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714 lines
21 KiB
714 lines
21 KiB
<?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: light commuter with 1 engines
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stall speed: 80.00kts
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max weight: 10494.00 lb
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length: 36.08 ft
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wing:
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span: 65.58 ft
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area: 257.28 sq-ft
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mean chord: 3.92 ft
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aspect ratio: 12.00:1
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taper ratio: 1.00:1
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incidence: 2.00 degrees
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dihedral: 2.00 degrees
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sweep: 5.00 degrees
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no. engines: 1
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engine type: Turboprop Engine
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engine layout: aft fuselage
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gear type: tricycle
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steering type: steering
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retractable?: yes
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Outputs:
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wing loading: 40.79 lb/sq-ft
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payload: 4039.89 lbs
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CL-alpha: 5.79 per radian
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CL-0: 0.41
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CL-max: 1.88
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CD-0: 0.02
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K: 0.04
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Mcrit: 0.70
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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" > 65.58 </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"> 41.17 </htailarea>
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<htailarm unit="FT" > 18.76 </htailarm>
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<vtailarea unit="FT2"> 25.73 </vtailarea>
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<vtailarm unit="FT" > 18.04 </vtailarm>
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<location name="AERORP" unit="IN">
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<x> 207.84 </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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<location name="EYEPOINT" unit="IN">
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<x> 56.29 </x>
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<y> -18.00 </y>
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<z> 45.00 </z>
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</location>
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<location name="VRP" unit="IN">
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<x> 0.0 </x>
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<y> 0.0 </y>
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<z> 0.0 </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"> 11931.18 </ixx>
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<iyy unit="SLUG*FT2"> 6420.77 </iyy>
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<izz unit="SLUG*FT2"> 17344.61 </izz>
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<emptywt unit="LBS" > 4901.00 </emptywt>
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<location name="CG" unit="IN">
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<x> 207.84 </x>
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<y> 0.00 </y>
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<z> -10.82 </z>
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</location>
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<pointmass name="Payload">
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<description> 4039.89 LBS should bring model up to entered max weight</description>
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<weight unit="LBS"> 2019.94 </weight>
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<location name="POINTMASS" unit="IN">
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<x> 207.84 </x>
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<y> 0.00 </y>
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<z> -10.82 </z>
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</location>
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</pointmass>
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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> 207.84 </x>
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<y> 0.00 </y>
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<z> -10.82 </z>
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</location>
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</pointmass>
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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> 207.84 </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="station3">
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<weight unit="LBS"> 510 </weight>
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<location name="POINTMASS" unit="IN">
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<x> 207.84 </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> 207.84 </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> 207.84 </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> 207.84 </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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</mass_balance>
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<propulsion>
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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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<tank type="FUEL" number="0">
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<location unit="IN">
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<x> 207.84 </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"> 776.56 </capacity>
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<contents unit="LBS"> 388.28 </contents>
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</tank>
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<tank type="FUEL" number="1">
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<location unit="IN">
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<x> 207.84 </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"> 776.56 </capacity>
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<contents unit="LBS"> 388.28 </contents>
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</tank>
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</propulsion>
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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> 56.29 </x>
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<y> 0.00 </y>
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<z> -51.96 </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"> 3148.20 </spring_coeff>
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<damping_coeff unit="LBS/FT/SEC"> 1574.10 </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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<contact type="BOGEY" name="LEFT_MAIN">
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<location unit="IN">
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<x> 216.15 </x>
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<y> -70.83 </y>
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<z> -51.96 </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"> 10494.00 </spring_coeff>
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<damping_coeff unit="LBS/FT/SEC"> 5247.00 </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>
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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> 216.15 </x>
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<y> 70.83 </y>
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<z> -51.96 </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"> 10494.00 </spring_coeff>
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<damping_coeff unit="LBS/FT/SEC"> 5247.00 </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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<contact type="STRUCTURE" name="LEFT_WING">
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<location unit="IN">
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<x> 207.84 </x>
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<y> -393.50 </y>
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<z> -10.82 </z>
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</location>
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<static_friction> 1 </static_friction>
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<dynamic_friction> 1 </dynamic_friction>
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<spring_coeff unit="LBS/FT"> 10494.00 </spring_coeff>
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<damping_coeff unit="LBS/FT/SEC"> 10494.00 </damping_coeff>
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</contact>
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<contact type="STRUCTURE" name="RIGHT_WING">
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<location unit="IN">
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<x> 207.84 </x>
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<y> 393.50 </y>
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<z> -10.82 </z>
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</location>
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<static_friction> 1 </static_friction>
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<dynamic_friction> 1 </dynamic_friction>
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<spring_coeff unit="LBS/FT"> 10494.00 </spring_coeff>
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<damping_coeff unit="LBS/FT/SEC"> 10494.00 </damping_coeff>
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</contact>
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</ground_reactions>
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<system file="Armament"/>
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<system file="Particles"/>
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<system file="Controls"/>
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<system file="LandingGear.xml"/>
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<aerodynamics>
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<axis name="LIFT">
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<function name="aero/force/Lift_alpha">
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<description>Lift due to alpha</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<table>
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<independentVar lookup="row">aero/alpha-rad</independentVar>
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<tableData>
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-0.20 -0.7494
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0.00 0.4077
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0.25 1.8824
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0.60 0.9976
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</tableData>
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</table>
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</product>
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</function>
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<function name="aero/force/Lift_pitch_rate">
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<description>Lift due to pitch rate</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>velocities/q-aero-rad_sec</property>
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<property>aero/ci2vel</property>
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<value> 6.4704 </value>
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</product>
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</function>
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<function name="aero/force/Lift_alpha_rate">
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<description>Lift due to alpha rate</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>aero/alphadot-rad_sec</property>
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<property>aero/ci2vel</property>
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<value> 1.8487 </value>
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</product>
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</function>
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<function name="aero/force/Lift_elevator">
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<description>Lift due to Elevator Deflection</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>fcs/elevator-pos-rad</property>
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<value> 0.2732 </value>
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</product>
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</function>
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</axis>
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<axis name="DRAG">
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<function name="aero/force/Drag_basic">
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<description>Drag at zero lift</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<table>
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<independentVar lookup="row">aero/alpha-rad</independentVar>
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<tableData>
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-1.57 1.4089
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-0.25 0.0508
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0.00 0.0219
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0.25 0.0508
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1.57 1.4089
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</tableData>
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</table>
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</product>
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</function>
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<function name="aero/force/Drag_induced">
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<description>Induced drag</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>aero/cl-squared</property>
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<value> 0.0240 </value>
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</product>
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</function>
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<function name="aero/force/Drag_mach">
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<description>Drag due to mach</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<tableData>
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0.00 0.0000
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0.70 0.0000
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1.10 0.0230
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1.80 0.0150
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</tableData>
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</table>
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</product>
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</function>
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<function name="aero/force/Drag_beta">
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<description>Drag due to sideslip</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<table>
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<independentVar lookup="row">aero/beta-rad</independentVar>
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<tableData>
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-1.57 1.2300
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-0.26 0.0500
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0.00 0.0000
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0.26 0.0500
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1.57 1.2300
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</tableData>
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</table>
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</product>
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</function>
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<function name="aero/force/Drag_elevator">
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<description>Drag due to Elevator Deflection</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<abs><property>fcs/elevator-pos-rad</property></abs>
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<value> 0.0400 </value>
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</product>
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</function>
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<function name="aero/force/Drag_gear">
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<description>Drag due to gear</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>gear/gear-pos-norm</property>
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<value> 0.0300 </value>
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</product>
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</function>
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</axis>
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<axis name="SIDE">
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<function name="aero/force/Side_beta">
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<description>Side force due to beta</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>aero/beta-rad</property>
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<value> -0.2310 </value>
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</product>
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</function>
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<function name="aero/force/Side_roll_rate">
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<description>Side force due to roll rate</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>aero/bi2vel</property>
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<property>velocities/p-aero-rad_sec</property>
|
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<table>
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<independentVar lookup="row">aero/Re</independentVar>
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<tableData>
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3372885 1.3390
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|
3710173 0.1141
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|
5059327 0.0507
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6689612 0.0290
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</tableData>
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</table>
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</product>
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</function>
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|
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<function name="aero/force/Side_yaw_rate">
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<description>Side force due to yaw rate</description>
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<product>
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<property>aero/qbar-psf</property>
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<property>metrics/Sw-sqft</property>
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<property>aero/bi2vel</property>
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<property>velocities/r-aero-rad_sec</property>
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|
<value> 0.1271 </value>
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|
</product>
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|
</function>
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<function name="aero/force/Side_rudder">
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<description>Side force due to rudder</description>
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<product>
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<property>aero/qbar-psf</property>
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|
<property>metrics/Sw-sqft</property>
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|
<property>fcs/rudder-pos-rad</property>
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<value> 0.1407 </value>
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|
</product>
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|
</function>
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</axis>
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|
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<axis name="PITCH">
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|
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<function name="aero/moment/Pitch_alpha">
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<description>Pitch moment due to alpha</description>
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|
<product>
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|
<property>aero/qbar-psf</property>
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|
<property>metrics/Sw-sqft</property>
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|
<property>metrics/cbarw-ft</property>
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|
<property>aero/alpha-rad</property>
|
|
<value> -2.3270 </value>
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|
</product>
|
|
</function>
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|
|
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<function name="aero/moment/Pitch_elevator">
|
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<description>Pitch moment due to elevator</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
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|
<property>metrics/Sw-sqft</property>
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|
<property>metrics/cbarw-ft</property>
|
|
<property>fcs/elevator-pos-rad</property>
|
|
<table>
|
|
<independentVar lookup="row">velocities/mach</independentVar>
|
|
<tableData>
|
|
0.0 -2.0259
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|
2.0 -0.5065
|
|
</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> -30.9711 </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> -8.8489 </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>
|
|
<table>
|
|
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
|
<independentVar lookup="column">aero/Re</independentVar>
|
|
<tableData>
|
|
3372885 3710173 5059327 6689612
|
|
-0.0349 -0.2578 -0.0647 -0.0550 -0.0520
|
|
0.3491 -0.6826 -0.1159 -0.1086 -0.1100
|
|
</tableData>
|
|
</table>
|
|
</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> -0.7313 </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>
|
|
<table>
|
|
<independentVar lookup="row">aero/alpha-rad</independentVar>
|
|
<independentVar lookup="column">aero/Re</independentVar>
|
|
<tableData>
|
|
3372885 3710173 5059327 6689612
|
|
-0.0349 0.1627 0.0587 0.0533 0.0514
|
|
0.3491 4.8174 0.6140 0.6086 0.6068
|
|
</tableData>
|
|
</table>
|
|
</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>
|
|
<table>
|
|
<independentVar lookup="row">velocities/mach</independentVar>
|
|
<tableData>
|
|
0.0 0.1700
|
|
2.0 0.0425
|
|
</tableData>
|
|
</table>
|
|
</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> 0.0100 </value>
|
|
</product>
|
|
</function>
|
|
|
|
</axis>
|
|
|
|
<axis name="YAW">
|
|
|
|
<!-- Stall initiator -->
|
|
<function name="aero/moment/Yaw_alpha">
|
|
<description>Yaw moment due to alpha</description>
|
|
<product>
|
|
<property>aero/qbar-psf</property>
|
|
<property>metrics/Sw-sqft</property>
|
|
<property>metrics/bw-ft</property>
|
|
<property>aero/alpha-rad</property>
|
|
<property>fcs/gear-no-wow</property>
|
|
<table>
|
|
<independentVar lookup="row">aero/beta-rad</independentVar>
|
|
<independentVar lookup="column">aero/Re</independentVar>
|
|
<tableData>
|
|
3372885 3710173
|
|
-0.3491 -1.0000 0.0000
|
|
0.3491 1.0000 0.0000
|
|
</tableData>
|
|
</table>
|
|
</product>
|
|
</function>
|
|
|
|
<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> 0.0635 </value>
|
|
</product>
|
|
</function>
|
|
|
|
<function name="aero/moment/Yaw_roll_rate">
|
|
<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-rad_sec</property>
|
|
<table>
|
|
<independentVar lookup="row">aero/Re</independentVar>
|
|
<tableData>
|
|
3372885 -2.3531
|
|
3710173 -0.2005
|
|
5059327 -0.0891
|
|
6689612 -0.0510
|
|
</tableData>
|
|
</table>
|
|
</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> -0.0474 </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> -0.0387 </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> -0.0100 </value>
|
|
</product>
|
|
</function>
|
|
|
|
</axis>
|
|
|
|
</aerodynamics>
|
|
<external_reactions>
|
|
</external_reactions>
|
|
|
|
</fdm_config>
|