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@ -15,150 +15,86 @@
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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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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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# 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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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: 0.06
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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" > 65.62 </wingspan>
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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"> 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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<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> 173.24 </x>
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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> 121.27 </x>
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<y> 0.00 </y>
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<z> 40.00 </z>
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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</x>
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<y>0</y>
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<z>0</z>
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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"> 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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<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> 173.24 </x>
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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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<z> -10.82 </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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<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> 173.24 </x>
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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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<z> -10.82 </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> 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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<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>
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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> 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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<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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<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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</ground_reactions>
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<propulsion>
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<engine file="TPE331-10">
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@ -189,255 +125,106 @@
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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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<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"> 2000.00 </capacity>
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<contents unit="LBS"> 1000.00 </contents>
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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> 173.24 </x>
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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"> 2000.00 </capacity>
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<contents unit="LBS"> 1000.00 </contents>
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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="Particles"/>
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<system file="Controls"/>
|
|
|
|
|
|
|
|
|
|
<flight_control name="FCS: MQ-9 Reaper">
|
|
|
|
|
|
|
|
|
|
<channel name="Pitch">
|
|
|
|
|
|
|
|
|
|
<summer name="Pitch Trim Sum">
|
|
|
|
|
<input>fcs/elevator-cmd-norm</input>
|
|
|
|
|
<input>fcs/pitch-trim-cmd-norm</input>
|
|
|
|
|
<clipto>
|
|
|
|
|
<min> -1 </min>
|
|
|
|
|
<max> 1 </max>
|
|
|
|
|
</clipto>
|
|
|
|
|
</summer>
|
|
|
|
|
|
|
|
|
|
<aerosurface_scale name="Elevator Control">
|
|
|
|
|
<input>fcs/pitch-trim-sum</input>
|
|
|
|
|
<range>
|
|
|
|
|
<min> -0.35 </min>
|
|
|
|
|
<max> 0.35 </max>
|
|
|
|
|
</range>
|
|
|
|
|
<output>fcs/elevator-pos-rad</output>
|
|
|
|
|
</aerosurface_scale>
|
|
|
|
|
|
|
|
|
|
<aerosurface_scale name="elevator normalization">
|
|
|
|
|
<input>fcs/elevator-pos-rad</input>
|
|
|
|
|
<domain>
|
|
|
|
|
<min> -0.35 </min>
|
|
|
|
|
<max> 0.35 </max>
|
|
|
|
|
</domain>
|
|
|
|
|
<range>
|
|
|
|
|
<min> -1 </min>
|
|
|
|
|
<max> 1 </max>
|
|
|
|
|
</range>
|
|
|
|
|
<output>fcs/elevator-pos-norm</output>
|
|
|
|
|
</aerosurface_scale>
|
|
|
|
|
|
|
|
|
|
</channel>
|
|
|
|
|
|
|
|
|
|
<channel name="Roll">
|
|
|
|
|
|
|
|
|
|
<summer name="Roll Trim Sum">
|
|
|
|
|
<input>fcs/aileron-cmd-norm</input>
|
|
|
|
|
<input>fcs/roll-trim-cmd-norm</input>
|
|
|
|
|
<clipto>
|
|
|
|
|
<min> -1 </min>
|
|
|
|
|
<max> 1 </max>
|
|
|
|
|
</clipto>
|
|
|
|
|
</summer>
|
|
|
|
|
|
|
|
|
|
<aerosurface_scale name="Left Aileron Control">
|
|
|
|
|
<input>fcs/roll-trim-sum</input>
|
|
|
|
|
<range>
|
|
|
|
|
<min> -0.35 </min>
|
|
|
|
|
<max> 0.35 </max>
|
|
|
|
|
</range>
|
|
|
|
|
<output>fcs/left-aileron-pos-rad</output>
|
|
|
|
|
</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>
|
|
|
|
|
<system file="LandingGear.xml"/>
|
|
|
|
|
|
|
|
|
|
<aerodynamics>
|
|
|
|
|
|
|
|
|
|
@ -451,32 +238,34 @@
|
|
|
|
|
<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
|
|
|
|
|
-0.20 -0.7494
|
|
|
|
|
0.00 0.4077
|
|
|
|
|
0.25 1.8824
|
|
|
|
|
0.60 0.9976
|
|
|
|
|
</tableData>
|
|
|
|
|
</table>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
<function name="aero/force/Lift_flap">
|
|
|
|
|
<description>Delta Lift due to flaps</description>
|
|
|
|
|
<function name="aero/force/Lift_pitch_rate">
|
|
|
|
|
<description>Lift due to pitch rate</description>
|
|
|
|
|
<product>
|
|
|
|
|
<property>aero/qbar-psf</property>
|
|
|
|
|
<property>metrics/Sw-sqft</property>
|
|
|
|
|
<property>fcs/flap-pos-deg</property>
|
|
|
|
|
<value> 0.01000 </value>
|
|
|
|
|
<property>velocities/q-aero-rad_sec</property>
|
|
|
|
|
<property>aero/ci2vel</property>
|
|
|
|
|
<value> 6.4704 </value>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
<function name="aero/force/Lift_speedbrake">
|
|
|
|
|
<description>Delta Lift due to speedbrake</description>
|
|
|
|
|
<function name="aero/force/Lift_alpha_rate">
|
|
|
|
|
<description>Lift due to alpha rate</description>
|
|
|
|
|
<product>
|
|
|
|
|
<property>aero/qbar-psf</property>
|
|
|
|
|
<property>metrics/Sw-sqft</property>
|
|
|
|
|
<property>fcs/speedbrake-pos-norm</property>
|
|
|
|
|
<value>0</value>
|
|
|
|
|
<property>aero/alphadot-rad_sec</property>
|
|
|
|
|
<property>aero/ci2vel</property>
|
|
|
|
|
<value> 1.8487 </value>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
@ -486,7 +275,7 @@
|
|
|
|
|
<property>aero/qbar-psf</property>
|
|
|
|
|
<property>metrics/Sw-sqft</property>
|
|
|
|
|
<property>fcs/elevator-pos-rad</property>
|
|
|
|
|
<value>0.2</value>
|
|
|
|
|
<value> 0.2732 </value>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
@ -502,11 +291,11 @@
|
|
|
|
|
<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
|
|
|
|
|
-1.57 1.4089
|
|
|
|
|
-0.25 0.0508
|
|
|
|
|
0.00 0.0219
|
|
|
|
|
0.25 0.0508
|
|
|
|
|
1.57 1.4089
|
|
|
|
|
</tableData>
|
|
|
|
|
</table>
|
|
|
|
|
</product>
|
|
|
|
|
@ -518,7 +307,7 @@
|
|
|
|
|
<property>aero/qbar-psf</property>
|
|
|
|
|
<property>metrics/Sw-sqft</property>
|
|
|
|
|
<property>aero/cl-squared</property>
|
|
|
|
|
<value>0.06</value>
|
|
|
|
|
<value> 0.0240 </value>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
@ -530,22 +319,40 @@
|
|
|
|
|
<table>
|
|
|
|
|
<independentVar lookup="row">velocities/mach</independentVar>
|
|
|
|
|
<tableData>
|
|
|
|
|
0.00 0.000
|
|
|
|
|
0.75 0.000
|
|
|
|
|
1.10 0.023
|
|
|
|
|
1.80 0.015
|
|
|
|
|
0.00 0.0000
|
|
|
|
|
0.70 0.0000
|
|
|
|
|
1.10 0.0230
|
|
|
|
|
1.80 0.0150
|
|
|
|
|
</tableData>
|
|
|
|
|
</table>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
<function name="aero/force/Drag_flap">
|
|
|
|
|
<description>Drag due to flaps</description>
|
|
|
|
|
<function name="aero/force/Drag_beta">
|
|
|
|
|
<description>Drag due to sideslip</description>
|
|
|
|
|
<product>
|
|
|
|
|
<property>aero/qbar-psf</property>
|
|
|
|
|
<property>metrics/Sw-sqft</property>
|
|
|
|
|
<property>fcs/flap-pos-deg</property>
|
|
|
|
|
<value> 0.00133 </value>
|
|
|
|
|
<table>
|
|
|
|
|
<independentVar lookup="row">aero/beta-rad</independentVar>
|
|
|
|
|
<tableData>
|
|
|
|
|
-1.57 1.2300
|
|
|
|
|
-0.26 0.0500
|
|
|
|
|
0.00 0.0000
|
|
|
|
|
0.26 0.0500
|
|
|
|
|
1.57 1.2300
|
|
|
|
|
</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-rad</property></abs>
|
|
|
|
|
<value> 0.0400 </value>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
@ -555,59 +362,116 @@
|
|
|
|
|
<property>aero/qbar-psf</property>
|
|
|
|
|
<property>metrics/Sw-sqft</property>
|
|
|
|
|
<property>gear/gear-pos-norm</property>
|
|
|
|
|
<value>0.03</value>
|
|
|
|
|
<value> 0.0300 </value>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
<function name="aero/force/Drag_speedbrake">
|
|
|
|
|
<description>Drag due to speedbrakes</description>
|
|
|
|
|
</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>fcs/speedbrake-pos-norm</property>
|
|
|
|
|
<value>0.02</value>
|
|
|
|
|
<property>aero/beta-rad</property>
|
|
|
|
|
<value> -0.2310 </value>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
<function name="aero/force/Drag_beta">
|
|
|
|
|
<description>Drag due to sideslip</description>
|
|
|
|
|
<function name="aero/force/Side_roll_rate">
|
|
|
|
|
<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/beta-rad</independentVar>
|
|
|
|
|
<independentVar lookup="row">aero/Re</independentVar>
|
|
|
|
|
<tableData>
|
|
|
|
|
-1.57 1.230
|
|
|
|
|
-0.26 0.050
|
|
|
|
|
0.00 0.000
|
|
|
|
|
0.26 0.050
|
|
|
|
|
1.57 1.230
|
|
|
|
|
3372885 1.3390
|
|
|
|
|
3710173 0.1141
|
|
|
|
|
5059327 0.0507
|
|
|
|
|
6689612 0.0290
|
|
|
|
|
</tableData>
|
|
|
|
|
</table>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
<function name="aero/force/Drag_elevator">
|
|
|
|
|
<description>Drag due to Elevator Deflection</description>
|
|
|
|
|
<function name="aero/force/Side_yaw_rate">
|
|
|
|
|
<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>
|
|
|
|
|
<value> 0.1271 </value>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
<function name="aero/force/Side_rudder">
|
|
|
|
|
<description>Side force due to rudder</description>
|
|
|
|
|
<product>
|
|
|
|
|
<property>aero/qbar-psf</property>
|
|
|
|
|
<property>metrics/Sw-sqft</property>
|
|
|
|
|
<abs><property>fcs/elevator-pos-norm</property></abs>
|
|
|
|
|
<value>0.04</value>
|
|
|
|
|
<property>fcs/rudder-pos-rad</property>
|
|
|
|
|
<value> 0.1407 </value>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
</axis>
|
|
|
|
|
|
|
|
|
|
<axis name="SIDE">
|
|
|
|
|
<axis name="PITCH">
|
|
|
|
|
|
|
|
|
|
<function name="aero/force/Side_beta">
|
|
|
|
|
<description>Side force due to beta</description>
|
|
|
|
|
<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>aero/beta-rad</property>
|
|
|
|
|
<value>-1</value>
|
|
|
|
|
<property>metrics/cbarw-ft</property>
|
|
|
|
|
<property>aero/alpha-rad</property>
|
|
|
|
|
<value> -2.3270 </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 -2.0259
|
|
|
|
|
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>
|
|
|
|
|
|
|
|
|
|
@ -622,7 +486,15 @@
|
|
|
|
|
<property>metrics/Sw-sqft</property>
|
|
|
|
|
<property>metrics/bw-ft</property>
|
|
|
|
|
<property>aero/beta-rad</property>
|
|
|
|
|
<value>-0.1</value>
|
|
|
|
|
<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>
|
|
|
|
|
|
|
|
|
|
@ -634,7 +506,7 @@
|
|
|
|
|
<property>metrics/bw-ft</property>
|
|
|
|
|
<property>aero/bi2vel</property>
|
|
|
|
|
<property>velocities/p-aero-rad_sec</property>
|
|
|
|
|
<value>-0.4</value>
|
|
|
|
|
<value> -0.7313 </value>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
@ -646,7 +518,15 @@
|
|
|
|
|
<property>metrics/bw-ft</property>
|
|
|
|
|
<property>aero/bi2vel</property>
|
|
|
|
|
<property>velocities/r-aero-rad_sec</property>
|
|
|
|
|
<value>0.15</value>
|
|
|
|
|
<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>
|
|
|
|
|
|
|
|
|
|
@ -657,7 +537,13 @@
|
|
|
|
|
<property>metrics/Sw-sqft</property>
|
|
|
|
|
<property>metrics/bw-ft</property>
|
|
|
|
|
<property>fcs/left-aileron-pos-rad</property>
|
|
|
|
|
<value>0.18</value>
|
|
|
|
|
<table>
|
|
|
|
|
<independentVar lookup="row">velocities/mach</independentVar>
|
|
|
|
|
<tableData>
|
|
|
|
|
0.0 0.1700
|
|
|
|
|
2.0 0.0425
|
|
|
|
|
</tableData>
|
|
|
|
|
</table>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
@ -668,78 +554,63 @@
|
|
|
|
|
<property>metrics/Sw-sqft</property>
|
|
|
|
|
<property>metrics/bw-ft</property>
|
|
|
|
|
<property>fcs/rudder-pos-rad</property>
|
|
|
|
|
<value>0.01</value>
|
|
|
|
|
<value> 0.0100 </value>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
</axis>
|
|
|
|
|
|
|
|
|
|
<axis name="PITCH">
|
|
|
|
|
<axis name="YAW">
|
|
|
|
|
|
|
|
|
|
<function name="aero/moment/Pitch_alpha">
|
|
|
|
|
<description>Pitch moment due to alpha</description>
|
|
|
|
|
<!-- 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/cbarw-ft</property>
|
|
|
|
|
<property>metrics/bw-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>
|
|
|
|
|
<property>fcs/gear-no-wow</property>
|
|
|
|
|
<table>
|
|
|
|
|
<independentVar lookup="row">velocities/mach</independentVar>
|
|
|
|
|
<independentVar lookup="row">aero/beta-rad</independentVar>
|
|
|
|
|
<independentVar lookup="column">aero/Re</independentVar>
|
|
|
|
|
<tableData>
|
|
|
|
|
0.0 -1.000
|
|
|
|
|
2.0 -0.250
|
|
|
|
|
3372885 3710173
|
|
|
|
|
-0.3491 -1.0000 0.0000
|
|
|
|
|
0.3491 1.0000 0.0000
|
|
|
|
|
</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>
|
|
|
|
|
<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/cbarw-ft</property>
|
|
|
|
|
<property>aero/ci2vel</property>
|
|
|
|
|
<property>aero/alphadot-rad_sec</property>
|
|
|
|
|
<value>-7</value>
|
|
|
|
|
<property>metrics/bw-ft</property>
|
|
|
|
|
<property>aero/beta-rad</property>
|
|
|
|
|
<value> 0.0635 </value>
|
|
|
|
|
</product>
|
|
|
|
|
</function>
|
|
|
|
|
|
|
|
|
|
</axis>
|
|
|
|
|
|
|
|
|
|
<axis name="YAW">
|
|
|
|
|
|
|
|
|
|
<function name="aero/moment/Yaw_beta">
|
|
|
|
|
<description>Yaw moment due to beta</description>
|
|
|
|
|
<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/beta-rad</property>
|
|
|
|
|
<value>0.12</value>
|
|
|
|
|
<property>aero/bi2vel</property>
|
|
|
|
|
<property>velocities/p-rad_sec</property>
|
|
|
|
|
<table>
|
|
|
|
|
<independentVar lookup="row">aero/Re</independentVar>
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<tableData>
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3372885 -2.3531
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3710173 -0.2005
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5059327 -0.0891
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6689612 -0.0510
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</tableData>
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</table>
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</product>
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</function>
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@ -751,7 +622,7 @@
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<property>metrics/bw-ft</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>-0.15</value>
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<value> -0.0474 </value>
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</product>
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</function>
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@ -762,7 +633,7 @@
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>fcs/rudder-pos-rad</property>
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<value>-0.1</value>
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<value> -0.0387 </value>
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</product>
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</function>
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@ -773,14 +644,13 @@
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<property>metrics/Sw-sqft</property>
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<property>metrics/bw-ft</property>
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<property>fcs/left-aileron-pos-rad</property>
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<value>-0.003</value>
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<value> -0.0100 </value>
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</product>
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</function>
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</axis>
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</aerodynamics>
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<external_reactions>
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</external_reactions>
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Meir Michanie
8 years ago