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/CDwbh">
|
|
<description>Drag_due_to_alpha</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>aero/function/kCDge</property>
|
|
<table>
|
|
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
|
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
|
|
<tableData>
|
|
0.0000 10.0000 20.0000 30.0000
|
|
-0.0873 0.0041 0.0000 0.0005 0.0014
|
|
-0.0698 0.0013 0.0004 0.0025 0.0041
|
|
-0.0524 0.0001 0.0023 0.0059 0.0084
|
|
-0.0349 0.0003 0.0057 0.0108 0.0141
|
|
-0.0175 0.0020 0.0105 0.0172 0.0212
|
|
0.0000 0.0052 0.0168 0.0251 0.0299
|
|
0.0175 0.0099 0.0248 0.0346 0.0402
|
|
0.0349 0.0162 0.0342 0.0457 0.0521
|
|
0.0524 0.0240 0.0452 0.0583 0.0655
|
|
0.0698 0.0334 0.0577 0.0724 0.0804
|
|
0.0873 0.0442 0.0718 0.0881 0.0968
|
|
0.1047 0.0566 0.0874 0.1053 0.1148
|
|
0.1222 0.0706 0.1045 0.1240 0.1343
|
|
0.1396 0.0860 0.1232 0.1442 0.1554
|
|
0.1571 0.0962 0.1353 0.1573 0.1690
|
|
0.1745 0.1069 0.1479 0.1708 0.1830
|
|
0.1920 0.1180 0.1610 0.1849 0.1975
|
|
0.2094 0.1298 0.1746 0.1995 0.2126
|
|
0.2269 0.1424 0.1892 0.2151 0.2286
|
|
0.2443 0.1565 0.2054 0.2323 0.2464
|
|
0.2618 0.1727 0.2240 0.2521 0.2667
|
|
0.2793 0.1782 0.2302 0.2587 0.2735
|
|
0.2967 0.1716 0.2227 0.2507 0.2653
|
|
0.3142 0.1618 0.2115 0.2388 0.2531
|
|
0.3316 0.1475 0.1951 0.2214 0.2351
|
|
0.3491 0.1097 0.1512 0.1744 0.1866
|
|
</tableData>
|
|
</table>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/CDDe">
|
|
<description>Drag_due_to_Elevator_Deflection</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>fcs/mag-elevator-pos-rad</property>
|
|
<value>0.0000</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/CDbeta">
|
|
<description>Drag_due_to_sideslip</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>aero/mag-beta-rad</property>
|
|
<value>0.1700</value>
|
|
</product>
|
|
</function>
|
|
</axis>
|
|
|
|
<axis name="SIDE">
|
|
<function name="aero/coefficient/CYb">
|
|
<description>Side_force_due_to_beta</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<table>
|
|
<independentVar lookup="row">aero/beta-rad</independentVar>
|
|
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
|
|
<tableData>
|
|
0.0000 30.0000
|
|
-0.3490 0.1370 0.1060
|
|
0.0000 0.0000 0.0000
|
|
0.3490 -0.1370 -0.1060
|
|
</tableData>
|
|
</table>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/CYda">
|
|
<description>Side_force_due_to_aileron</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>fcs/left-aileron-pos-rad</property>
|
|
<value>0.0000</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/CYdr">
|
|
<description>Side_force_due_to_rudder</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>fcs/rudder-pos-rad</property>
|
|
<value>0.1870</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/CYp">
|
|
<description>Side_force_due_to_roll_rate</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>aero/bi2vel</property>
|
|
<property>velocities/p-aero-rad_sec</property>
|
|
<table>
|
|
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
|
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
|
|
<tableData>
|
|
0.0000 30.0000
|
|
0.0000 -0.0750 -0.1610
|
|
0.0940 -0.1450 -0.2310
|
|
</tableData>
|
|
</table>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/CYr">
|
|
<description>Side_force_due_to_yaw_rate</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>aero/bi2vel</property>
|
|
<property>velocities/r-aero-rad_sec</property>
|
|
<table>
|
|
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
|
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
|
|
<tableData>
|
|
0.0000 30.0000
|
|
0.0000 0.2140 0.1620
|
|
0.0940 0.2670 0.2150
|
|
</tableData>
|
|
</table>
|
|
</product>
|
|
</function>
|
|
</axis>
|
|
|
|
<axis name="LIFT">
|
|
<function name="aero/coefficient/CLwbh">
|
|
<description>Lift_due_to_alpha</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>aero/function/kCLge</property>
|
|
<table>
|
|
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
|
<independentVar lookup="column">aero/stall-hyst-norm</independentVar>
|
|
<tableData>
|
|
0.0000 1.0000
|
|
-0.0900 -0.2200 -0.2200
|
|
0.0000 0.2500 0.2500
|
|
0.0900 0.7300 0.7300
|
|
0.1000 0.8300 0.7800
|
|
0.1200 0.9200 0.7900
|
|
0.1400 1.0200 0.8100
|
|
0.1600 1.0800 0.8200
|
|
0.1700 1.1300 0.8300
|
|
0.1900 1.1900 0.8500
|
|
0.2100 1.2500 0.8600
|
|
0.2400 1.3500 0.8800
|
|
0.2600 1.4400 0.9000
|
|
0.2800 1.4700 0.9200
|
|
0.3000 1.4300 0.9500
|
|
0.3200 1.3800 0.9900
|
|
0.3400 1.3000 1.0500
|
|
0.3600 1.1500 1.1500
|
|
</tableData>
|
|
</table>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/CLDf">
|
|
<description>Delta_lift_due_to_flap_deflection</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>aero/function/kCLge</property>
|
|
<table>
|
|
<independentVar>fcs/flap-pos-deg</independentVar>
|
|
<tableData>
|
|
0.0000 0.0000
|
|
10.0000 0.2000
|
|
20.0000 0.3000
|
|
30.0000 0.3500
|
|
</tableData>
|
|
</table>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/CLDe">
|
|
<description>Lift_due_to_Elevator_Deflection</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>fcs/elevator-pos-rad</property>
|
|
<value>0.4300</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/CLadot">
|
|
<description>Lift_due_to_alpha_rate</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>aero/alphadot-rad_sec</property>
|
|
<property>aero/ci2vel</property>
|
|
<value>1.7000</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/CLq">
|
|
<description>Lift_due_to_pitch_rate</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>velocities/q-aero-rad_sec</property>
|
|
<property>aero/ci2vel</property>
|
|
<value>3.9000</value>
|
|
</product>
|
|
</function>
|
|
</axis>
|
|
|
|
<axis name="ROLL">
|
|
<function name="aero/coefficient/Clb">
|
|
<description>Roll_moment_due_to_beta</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<table>
|
|
<independentVar>aero/beta-rad</independentVar>
|
|
<tableData>
|
|
-0.3490 0.0322
|
|
0.0000 0.0000
|
|
0.3490 -0.0322
|
|
</tableData>
|
|
</table>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/Clp">
|
|
<description>Roll_moment_due_to_roll_rate_(roll_damping)</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<property>aero/bi2vel</property>
|
|
<property>velocities/p-aero-rad_sec</property>
|
|
<value>-0.4840</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/Clr">
|
|
<description>Roll_moment_due_to_yaw_rate</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<property>aero/bi2vel</property>
|
|
<property>velocities/r-aero-rad_sec</property>
|
|
<table>
|
|
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
|
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
|
|
<tableData>
|
|
0.0000 30.0000
|
|
0.0000 0.0798 0.1246
|
|
0.0940 0.1869 0.2317
|
|
</tableData>
|
|
</table>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/ClDa">
|
|
<description>Roll_moment_due_to_aileron</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<property>fcs/left-aileron-pos-rad</property>
|
|
<value>0.2290</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/Cldr">
|
|
<description>Roll_moment_due_to_rudder</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<property>fcs/rudder-pos-rad</property>
|
|
<value>0.0147</value>
|
|
</product>
|
|
</function>
|
|
</axis>
|
|
|
|
<axis name="PITCH">
|
|
<function name="aero/coefficient/Cmo">
|
|
<description>Pitching_moment_at_zero_alpha</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/cbarw-ft</property>
|
|
<value>0.1000</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/Cmalpha">
|
|
<description>Pitch_moment_due_to_alpha</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/cbarw-ft</property>
|
|
<sin>
|
|
<property>aero/alpha-rad</property>
|
|
</sin>
|
|
<value>-1.8000</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/Cmq">
|
|
<description>Pitch_moment_due_to_pitch_rate</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/cbarw-ft</property>
|
|
<property>aero/ci2vel</property>
|
|
<property>velocities/q-aero-rad_sec</property>
|
|
<value>-12.4000</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/Cmadot">
|
|
<description>Pitch_moment_due_to_alpha_rate</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/cbarw-ft</property>
|
|
<property>aero/ci2vel</property>
|
|
<property>aero/alphadot-rad_sec</property>
|
|
<value>-7.2700</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/Cmde">
|
|
<description>Pitch_moment_due_to_elevator_deflection</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/cbarw-ft</property>
|
|
<property>fcs/elevator-pos-rad</property>
|
|
<value>-1.1220</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/Cmdf">
|
|
<description>Delta_pitching_moment_due_to_flap_deflection</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/cbarw-ft</property>
|
|
<table>
|
|
<independentVar>fcs/flap-pos-deg</independentVar>
|
|
<tableData>
|
|
0.0000 0.0000
|
|
10.0000 -0.0654
|
|
20.0000 -0.0981
|
|
30.0000 -0.1140
|
|
</tableData>
|
|
</table>
|
|
</product>
|
|
</function>
|
|
</axis>
|
|
|
|
<axis name="YAW">
|
|
<function name="aero/coefficient/Cnb">
|
|
<description>Yaw_moment_due_to_beta</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<table>
|
|
<independentVar>aero/beta-rad</independentVar>
|
|
<tableData>
|
|
-0.3490 -0.0205
|
|
0.0000 0.0000
|
|
0.3490 0.0205
|
|
</tableData>
|
|
</table>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/Cnp">
|
|
<description>Yaw_moment_due_to_roll_rate</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<property>aero/bi2vel</property>
|
|
<property>velocities/p-aero-rad_sec</property>
|
|
<value>-0.0278</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/Cnr">
|
|
<description>Yaw_moment_due_to_yaw_rate</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<property>aero/bi2vel</property>
|
|
<property>velocities/r-aero-rad_sec</property>
|
|
<value>-0.0937</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/Cnda">
|
|
<description>Yaw_moment_due_to_aileron</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<property>fcs/left-aileron-pos-rad</property>
|
|
<value>-0.0053</value>
|
|
</product>
|
|
</function>
|
|
<function name="aero/coefficient/Cndr">
|
|
<description>Yaw_moment_due_to_rudder</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<property>fcs/rudder-pos-rad</property>
|
|
<value>-0.0430</value>
|
|
</product>
|
|
</function>
|
|
</axis>
|
|
</aerodynamics>
|
|
<!--
|
|
<output name="JSBout172C.csv" type="CSV" rate="60">
|
|
<property> aero/qbar-psf </property>
|
|
<property> accelerations/udot-ft_sec2 </property>
|
|
<property> accelerations/vdot-ft_sec2 </property>
|
|
<property> accelerations/wdot-ft_sec2 </property>
|
|
<property> accelerations/a-pilot-x-ft_sec2 </property>
|
|
<property> accelerations/a-pilot-y-ft_sec2 </property>
|
|
<property> accelerations/a-pilot-z-ft_sec2 </property>
|
|
<property> accelerations/n-pilot-x-norm </property>
|
|
<property> accelerations/n-pilot-y-norm </property>
|
|
<property> accelerations/n-pilot-z-norm </property>
|
|
<rates> ON </rates>
|
|
<velocities> ON </velocities>
|
|
<forces> ON </forces>
|
|
<moments> ON </moments>
|
|
<position> ON </position>
|
|
<fcs> OFF </fcs>
|
|
<propulsion> OFF </propulsion>
|
|
<aerosurfaces> OFF </aerosurfaces>
|
|
<fcs> OFF </fcs>
|
|
<ground_reactions> OFF </ground_reactions>
|
|
</output>
|
|
-->
|
|
</fdm_config>
|