first commit
This commit is contained in:
Meir Michanie
+843
@@ -0,0 +1,843 @@
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||||
<?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="MQ-9 Reaper" version="2.0" release="ALPHA"
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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> Petar Jedvaj </author>
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<filecreationdate>2016-06-29</filecreationdate>
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<version>$Revision: 1.15 $</version>
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<description> General Atomics MQ-9 Reaper. </description>
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</fileheader>
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<!--
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File: MQ-9 Reaper.xml
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Inputs:
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name: MQ-9 Reaper
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type: WWII fighter, subsonic sport, aerobatic
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max weight: 10495.8 lb
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wing span: 65.62 ft
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length: 36.091 ft
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wing area: 257.2825679 sq-ft
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gear type: tricycle
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retractable?: yes
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||||
# engines: 1
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engine type: turboprop
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engine layout: aft fuselage
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yaw damper? yes
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||||
Outputs:
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wing loading: 40.79 lb/sq-ft
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payload: 4313.6 lbs
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||||
CL-alpha: 4.5 per radian
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CL-0: 0.17
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||||
CL-max: 1.2
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||||
CD-0: 0.02
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||||
K: 0.06
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||||
-->
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||||
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||||
<metrics>
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||||
<wingarea unit="FT2"> 257.28 </wingarea>
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||||
<wingspan unit="FT" > 65.62 </wingspan>
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||||
<wing_incidence> 2.00 </wing_incidence>
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||||
<chord unit="FT" > 3.92 </chord>
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||||
<htailarea unit="FT2"> 32.29 </htailarea>
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||||
<htailarm unit="FT" > 21.65 </htailarm>
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||||
<vtailarea unit="FT2"> 10.76 </vtailarea>
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||||
<vtailarm unit="FT" > 21.65 </vtailarm>
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||||
<location name="AERORP" unit="IN">
|
||||
<x> 173.24 </x>
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||||
<y> 0.00 </y>
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||||
<z> 0.00 </z>
|
||||
</location>
|
||||
<location name="EYEPOINT" unit="IN">
|
||||
<x> 121.27 </x>
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||||
<y> 0.00 </y>
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||||
<z> 40.00 </z>
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||||
</location>
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||||
<location name="VRP" unit="IN">
|
||||
<x>0</x>
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||||
<y>0</y>
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||||
<z>0</z>
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||||
</location>
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||||
</metrics>
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||||
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||||
<mass_balance>
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||||
<ixx unit="SLUG*FT2"> 11946 </ixx>
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||||
<iyy unit="SLUG*FT2"> 6424 </iyy>
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||||
<izz unit="SLUG*FT2"> 17362 </izz>
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||||
<emptywt unit="LBS" > 4902 </emptywt>
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||||
<location name="CG" unit="IN">
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||||
<x> 173.24 </x>
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||||
<y> 0.00 </y>
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||||
<z> -10.83 </z>
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||||
</location>
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||||
<pointmass name="Payload">
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||||
<description> 4314 LBS + full (1280 LBS) fuel should bring model up to entered max weight</description>
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||||
<weight unit="LBS"> 2156.8 </weight>
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||||
<location name="POINTMASS" unit="IN">
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||||
<x> 173.24 </x>
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||||
<y> 0.00 </y>
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||||
<z> -10.83 </z>
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||||
</location>
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||||
</pointmass>
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||||
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||||
<pointmass name="station1">
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||||
<weight unit="LBS"> 100 </weight>
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||||
<location name="POINTMASS" unit="IN">
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||||
<x> 173 </x>
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||||
<y> -89 </y>
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||||
<z> -3 </z>
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||||
</location>
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||||
</pointmass>
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||||
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||||
<pointmass name="station2">
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||||
<weight unit="LBS"> 100 </weight>
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||||
<location name="POINTMASS" unit="IN">
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||||
<x> 173 </x>
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||||
<y> -74 </y>
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||||
<z> -3 </z>
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||||
</location>
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||||
</pointmass>
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||||
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||||
<pointmass name="station3">
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||||
<weight unit="LBS"> 510 </weight>
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||||
<location name="POINTMASS" unit="IN">
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||||
<x> 173 </x>
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||||
<y> -48 </y>
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||||
<z> -3 </z>
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||||
</location>
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||||
</pointmass>
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||||
|
||||
<pointmass name="station4">
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||||
<weight unit="LBS"> 510 </weight>
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||||
<location name="POINTMASS" unit="IN">
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||||
<x> 173 </x>
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||||
<y> 48 </y>
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||||
<z> -3 </z>
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||||
</location>
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||||
</pointmass>
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||||
|
||||
<pointmass name="station5">
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||||
<weight unit="LBS"> 100 </weight>
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||||
<location name="POINTMASS" unit="IN">
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||||
<x> 173 </x>
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||||
<y> 74 </y>
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||||
<z> -3 </z>
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||||
</location>
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||||
</pointmass>
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||||
|
||||
<pointmass name="station6">
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||||
<weight unit="LBS"> 100 </weight>
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||||
<location name="POINTMASS" unit="IN">
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||||
<x> 173 </x>
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||||
<y> 89 </y>
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||||
<z> -3 </z>
|
||||
</location>
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||||
</pointmass>
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||||
|
||||
</mass_balance>
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||||
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||||
<ground_reactions>
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||||
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||||
<contact type="BOGEY" name="NOSE">
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||||
<location unit="IN">
|
||||
<x> 56.30 </x>
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||||
<y> 0.00 </y>
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||||
<z> -51.97 </z>
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||||
</location>
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||||
<static_friction> 0.80 </static_friction>
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||||
<dynamic_friction> 0.50 </dynamic_friction>
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||||
<rolling_friction> 0.02 </rolling_friction>
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||||
<spring_coeff unit="LBS/FT"> 3148.74 </spring_coeff>
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||||
<damping_coeff unit="LBS/FT/SEC"> 5247.90 </damping_coeff>
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||||
<max_steer unit="DEG"> 5.00 </max_steer>
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||||
<brake_group>NONE</brake_group>
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||||
<retractable>1</retractable>
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||||
</contact>
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||||
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||||
<contact type="BOGEY" name="LEFT_MAIN">
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||||
<location unit="IN">
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||||
<x> 180.17 </x>
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||||
<y> -118.12 </y>
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||||
<z> -51.97 </z>
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||||
</location>
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||||
<static_friction> 0.80 </static_friction>
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||||
<dynamic_friction> 0.50 </dynamic_friction>
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||||
<rolling_friction> 0.02 </rolling_friction>
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||||
<spring_coeff unit="LBS/FT"> 10495.80 </spring_coeff>
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||||
<damping_coeff unit="LBS/FT/SEC"> 5247.90 </damping_coeff>
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||||
<max_steer unit="DEG">0</max_steer>
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||||
<brake_group>LEFT</brake_group>
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||||
<retractable>1</retractable>
|
||||
</contact>
|
||||
|
||||
<contact type="BOGEY" name="RIGHT_MAIN">
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||||
<location unit="IN">
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||||
<x> 180.17 </x>
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||||
<y> 118.12 </y>
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||||
<z> -51.97 </z>
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||||
</location>
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||||
<static_friction> 0.80 </static_friction>
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||||
<dynamic_friction> 0.50 </dynamic_friction>
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||||
<rolling_friction> 0.02 </rolling_friction>
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||||
<spring_coeff unit="LBS/FT"> 10495.80 </spring_coeff>
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||||
<damping_coeff unit="LBS/FT/SEC"> 5247.90 </damping_coeff>
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||||
<max_steer unit="DEG">0</max_steer>
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||||
<brake_group>RIGHT</brake_group>
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||||
<retractable>1</retractable>
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||||
</contact>
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||||
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||||
<contact type="STRUCTURE" name="LEFT_WING">
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||||
<location unit="IN">
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||||
<x> 173.24 </x>
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||||
<y> -32.81 </y>
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||||
<z> -10.83 </z>
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||||
</location>
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||||
<static_friction> 1.00 </static_friction>
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||||
<dynamic_friction> 1.00 </dynamic_friction>
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||||
<spring_coeff unit="LBS/FT"> 10495.80 </spring_coeff>
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||||
<damping_coeff unit="LBS/FT/SEC"> 10495.80 </damping_coeff>
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||||
</contact>
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||||
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||||
<contact type="STRUCTURE" name="RIGHT_WING">
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||||
<location unit="IN">
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||||
<x> 173.24 </x>
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||||
<y> 32.81 </y>
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||||
<z> -10.83 </z>
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||||
</location>
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||||
<static_friction> 1.00 </static_friction>
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||||
<dynamic_friction> 1.00 </dynamic_friction>
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||||
<spring_coeff unit="LBS/FT"> 10495.80 </spring_coeff>
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||||
<damping_coeff unit="LBS/FT/SEC"> 10495.80 </damping_coeff>
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||||
</contact>
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||||
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||||
</ground_reactions>
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||||
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||||
<propulsion>
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||||
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||||
<engine file="TPE331-10">
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||||
<location unit="IN">
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||||
<x> 373.09 </x>
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||||
<y> 0.00 </y>
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||||
<z> 0.00 </z>
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||||
</location>
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||||
<orient unit="DEG">
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||||
<pitch> 0.00 </pitch>
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||||
<roll> 0.00 </roll>
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||||
<yaw> 0.00 </yaw>
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||||
</orient>
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||||
<feed>0</feed>
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||||
<thruster file="Direct">
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||||
<location unit="IN">
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||||
<x> 373.09 </x>
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||||
<y> 0.00 </y>
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||||
<z> 0.00 </z>
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||||
</location>
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||||
<orient unit="DEG">
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||||
<pitch> 0.00 </pitch>
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||||
<roll> 0.00 </roll>
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||||
<yaw> 0.00 </yaw>
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||||
</orient>
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||||
</thruster>
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||||
</engine>
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||||
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||||
<tank type="FUEL" number="0">
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||||
<location unit="IN">
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||||
<x> 173.24 </x>
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||||
<y> 0.00 </y>
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||||
<z> -10.83 </z>
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||||
</location>
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||||
<capacity unit="LBS"> 2000.00 </capacity>
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||||
<contents unit="LBS"> 1000.00 </contents>
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||||
</tank>
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||||
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||||
<tank type="FUEL" number="1">
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||||
<location unit="IN">
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||||
<x> 173.24 </x>
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||||
<y> 0.00 </y>
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||||
<z> -10.83 </z>
|
||||
</location>
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||||
<capacity unit="LBS"> 2000.00 </capacity>
|
||||
<contents unit="LBS"> 1000.00 </contents>
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||||
</tank>
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||||
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||||
</propulsion>
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||||
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||||
<system file="Armament"/>
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||||
<system file="Particles"/>
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||||
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||||
<flight_control name="FCS: MQ-9 Reaper">
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||||
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||||
<channel name="Pitch">
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||||
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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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||||
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||||
<aerosurface_scale name="Elevator Control">
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||||
<input>fcs/pitch-trim-sum</input>
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||||
<range>
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||||
<min> -0.35 </min>
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||||
<max> 0.35 </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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||||
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||||
<aerosurface_scale name="elevator normalization">
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||||
<input>fcs/elevator-pos-rad</input>
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||||
<domain>
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||||
<min> -0.35 </min>
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||||
<max> 0.35 </max>
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||||
</domain>
|
||||
<range>
|
||||
<min> -1 </min>
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||||
<max> 1 </max>
|
||||
</range>
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||||
<output>fcs/elevator-pos-norm</output>
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||||
</aerosurface_scale>
|
||||
|
||||
</channel>
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||||
|
||||
<channel name="Roll">
|
||||
|
||||
<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>
|
||||
<clipto>
|
||||
<min> -1 </min>
|
||||
<max> 1 </max>
|
||||
</clipto>
|
||||
</summer>
|
||||
|
||||
<aerosurface_scale name="Left Aileron Control">
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||||
<input>fcs/roll-trim-sum</input>
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||||
<range>
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||||
<min> -0.35 </min>
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||||
<max> 0.35 </max>
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||||
</range>
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||||
<output>fcs/left-aileron-pos-rad</output>
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||||
</aerosurface_scale>
|
||||
|
||||
<aerosurface_scale name="Right Aileron Control">
|
||||
<input>fcs/roll-trim-sum</input>
|
||||
<range>
|
||||
<min> -0.35 </min>
|
||||
<max> 0.35 </max>
|
||||
</range>
|
||||
<output>fcs/right-aileron-pos-rad</output>
|
||||
</aerosurface_scale>
|
||||
|
||||
<aerosurface_scale name="left aileron normalization">
|
||||
<input>fcs/left-aileron-pos-rad</input>
|
||||
<domain>
|
||||
<min> -0.35 </min>
|
||||
<max> 0.35 </max>
|
||||
</domain>
|
||||
<range>
|
||||
<min> -1 </min>
|
||||
<max> 1 </max>
|
||||
</range>
|
||||
<output>fcs/left-aileron-pos-norm</output>
|
||||
</aerosurface_scale>
|
||||
|
||||
<aerosurface_scale name="right aileron normalization">
|
||||
<input>fcs/right-aileron-pos-rad</input>
|
||||
<domain>
|
||||
<min> -0.35 </min>
|
||||
<max> 0.35 </max>
|
||||
</domain>
|
||||
<range>
|
||||
<min> -1 </min>
|
||||
<max> 1 </max>
|
||||
</range>
|
||||
<output>fcs/right-aileron-pos-norm</output>
|
||||
</aerosurface_scale>
|
||||
|
||||
</channel>
|
||||
|
||||
<property value="1">fcs/yaw-damper-enable</property>
|
||||
<channel name="Yaw">
|
||||
|
||||
<summer name="Rudder Command Sum">
|
||||
<input>fcs/rudder-cmd-norm</input>
|
||||
<input>fcs/yaw-trim-cmd-norm</input>
|
||||
<clipto>
|
||||
<min> -1 </min>
|
||||
<max> 1 </max>
|
||||
</clipto>
|
||||
</summer>
|
||||
|
||||
<scheduled_gain name="Yaw Damper Rate">
|
||||
<input>velocities/r-aero-rad_sec</input>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/ve-kts</independentVar>
|
||||
<tableData>
|
||||
30 0.00
|
||||
60 2.00
|
||||
</tableData>
|
||||
</table>
|
||||
<gain>fcs/yaw-damper-enable</gain>
|
||||
</scheduled_gain>
|
||||
|
||||
<summer name="Rudder Sum">
|
||||
<input>fcs/rudder-command-sum</input>
|
||||
<input>fcs/yaw-damper-rate</input>
|
||||
<clipto>
|
||||
<min> -1.1 </min>
|
||||
<max> 1.1 </max>
|
||||
</clipto>
|
||||
</summer>
|
||||
|
||||
<aerosurface_scale name="Rudder Control">
|
||||
<input>fcs/rudder-sum</input>
|
||||
<domain>
|
||||
<min> -1.1 </min>
|
||||
<max> 1.1 </max>
|
||||
</domain>
|
||||
<range>
|
||||
<min> -0.35 </min>
|
||||
<max> 0.35 </max>
|
||||
</range>
|
||||
<output>fcs/rudder-pos-rad</output>
|
||||
</aerosurface_scale>
|
||||
|
||||
<aerosurface_scale name="rudder normalization">
|
||||
<input>fcs/rudder-pos-rad</input>
|
||||
<domain>
|
||||
<min> -0.35 </min>
|
||||
<max> 0.35 </max>
|
||||
</domain>
|
||||
<range>
|
||||
<min> -1 </min>
|
||||
<max> 1 </max>
|
||||
</range>
|
||||
<output>fcs/rudder-pos-norm</output>
|
||||
</aerosurface_scale>
|
||||
|
||||
</channel>
|
||||
|
||||
<channel name="Flaps">
|
||||
<kinematic name="Flaps Control">
|
||||
<input>fcs/flap-cmd-norm</input>
|
||||
<traverse>
|
||||
<setting>
|
||||
<position> 0 </position>
|
||||
<time> 0 </time>
|
||||
</setting>
|
||||
<setting>
|
||||
<position> 15 </position>
|
||||
<time> 4 </time>
|
||||
</setting>
|
||||
<setting>
|
||||
<position> 30 </position>
|
||||
<time> 3 </time>
|
||||
</setting>
|
||||
</traverse>
|
||||
<output>fcs/flap-pos-deg</output>
|
||||
</kinematic>
|
||||
|
||||
<aerosurface_scale name="flap normalization">
|
||||
<input>fcs/flap-pos-deg</input>
|
||||
<domain>
|
||||
<min> 0 </min>
|
||||
<max> 30 </max>
|
||||
</domain>
|
||||
<range>
|
||||
<min> 0 </min>
|
||||
<max> 1 </max>
|
||||
</range>
|
||||
<output>fcs/flap-pos-norm</output>
|
||||
</aerosurface_scale>
|
||||
|
||||
</channel>
|
||||
|
||||
<channel name="Landing Gear">
|
||||
<kinematic name="Gear Control">
|
||||
<input>gear/gear-cmd-norm</input>
|
||||
<traverse>
|
||||
<setting>
|
||||
<position> 0 </position>
|
||||
<time> 0 </time>
|
||||
</setting>
|
||||
<setting>
|
||||
<position> 1 </position>
|
||||
<time> 5 </time>
|
||||
</setting>
|
||||
</traverse>
|
||||
<output>gear/gear-pos-norm</output>
|
||||
</kinematic>
|
||||
|
||||
</channel>
|
||||
|
||||
<channel name="Speedbrake">
|
||||
<kinematic name="Speedbrake Control">
|
||||
<input>fcs/speedbrake-cmd-norm</input>
|
||||
<traverse>
|
||||
<setting>
|
||||
<position> 0 </position>
|
||||
<time> 0 </time>
|
||||
</setting>
|
||||
<setting>
|
||||
<position> 1 </position>
|
||||
<time> 1 </time>
|
||||
</setting>
|
||||
</traverse>
|
||||
<output>fcs/speedbrake-pos-norm</output>
|
||||
</kinematic>
|
||||
|
||||
</channel>
|
||||
|
||||
</flight_control>
|
||||
|
||||
<aerodynamics>
|
||||
|
||||
<axis name="LIFT">
|
||||
|
||||
<function name="aero/force/Lift_alpha">
|
||||
<description>Lift due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-0.20 -0.730
|
||||
0.00 0.170
|
||||
0.23 1.200
|
||||
0.60 0.582
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_flap">
|
||||
<description>Delta Lift due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.01000 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_speedbrake">
|
||||
<description>Delta Lift due to speedbrake</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>0</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Lift_elevator">
|
||||
<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>0.2</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="DRAG">
|
||||
|
||||
<function name="aero/force/Drag_basic">
|
||||
<description>Drag at zero lift</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.500
|
||||
-0.26 0.026
|
||||
0.00 0.020
|
||||
0.26 0.026
|
||||
1.57 1.500
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_induced">
|
||||
<description>Induced drag</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/cl-squared</property>
|
||||
<value>0.06</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_mach">
|
||||
<description>Drag due to mach</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.00 0.000
|
||||
0.75 0.000
|
||||
1.10 0.023
|
||||
1.80 0.015
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_flap">
|
||||
<description>Drag due to flaps</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/flap-pos-deg</property>
|
||||
<value> 0.00133 </value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_gear">
|
||||
<description>Drag due to gear</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>gear/gear-pos-norm</property>
|
||||
<value>0.03</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_speedbrake">
|
||||
<description>Drag due to speedbrakes</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>fcs/speedbrake-pos-norm</property>
|
||||
<value>0.02</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_beta">
|
||||
<description>Drag due to sideslip</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<table>
|
||||
<independentVar lookup="row">aero/beta-rad</independentVar>
|
||||
<tableData>
|
||||
-1.57 1.230
|
||||
-0.26 0.050
|
||||
0.00 0.000
|
||||
0.26 0.050
|
||||
1.57 1.230
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/force/Drag_elevator">
|
||||
<description>Drag due to Elevator Deflection</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<abs><property>fcs/elevator-pos-norm</property></abs>
|
||||
<value>0.04</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="SIDE">
|
||||
|
||||
<function name="aero/force/Side_beta">
|
||||
<description>Side force due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="ROLL">
|
||||
|
||||
<function name="aero/moment/Roll_beta">
|
||||
<description>Roll moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>-0.1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_damp">
|
||||
<description>Roll 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>-0.4</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_yaw">
|
||||
<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>
|
||||
<value>0.15</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_aileron">
|
||||
<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>0.18</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Roll_rudder">
|
||||
<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>0.01</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="PITCH">
|
||||
|
||||
<function name="aero/moment/Pitch_alpha">
|
||||
<description>Pitch moment due to alpha</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>aero/alpha-rad</property>
|
||||
<value>-0.5</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_elevator">
|
||||
<description>Pitch moment due to elevator</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/cbarw-ft</property>
|
||||
<property>fcs/elevator-pos-rad</property>
|
||||
<table>
|
||||
<independentVar lookup="row">velocities/mach</independentVar>
|
||||
<tableData>
|
||||
0.0 -1.000
|
||||
2.0 -0.250
|
||||
</tableData>
|
||||
</table>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_damp">
|
||||
<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>-15</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Pitch_alphadot">
|
||||
<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</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
<axis name="YAW">
|
||||
|
||||
<function name="aero/moment/Yaw_beta">
|
||||
<description>Yaw moment due to beta</description>
|
||||
<product>
|
||||
<property>aero/qbar-psf</property>
|
||||
<property>metrics/Sw-sqft</property>
|
||||
<property>metrics/bw-ft</property>
|
||||
<property>aero/beta-rad</property>
|
||||
<value>0.12</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_damp">
|
||||
<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>-0.15</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_rudder">
|
||||
<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>-0.1</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
<function name="aero/moment/Yaw_aileron">
|
||||
<description>Adverse yaw</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>-0.003</value>
|
||||
</product>
|
||||
</function>
|
||||
|
||||
</axis>
|
||||
|
||||
</aerodynamics>
|
||||
|
||||
<external_reactions>
|
||||
</external_reactions>
|
||||
|
||||
</fdm_config>
|
||||
Reference in New Issue
Block a user