843 lines
23 KiB
XML
843 lines
23 KiB
XML
|
<?xml version="1.0"?>
|
||
|
|
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
|
||
|
|
<fdm_config name="MQ-9 Reaper" version="2.0" release="ALPHA"
|
||
|
|
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
|
||
|
|
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
|
||
|
|
|
||
|
|
<fileheader>
|
||
|
|
<author> Petar Jedvaj </author>
|
||
|
|
<filecreationdate>2016-06-29</filecreationdate>
|
||
|
|
<version>$Revision: 1.15 $</version>
|
||
|
|
<description> General Atomics MQ-9 Reaper. </description>
|
||
|
|
</fileheader>
|
||
|
|
|
||
|
|
<!--
|
||
|
|
File: MQ-9 Reaper.xml
|
||
|
|
Inputs:
|
||
|
|
name: MQ-9 Reaper
|
||
|
|
type: WWII fighter, subsonic sport, aerobatic
|
||
|
|
max weight: 10495.8 lb
|
||
|
|
wing span: 65.62 ft
|
||
|
|
length: 36.091 ft
|
||
|
|
wing area: 257.2825679 sq-ft
|
||
|
|
gear type: tricycle
|
||
|
|
retractable?: yes
|
||
|
|
# engines: 1
|
||
|
|
engine type: turboprop
|
||
|
|
engine layout: aft fuselage
|
||
|
|
yaw damper? yes
|
||
|
|
Outputs:
|
||
|
|
wing loading: 40.79 lb/sq-ft
|
||
|
|
payload: 4313.6 lbs
|
||
|
|
CL-alpha: 4.5 per radian
|
||
|
|
CL-0: 0.17
|
||
|
|
CL-max: 1.2
|
||
|
|
CD-0: 0.02
|
||
|
|
K: 0.06
|
||
|
|
-->
|
||
|
|
|
||
|
|
<metrics>
|
||
|
|
<wingarea unit="FT2"> 257.28 </wingarea>
|
||
|
|
<wingspan unit="FT" > 65.62 </wingspan>
|
||
|
|
<wing_incidence> 2.00 </wing_incidence>
|
||
|
|
<chord unit="FT" > 3.92 </chord>
|
||
|
|
<htailarea unit="FT2"> 32.29 </htailarea>
|
||
|
|
<htailarm unit="FT" > 21.65 </htailarm>
|
||
|
|
<vtailarea unit="FT2"> 10.76 </vtailarea>
|
||
|
|
<vtailarm unit="FT" > 21.65 </vtailarm>
|
||
|
|
<location name="AERORP" unit="IN">
|
||
|
|
<x> 173.24 </x>
|
||
|
|
<y> 0.00 </y>
|
||
|
|
<z> 0.00 </z>
|
||
|
|
</location>
|
||
|
|
<location name="EYEPOINT" unit="IN">
|
||
|
|
<x> 121.27 </x>
|
||
|
|
<y> 0.00 </y>
|
||
|
|
<z> 40.00 </z>
|
||
|
|
</location>
|
||
|
|
<location name="VRP" unit="IN">
|
||
|
|
<x>0</x>
|
||
|
|
<y>0</y>
|
||
|
|
<z>0</z>
|
||
|
|
</location>
|
||
|
|
</metrics>
|
||
|
|
|
||
|
|
<mass_balance>
|
||
|
|
<ixx unit="SLUG*FT2"> 11946 </ixx>
|
||
|
|
<iyy unit="SLUG*FT2"> 6424 </iyy>
|
||
|
|
<izz unit="SLUG*FT2"> 17362 </izz>
|
||
|
|
<emptywt unit="LBS" > 4902 </emptywt>
|
||
|
|
<location name="CG" unit="IN">
|
||
|
|
<x> 173.24 </x>
|
||
|
|
<y> 0.00 </y>
|
||
|
|
<z> -10.83 </z>
|
||
|
|
</location>
|
||
|
|
<pointmass name="Payload">
|
||
|
|
<description> 4314 LBS + full (1280 LBS) fuel should bring model up to entered max weight</description>
|
||
|
|
<weight unit="LBS"> 2156.8 </weight>
|
||
|
|
<location name="POINTMASS" unit="IN">
|
||
|
|
<x> 173.24 </x>
|
||
|
|
<y> 0.00 </y>
|
||
|
|
<z> -10.83 </z>
|
||
|
|
</location>
|
||
|
|
</pointmass>
|
||
|
|
|
||
|
|
<pointmass name="station1">
|
||
|
|
<weight unit="LBS"> 100 </weight>
|
||
|
|
<location name="POINTMASS" unit="IN">
|
||
|
|
<x> 173 </x>
|
||
|
|
<y> -89 </y>
|
||
|
|
<z> -3 </z>
|
||
|
|
</location>
|
||
|
|
</pointmass>
|
||
|
|
|
||
|
|
<pointmass name="station2">
|
||
|
|
<weight unit="LBS"> 100 </weight>
|
||
|
|
<location name="POINTMASS" unit="IN">
|
||
|
|
<x> 173 </x>
|
||
|
|
<y> -74 </y>
|
||
|
|
<z> -3 </z>
|
||
|
|
</location>
|
||
|
|
</pointmass>
|
||
|
|
|
||
|
|
<pointmass name="station3">
|
||
|
|
<weight unit="LBS"> 510 </weight>
|
||
|
|
<location name="POINTMASS" unit="IN">
|
||
|
|
<x> 173 </x>
|
||
|
|
<y> -48 </y>
|
||
|
|
<z> -3 </z>
|
||
|
|
</location>
|
||
|
|
</pointmass>
|
||
|
|
|
||
|
|
<pointmass name="station4">
|
||
|
|
<weight unit="LBS"> 510 </weight>
|
||
|
|
<location name="POINTMASS" unit="IN">
|
||
|
|
<x> 173 </x>
|
||
|
|
<y> 48 </y>
|
||
|
|
<z> -3 </z>
|
||
|
|
</location>
|
||
|
|
</pointmass>
|
||
|
|
|
||
|
|
<pointmass name="station5">
|
||
|
|
<weight unit="LBS"> 100 </weight>
|
||
|
|
<location name="POINTMASS" unit="IN">
|
||
|
|
<x> 173 </x>
|
||
|
|
<y> 74 </y>
|
||
|
|
<z> -3 </z>
|
||
|
|
</location>
|
||
|
|
</pointmass>
|
||
|
|
|
||
|
|
<pointmass name="station6">
|
||
|
|
<weight unit="LBS"> 100 </weight>
|
||
|
|
<location name="POINTMASS" unit="IN">
|
||
|
|
<x> 173 </x>
|
||
|
|
<y> 89 </y>
|
||
|
|
<z> -3 </z>
|
||
|
|
</location>
|
||
|
|
</pointmass>
|
||
|
|
|
||
|
|
</mass_balance>
|
||
|
|
|
||
|
|
<ground_reactions>
|
||
|
|
|
||
|
|
<contact type="BOGEY" name="NOSE">
|
||
|
|
<location unit="IN">
|
||
|
|
<x> 56.30 </x>
|
||
|
|
<y> 0.00 </y>
|
||
|
|
<z> -51.97 </z>
|
||
|
|
</location>
|
||
|
|
<static_friction> 0.80 </static_friction>
|
||
|
|
<dynamic_friction> 0.50 </dynamic_friction>
|
||
|
|
<rolling_friction> 0.02 </rolling_friction>
|
||
|
|
<spring_coeff unit="LBS/FT"> 3148.74 </spring_coeff>
|
||
|
|
<damping_coeff unit="LBS/FT/SEC"> 5247.90 </damping_coeff>
|
||
|
|
<max_steer unit="DEG"> 5.00 </max_steer>
|
||
|
|
<brake_group>NONE</brake_group>
|
||
|
|
<retractable>1</retractable>
|
||
|
|
</contact>
|
||
|
|
|
||
|
|
<contact type="BOGEY" name="LEFT_MAIN">
|
||
|
|
<location unit="IN">
|
||
|
|
<x> 180.17 </x>
|
||
|
|
<y> -118.12 </y>
|
||
|
|
<z> -51.97 </z>
|
||
|
|
</location>
|
||
|
|
<static_friction> 0.80 </static_friction>
|
||
|
|
<dynamic_friction> 0.50 </dynamic_friction>
|
||
|
|
<rolling_friction> 0.02 </rolling_friction>
|
||
|
|
<spring_coeff unit="LBS/FT"> 10495.80 </spring_coeff>
|
||
|
|
<damping_coeff unit="LBS/FT/SEC"> 5247.90 </damping_coeff>
|
||
|
|
<max_steer unit="DEG">0</max_steer>
|
||
|
|
<brake_group>LEFT</brake_group>
|
||
|
|
<retractable>1</retractable>
|
||
|
|
</contact>
|
||
|
|
|
||
|
|
<contact type="BOGEY" name="RIGHT_MAIN">
|
||
|
|
<location unit="IN">
|
||
|
|
<x> 180.17 </x>
|
||
|
|
<y> 118.12 </y>
|
||
|
|
<z> -51.97 </z>
|
||
|
|
</location>
|
||
|
|
<static_friction> 0.80 </static_friction>
|
||
|
|
<dynamic_friction> 0.50 </dynamic_friction>
|
||
|
|
<rolling_friction> 0.02 </rolling_friction>
|
||
|
|
<spring_coeff unit="LBS/FT"> 10495.80 </spring_coeff>
|
||
|
|
<damping_coeff unit="LBS/FT/SEC"> 5247.90 </damping_coeff>
|
||
|
|
<max_steer unit="DEG">0</max_steer>
|
||
|
|
<brake_group>RIGHT</brake_group>
|
||
|
|
<retractable>1</retractable>
|
||
|
|
</contact>
|
||
|
|
|
||
|
|
<contact type="STRUCTURE" name="LEFT_WING">
|
||
|
|
<location unit="IN">
|
||
|
|
<x> 173.24 </x>
|
||
|
|
<y> -32.81 </y>
|
||
|
|
<z> -10.83 </z>
|
||
|
|
</location>
|
||
|
|
<static_friction> 1.00 </static_friction>
|
||
|
|
<dynamic_friction> 1.00 </dynamic_friction>
|
||
|
|
<spring_coeff unit="LBS/FT"> 10495.80 </spring_coeff>
|
||
|
|
<damping_coeff unit="LBS/FT/SEC"> 10495.80 </damping_coeff>
|
||
|
|
</contact>
|
||
|
|
|
||
|
|
<contact type="STRUCTURE" name="RIGHT_WING">
|
||
|
|
<location unit="IN">
|
||
|
|
<x> 173.24 </x>
|
||
|
|
<y> 32.81 </y>
|
||
|
|
<z> -10.83 </z>
|
||
|
|
</location>
|
||
|
|
<static_friction> 1.00 </static_friction>
|
||
|
|
<dynamic_friction> 1.00 </dynamic_friction>
|
||
|
|
<spring_coeff unit="LBS/FT"> 10495.80 </spring_coeff>
|
||
|
|
<damping_coeff unit="LBS/FT/SEC"> 10495.80 </damping_coeff>
|
||
|
|
</contact>
|
||
|
|
|
||
|
|
</ground_reactions>
|
||
|
|
|
||
|
|
<propulsion>
|
||
|
|
|
||
|
|
<engine file="TPE331-10">
|
||
|
|
<location unit="IN">
|
||
|
|
<x> 373.09 </x>
|
||
|
|
<y> 0.00 </y>
|
||
|
|
<z> 0.00 </z>
|
||
|
|
</location>
|
||
|
|
<orient unit="DEG">
|
||
|
|
<pitch> 0.00 </pitch>
|
||
|
|
<roll> 0.00 </roll>
|
||
|
|
<yaw> 0.00 </yaw>
|
||
|
|
</orient>
|
||
|
|
<feed>0</feed>
|
||
|
|
<thruster file="Direct">
|
||
|
|
<location unit="IN">
|
||
|
|
<x> 373.09 </x>
|
||
|
|
<y> 0.00 </y>
|
||
|
|
<z> 0.00 </z>
|
||
|
|
</location>
|
||
|
|
<orient unit="DEG">
|
||
|
|
<pitch> 0.00 </pitch>
|
||
|
|
<roll> 0.00 </roll>
|
||
|
|
<yaw> 0.00 </yaw>
|
||
|
|
</orient>
|
||
|
|
</thruster>
|
||
|
|
</engine>
|
||
|
|
|
||
|
|
<tank type="FUEL" number="0">
|
||
|
|
<location unit="IN">
|
||
|
|
<x> 173.24 </x>
|
||
|
|
<y> 0.00 </y>
|
||
|
|
<z> -10.83 </z>
|
||
|
|
</location>
|
||
|
|
<capacity unit="LBS"> 2000.00 </capacity>
|
||
|
|
<contents unit="LBS"> 1000.00 </contents>
|
||
|
|
</tank>
|
||
|
|
|
||
|
|
<tank type="FUEL" number="1">
|
||
|
|
<location unit="IN">
|
||
|
|
<x> 173.24 </x>
|
||
|
|
<y> 0.00 </y>
|
||
|
|
<z> -10.83 </z>
|
||
|
|
</location>
|
||
|
|
<capacity unit="LBS"> 2000.00 </capacity>
|
||
|
|
<contents unit="LBS"> 1000.00 </contents>
|
||
|
|
</tank>
|
||
|
|
|
||
|
|
</propulsion>
|
||
|
|
|
||
|
|
<system file="Armament"/>
|
||
|
|
<system file="Particles"/>
|
||
|
|
|
||
|
|
<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>
|
||
|
|
|
||
|
|
<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>
|