[Jsbsim-cvslogs] CVS: JSBSim/aircraft/paraglider paraglider.xml, 1.10, 1.11

[Erik H. <eh...@us...>]

Update of /cvsroot/jsbsim/JSBSim/aircraft/paraglider
In directory sfp-cvs-1.v30.ch3.sourceforge.com:/tmp/cvs-serv13019

Modified Files:
	paraglider.xml 
Log Message:
Update the paraglider to a true ram-air parachute FDM with a pilot at an offset and an added small piston egnine for propulsion

Index: paraglider.xml
===================================================================
RCS file: /cvsroot/jsbsim/JSBSim/aircraft/paraglider/paraglider.xml,v
retrieving revision 1.10
retrieving revision 1.11
diff -C2 -r1.10 -r1.11
*** paraglider.xml	22 Dec 2012 15:22:22 -0000	1.10
--- paraglider.xml	18 May 2016 12:24:16 -0000	1.11
***************
*** 2,276 ****
  <?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
  <fdm_config name="paraglider" version="2.0" release="BETA"
!     xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
!     xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
  
!     <fileheader>
!         <author> Unknown </author>
!         <filecreationdate> 2001-01-01 </filecreationdate>
!         <version> $Revision$ </version>
!         <description> Paraglider </description>
!         <note>
!         This model was created using publicly available data, publicly available
!         technical reports, textbooks, and guesses. It contains no proprietary or
!         restricted data. If this model has been validated at all, it would be
!         only to the extent that it seems to "fly right", and that it possibly
!         complies with published, publicly known, performance data (maximum speed,
!         endurance, etc.). Thus, this model is meant for educational and entertainment
!         purposes only.
! 
!         This simulation model is not endorsed by the manufacturer. This model is not
!         to be sold.
!         </note>
!     </fileheader>
! 
!     <metrics>
!         <wingarea unit="FT2"> 160 </wingarea>
!         <wingspan unit="FT"> 20 </wingspan>
!         <chord unit="FT"> 8 </chord>
!         <htailarea unit="FT2"> 1 </htailarea>
!         <htailarm unit="FT"> 1 </htailarm>
!         <vtailarea unit="FT2"> 1 </vtailarea>
!         <vtailarm unit="FT"> 0 </vtailarm>
!         <location name="AERORP" unit="IN">
!             <x> 48 </x>
!             <y> 0 </y>
!             <z> 0 </z>
!         </location>
!         <location name="EYEPOINT" unit="IN">
!             <x> 48 </x>
!             <y> 0 </y>
!             <z> -120 </z>
!         </location>
!         <location name="VRP" unit="IN">
!             <x> 0 </x>
!             <y> 0 </y>
!             <z> 0 </z>
!         </location>
!     </metrics>
! 
!     <mass_balance>
!         <ixx unit="SLUG*FT2"> 2000 </ixx>
!         <iyy unit="SLUG*FT2"> 2000 </iyy>
!         <izz unit="SLUG*FT2"> 100 </izz>
!         <emptywt unit="LBS"> 200 </emptywt>
!         <location name="CG" unit="IN">
!             <x> 48 </x>
!             <y> 0 </y>
!             <z> -144 </z>
!         </location>
!     </mass_balance>
! 
!     <ground_reactions>
!         <contact type="BOGEY" name="LMLG">
!             <location unit="IN">
!                 <x> 48 </x>
!                 <y> -10 </y>
!                 <z> -180 </z>
!             </location>
!             <static_friction> 0.8 </static_friction>
!             <dynamic_friction> 0.5 </dynamic_friction>
!             <rolling_friction> 0.5 </rolling_friction>
!             <spring_coeff unit="LBS/FT"> 200 </spring_coeff>
!             <damping_coeff unit="LBS/FT/SEC"> 50 </damping_coeff>
!             <max_steer unit="DEG"> 0.0 </max_steer>
!             <brake_group> NONE </brake_group>
!             <retractable>0</retractable>
!         </contact>
!         <contact type="BOGEY" name="RMLG">
!             <location unit="IN">
!                 <x> 48 </x>
!                 <y> 10 </y>
!                 <z> -180 </z>
!             </location>
!             <static_friction> 0.8 </static_friction>
!             <dynamic_friction> 0.5 </dynamic_friction>
!             <rolling_friction> 0.5 </rolling_friction>
!             <spring_coeff unit="LBS/FT"> 200 </spring_coeff>
!             <damping_coeff unit="LBS/FT/SEC"> 50 </damping_coeff>
!             <max_steer unit="DEG"> 0.0 </max_steer>
!             <brake_group> NONE </brake_group>
!             <retractable>0</retractable>
!         </contact>
!         <contact type="BOGEY" name="NOSE_LG">
!             <location unit="IN">
!                 <x> 30 </x>
!                 <y> 0 </y>
!                 <z> -180 </z>
!             </location>
!             <static_friction> 0.8 </static_friction>
!             <dynamic_friction> 0.5 </dynamic_friction>
!             <rolling_friction> 0.5 </rolling_friction>
!             <spring_coeff unit="LBS/FT"> 200 </spring_coeff>
!             <damping_coeff unit="LBS/FT/SEC"> 50 </damping_coeff>
!             <max_steer unit="DEG"> 80 </max_steer>
!             <brake_group> NONE </brake_group>
!             <retractable>0</retractable>
!         </contact>
!     </ground_reactions>
!     <propulsion>
!     </propulsion>
!     <flight_control name="FCS: paraglider_FCS">
!         <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>
!                 <gain>0.018</gain>
!                 <range>
!                     <min>-25</min>
!                     <max>35</max>
!                 </range>
!                 <output>fcs/elevator-pos-rad</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>
!                 <gain>0.02</gain>
!                 <range>
!                     <min>-20</min>
!                     <max>15</max>
!                 </range>
!                 <output>fcs/left-aileron-pos-rad</output>
!             </aerosurface_scale>
! 
!             <aerosurface_scale name="Right Aileron Control">
!                 <input>-fcs/roll-trim-sum</input>
!                 <gain>0.02</gain>
!                 <range>
!                     <min>-20</min>
!                     <max>15</max>
!                 </range>
!                 <output>fcs/right-aileron-pos-rad</output>
!             </aerosurface_scale>
!         </channel>
!     </flight_control>
!     <aerodynamics>
! 
!         <axis name="DRAG">
!             <function name="aero/coefficient/CD0">
!                 <description>Drag_at_zero_lift</description>
!                 <product>
!                     <property>aero/qbar-psf</property>
!                     <property>metrics/Sw-sqft</property>
!                     <value>0.05</value>
!                 </product>
!             </function>
!             <function name="aero/coefficient/CDalpha">
!                 <description>Drag_due_to_alpha</description>
!                 <product>
!                     <property>aero/qbar-psf</property>
!                     <property>metrics/Sw-sqft</property>
!                     <property>aero/alpha-rad</property>
!                     <value>0.5</value>
!                 </product>
!             </function>
!             <function name="aero/coefficient/CDde">
!                 <description>Drag_due_to_Elevator_Deflection</description>
!                 <product>
!                     <property>aero/qbar-psf</property>
!                     <property>metrics/Sw-sqft</property>
!                     <property>fcs/elevator-pos-norm</property>
!                     <value>0.03</value>
!                 </product>
!             </function>
!         </axis>
! 
!         <axis name="LIFT">
!             <function name="aero/coefficient/CLalpha">
!                 <description>Lift_due_to_alpha</description>
!                 <product>
!                     <property>aero/qbar-psf</property>
!                     <property>metrics/Sw-sqft</property>
!                     <property>aero/alpha-rad</property>
!                     <value>10</value>
!                 </product>
!             </function>
!         </axis>
! 
!         <axis name="ROLL">
!             <function name="aero/coefficient/Clt">
!                 <description>Roll_moment_due_to_roll_angle</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>-5</value>
!                 </product>
!             </function>
!             <function name="aero/coefficient/Clp">
!                 <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>-3</value>
!                 </product>
!             </function>
!             <function name="aero/coefficient/Clda">
!                 <description>Roll_moment_due_to_aileron</description>
!                 <product>
!                     <property>aero/qbar-psf</property>
!                     <property>metrics/Sw-sqft</property>
!                     <property>metrics/bw-ft</property>
!                     <property>fcs/left-aileron-pos-rad</property>
!                     <value>0.2</value>
!                 </product>
!             </function>
!         </axis>
! 
!         <axis name="PITCH">
!             <function name="aero/coefficient/Cmalpha">
!                 <description>Pitch_moment_due_to_alpha</description>
!                 <product>
!                     <property>aero/qbar-psf</property>
!                     <property>metrics/Sw-sqft</property>
!                     <property>metrics/cbarw-ft</property>
!                     <property>aero/alpha-rad</property>
!                     <value>-3</value>
!                 </product>
!             </function>
!             <function name="aero/coefficient/Cmde">
!                 <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>
!                     <value>-2</value>
!                 </product>
!             </function>
!             <function name="aero/coefficient/Cmq">
!                 <description>Pitch_moment_due_to_pitch_rate</description>
!                 <product>
!                     <property>aero/qbar-psf</property>
!                     <property>metrics/Sw-sqft</property>
!                     <property>metrics/cbarw-ft</property>
!                     <property>aero/ci2vel</property>
!                     <property>velocities/q-aero-rad_sec</property>
!                     <value>-30</value>
!                 </product>
!             </function>
!         </axis>
!     </aerodynamics>
  </fdm_config>
--- 2,634 ----
  <?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
  <fdm_config name="paraglider" version="2.0" release="BETA"
!   xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
!   xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
  
!   <fileheader>
!     <author> David Culp, Erik Hofman </author>
!     <filecreationdate> 2001-01-01 </filecreationdate>
!     <version> 2.1 </version>
!     <description> (Powered) Paraglider </description>
! <!--
!     Reference:
!     CFD Calculation of Stability and Control Derivatives
!     For Ram-Air Parachutes
! 
!     http://www.cobaltcfd.com/pdfs/2016/AIAA-2016-1536.pdf
! -->
!   </fileheader>
! 
!   <metrics>
!     <wingarea unit="FT2"> 300 </wingarea>
!     <wingspan unit="FT"> 32 </wingspan>
!     <chord unit="FT"> 7 </chord>
!     <htailarea unit="FT2"> 0 </htailarea>
!     <htailarm unit="FT"> 0 </htailarm>
!     <vtailarea unit="FT2"> 0 </vtailarea>
!     <vtailarm unit="FT"> 0 </vtailarm>
!     <location name="AERORP" unit="IN">
!       <x> 0 </x>
!       <y> 0 </y>
!       <z> 0 </z>
!     </location>
!     <location name="EYEPOINT" unit="IN">
!       <x> 0 </x>
!       <y> 0 </y>
!       <z> -330 </z>
!     </location>
!     <location name="VRP" unit="IN">
!       <x> 0 </x>
!       <y> 0 </y>
!       <z> -330 </z>
!     </location>
!   </metrics>
! 
!   <mass_balance>
!   <ixx unit="SLUG*FT2">1.703</ixx>
!   <iyy unit="SLUG*FT2">1.898</iyy>
!   <izz unit="SLUG*FT2">1.360</izz>
!   <emptywt unit="LBS"> 10</emptywt>
!     <location name="CG" unit="IN">
!       <x> 0 </x>
!       <y> 0 </y>
!       <z> 0 </z>
!     </location>
!     <pointmass name="Pilot">
!       <weight unit="LBS"> 180 </weight>
!       <location name="POINTMASS" unit="IN">
!         <x>  0 </x>
!         <y>  0 </y>
!         <z> -330 </z>
!       </location>
!     </pointmass>
!     <pointmass name="Polini Engine">
!       <weight unit="LBS"> 25.13 </weight>
!       <location name="POINTMASS" unit="IN">
!         <x>  4 </x>
!         <y>  0 </y>
!         <z> -330 </z>
!       </location>
!     </pointmass>
!     <pointmass name="DT Propeller">
!       <weight unit="LBS"> 25.13 </weight>
!       <location name="POINTMASS" unit="IN">
!         <x> 10 </x>
!         <y>  0 </y>
!         <z> -330 </z>
!       </location>
!     </pointmass>
!   </mass_balance>
! 
!   <ground_reactions>
!     <contact type="BOGEY" name="LMLG">
!       <location unit="IN">
!         <x> 0 </x>
!         <y> -10 </y>
!         <z> -180 </z>
!       </location>
!       <static_friction> 0.8 </static_friction>
!       <dynamic_friction> 0.5 </dynamic_friction>
!       <rolling_friction> 0.5 </rolling_friction>
!       <spring_coeff unit="LBS/FT"> 200 </spring_coeff>
!       <damping_coeff unit="LBS/FT/SEC"> 50 </damping_coeff>
!       <max_steer unit="DEG"> 0.0 </max_steer>
!       <brake_group> NONE </brake_group>
!       <retractable>0</retractable>
!     </contact>
!     <contact type="BOGEY" name="RMLG">
!       <location unit="IN">
!         <x> 0 </x>
!         <y> 10 </y>
!         <z> -180 </z>
!       </location>
!       <static_friction> 0.8 </static_friction>
!       <dynamic_friction> 0.5 </dynamic_friction>
!       <rolling_friction> 0.5 </rolling_friction>
!       <spring_coeff unit="LBS/FT"> 200 </spring_coeff>
!       <damping_coeff unit="LBS/FT/SEC"> 50 </damping_coeff>
!       <max_steer unit="DEG"> 0.0 </max_steer>
!       <brake_group> NONE </brake_group>
!       <retractable>0</retractable>
!     </contact>
!   </ground_reactions>
! 
!   <system file="Controls.xml"/>
! 
!   <propulsion>
!     <engine file="Polini_THOR80">
!     <location unit="IN">
!       <x>     4.00 </x>
!       <y>     0.00 </y>
!       <z>  -330.00 </z>
!     </location>
!     <orient unit="DEG">
!       <pitch>     0.00 </pitch>
!        <roll>     0.00 </roll>
!         <yaw>     0.00 </yaw>
!     </orient>
!     <feed> 0 </feed>
! 
!     <thruster file="DT_Propeller">
!      <sense> 1 </sense>
!      <location unit="IN">
!        <x>    10.00 </x>
!        <y>     0.00 </y>
!        <z>  -330.00 </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>     8.00 </x>
!        <y>     0.00 </y>
!        <z>  -250.00 </z>
!      </location>
!      <capacity unit="LBS"> 3.5 </capacity>
!      <contents unit="LBS"> 1.0 </contents>
!   </tank>
!   </propulsion>
! 
!   <flight_control name="FCS: paraglider_FCS">
!   </flight_control>
! 
!   <aerodynamics>
! 
!     <!--
!       Drag of a spehere: 	0.5
!        Re	CD(rough)	CD(clean)
!        10^2	1.2		1.2
!        10^3	0.5		0.5
!        10^4	0.5		0.5
!        10^5	0.2		0.5
!        50^5			0.1
!        10^6	0.4		0.35
!        10^7	0.5 		0.48
!     -->
!     <!-- Pilot area (area of a circle with a diameter of 1.25 meter) -->
!     <property type="float" value="13.2">metrics/Sp-sqft</property>
! 
!     <!-- Pilot arm (-330 inches equals to 27.5 foot -->
!     <property type="float" value="27.5">metrics/bp-ft</property>
! 
!     <axis name="DRAG">
!      <function name="aero/coefficient/CDalpha">
!       <description>Drag_due_to_alpha</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <table>
!         <independentVar lookup="row">aero/alpha-deg</independentVar>
!         <independentVar lookup="column">fcs/elevator-pos-norm</independentVar>
!         <tableData>
!                   0.0     2.0
!             0.0   0.065   0.144
!             2.5   0.065   0.168
!             5.0   0.085   0.206
!             7.5   0.109   0.236
!             9.0   0.137   0.322
!            11.0   0.160   0.386
!            12.5   0.199   0.434
!            15.0   0.237   0.578
!            17.5   0.328   0.706
!            19.0   0.339   0.786
!            20.0   0.358   0.866
!         </tableData>
!        </table>
!       </product>
!      </function>
!      <function name="aero/coefficient/CDpilot">
!       <description>Drag_due_to_pilot</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sp-sqft</property>
!        <value>0.5</value>
!       </product>
!      </function>
!     </axis>
! 
!     <axis name="SIDE">
!      <function name="aero/coefficient/CYDa">
!       <description>Side_force_due_to_aileron</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <table>
!         <independentVar lookup="row">aero/alpha-deg</independentVar>
!         <independentVar lookup="column">fcs/aileron-pos-norm</independentVar>
!         <tableData>
!                  -1.0     0.0     1.0
!             0.0   0.004   0.000  -0.004
!             2.5   0.005   0.000  -0.005
!             5.0   0.006   0.000  -0.006
!             7.5   0.007   0.000  -0.007
!             9.0   0.008  -0.000  -0.008
!            11.0   0.003  -0.001  -0.003
!            12.5   0.002  -0.002  -0.002
!            15.0  -0.006   0.002   0.006
!            17.5   0.001  -0.001  -0.001
!            19.0  -0.009  -0.002   0.009
!            20.0  -0.004  -0.002   0.004
!         </tableData>
!        </table>
!       </product>
!      </function>
!      <function name="aero/coefficient/CYb">
!       <description>Side_force_due_to_beta</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <property>aero/beta-rad</property>
!        <table>
!         <independentVar>aero/alpha-deg</independentVar>
!         <tableData>
!            0   -0.053
!            2   -0.035
!            4   -0.020
!            6   -0.039
!            8   -0.072
!           10   -0.056
!         </tableData>
!        </table>
!       </product>
!      </function>
!      <function name="aero/coefficient/CYpilot">
!       <description>Side_force_due_to_pilot</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sp-sqft</property>
!        <property>aero/beta-rad</property>
!        <value>-0.5</value>
!       </product>
!      </function>
!      <function name="aero/coefficient/CYp">
!       <description>Side_force_due_to_roll_rate</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <property>aero/bi2vel</property>
!        <property>velocities/p-aero-rad_sec</property>
!        <table>
!         <independentVar>aero/alpha-deg</independentVar>
!         <tableData>
!            0   -0.040
!            2   -0.061
!            4   -0.086
!            6   -0.150
!            8   -0.193
!           10   -0.179
!         </tableData>
!        </table>
!       </product>
!      </function>
!     </axis>
! 
!     <axis name="LIFT">
!      <function name="aero/coefficient/CLalpha">
!       <description>Lift_due_to_alpha</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <table>
!         <independentVar lookup="row">aero/alpha-deg</independentVar>
!         <independentVar lookup="column">fcs/elevator-pos-norm</independentVar>
!         <tableData>
!                   0.0     2.0
!             0.0   0.275   0.642
!             2.5   0.395   0.924
!             5.0   0.495   1.166
!             7.5   0.609   1.410
!             9.0   0.628   1.546
!            11.0   0.628   1.546
!            12.5   0.649   1.450
!            15.0   0.614   1.636
!            17.5   0.789   1.726
!            19.0   0.669   1.902
!            20.0   0.705   2.026
!         </tableData>
!        </table>
!       </product>
!      </function>
!      <function name="aero/force/CLadot">
!       <description>Lift_due_to_alpha_rate</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <property>aero/ci2vel</property>
!        <property>aero/alphadot-rad_sec</property>
!        <table>
!         <independentVar>aero/alpha-deg</independentVar>
!         <tableData>
!            0.0   8.1
!            2.0  11.1
!            4.0   1.2
!            6.0   0.5
!            8.0   2.4
!           10.0  10.1
!         </tableData>
!        </table>
!       </product>
!      </function>
!      <function name="aero/force/CLq">
!       <description>Lift_due_to_pitch_rate</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <property>aero/ci2vel</property>
!        <property>velocities/q-aero-rad_sec</property>
!        <table>
!         <independentVar>aero/alpha-deg</independentVar>
!         <tableData>
!            0.0  11.9
!            2.0  13.6
!            4.0   0.8
!            6.0   0.9
!            8.0   2.4
!           10.0  14.9
!         </tableData>
!        </table>
!       </product>
!      </function>
!     </axis>
! 
!     <axis name="ROLL">
!      <function name="aero/coefficient/ClDa">
!       <description>Roll_moment_due_to_aileron</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <property>metrics/bw-ft</property>
!        <table>
!         <independentVar lookup="row">aero/alpha-deg</independentVar>
!         <independentVar lookup="column">fcs/aileron-pos-norm</independentVar>
!         <tableData>
!                  -1.0     0.0     1.0
!             0.0  -0.018   0.000   0.018
!             2.5  -0.020   0.000   0.020
!             5.0  -0.021   0.000   0.021
!             7.5  -0.022   0.000   0.022
!             9.0  -0.021   0.002   0.021
!            11.0  -0.004   0.002   0.004
!            12.5   0.003  -0.003  -0.003
!            15.0  -0.008  -0.008   0.008
!            17.5  -0.015   0.012   0.015
!            19.0  -0.004   0.008   0.004
!            20.0   0.000   0.018   0.000
!         </tableData>
!        </table>
!       </product>
!      </function>
!      <function name="aero/moment/Clb">
!       <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>aero/alpha-deg</independentVar>
!         <tableData>
!           0  -0.080
!           2  -0.051
!           4  -0.088
!           6  -0.107
!           8  -0.133 
!          10  -0.152
!         </tableData>
!        </table>
!       </product>
!      </function>
!      <function name="aero/moment/Clpilot">
!       <description>Roll moment due to pilot</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sp-sqft</property>
!        <property>metrics/bp-ft</property>
!        <property>aero/beta-rad</property>
!        <value>-0.5</value>
!       </product>
!      </function>
!      <function name="aero/coefficient/Clp">
!       <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>
!        <table>
!         <independentVar>aero/alpha-deg</independentVar>
!         <tableData>
!           0  -0.320
!           2  -0.348
!           4  -0.200
!           6  -0.358
!           8  -0.393
!          10  -0.367
!         </tableData>
!        </table>
!       </product>
!      </function>
!      <function name="aero/moment/Clr">
!       <description>Roll moment due to yaw rate</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <property>metrics/bw-ft</property>
!        <property>aero/bi2vel</property>
!        <property>velocities/r-aero-rad_sec</property>
!        <table>
!         <independentVar>aero/alpha-deg</independentVar>
!         <tableData>
!           0  -0.050
!           2   0.110
!           4   0.077
!           6   0.080
!           8   0.061
!          10   0.039
!         </tableData>
!        </table>
!       </product>
!      </function>
!     </axis>
! 
!     <axis name="PITCH">
!      <function name="aero/coefficient/CmDe">
!       <description>Pitch_moment_due_to_elevator</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <property>metrics/cbarw-ft</property>
!        <table>
!         <independentVar lookup="row">aero/alpha-deg</independentVar>
!         <independentVar lookup="column">fcs/elevator-pos-norm</independentVar>
!         <tableData>
!                   0.0     2.0
!             0.0   0.000  -0.046
!             2.5  -0.006  -0.062
!             5.0  -0.007  -0.084
!             7.5  -0.008  -0.084
!             9.0  -0.056  -0.176
!            11.0  -0.070  -0.196
!            12.5  -0.082  -0.242
!            15.0  -0.104  -0.242
!            17.5  -0.113  -0.296
!            19.0  -0.119  -0.284
!            20.0  -0.115  -0.296
!         </tableData>
!        </table>
!       </product>
!      </function>
!      <function name="aero/coefficient/Cmpilot">
!       <description>Pitch_moment_due_to_pilot</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sp-sqft</property>
!        <property>metrics/bp-ft</property>
!        <value>-0.5</value>
!        </product>
!      </function>
!      <function name="aero/moment/Cmadot">
!       <description>Pitch moment due to alpha rate</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <property>metrics/cbarw-ft</property>
!        <property>aero/ci2vel</property>
!        <property>aero/alphadot-rad_sec</property>
!        <table>
!         <independentVar>aero/alpha-deg</independentVar>
!         <tableData>
!            0.0  -2.5
!            2.0  -0.5
!            4.0   2.8
!            6.0   0.1
!            8.0  -0.4
!           10.0   0.0
!         </tableData>
!        </table>
!       </product>
!      </function>
!      <function name="aero/moment/Cmq">
!       <description>Pitch moment due to pitch rate</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <property>metrics/cbarw-ft</property>
!        <property>aero/ci2vel</property>
!        <property>velocities/q-aero-rad_sec</property>
!        <value>-30</value>
! <!--
!        <table>
!         <independentVar>aero/alpha-deg</independentVar>
!         <tableData>
!            0.0  -1.9
!            2.0   0.5
!            4.0   0.0
!            6.0   2.9
!            8.0  -0.5
!           10.0   0.5
!         </tableData>
!        </table>
! -->
!       </product>
!      </function>
!     </axis>
! 
!     <axis name="YAW">
!      <function name="aero/coefficient/CnDa">
!       <description>Yaw_moment_due_to_aileron</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <property>metrics/bw-ft</property>
!        <table>
!         <independentVar lookup="row">aero/alpha-deg</independentVar>
!         <independentVar lookup="column">fcs/aileron-pos-norm</independentVar>
!         <tableData>
!                  -1.0     0.0     1.0
!             0.0   0.007   0.001  -0.007
!             2.5   0.007  -0.001  -0.007
!             5.0   0.007   0.001  -0.007
!             7.5   0.010  -0.001  -0.010
!             9.0   0.010   0.001  -0.010
!            11.0   0.012   0.002  -0.012
!            12.5   0.016   0.000  -0.016
!            15.0   0.016   0.000  -0.016
!            17.5   0.007  -0.001  -0.007
!            19.0   0.011   0.001  -0.011
!            20.0   0.014   0.001  -0.014
!         </tableData>
!        </table>
!       </product>
!      </function>
!      <function name="aero/moment/Cnb">
!       <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>
!        <table>
!         <independentVar>aero/alpha-deg</independentVar>
!         <tableData>
!           0   0.0009
!           2  -0.0176
!           4  -0.0040
!           6   0.0000
!           8   0.0224
!          10   0.0176
!         </tableData>
!        </table>
!       </product>
!      </function>
!      <function name="aero/moment/Cnp">
!       <description>Yaw_moment_due_to_roll_rate</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <property>metrics/bw-ft</property>
!        <property>aero/bi2vel</property>
!        <property>velocities/p-aero-rad_sec</property>
!        <table>
!         <independentVar>aero/alpha-deg</independentVar>
!         <tableData>
!           0  -0.320
!           2  -0.348
!           4  -0.200
!           6  -0.358
!           8  -0.393
!          10  -0.367
!         </tableData>
!        </table>
!       </product>
!      </function>
!      <function name="aero/moment/Cnr">
!       <description>Yaw moment due to yaw rate</description>
!       <product>
!        <property>aero/qbar-psf</property>
!        <property>metrics/Sw-sqft</property>
!        <property>metrics/bw-ft</property>
!        <property>aero/bi2vel</property>
!        <property>velocities/r-aero-rad_sec</property>
!        <table>
!         <independentVar>aero/alpha-deg</independentVar>
!         <tableData>
!           0  -0.070
!           2  -0.112
!           4  -0.156
!           6  -0.036
!           8  -0.072
!          10  -0.072
!         </tableData>
!        </table>
!       </product>
!      </function>
!     </axis>
!   </aerodynamics>
  </fdm_config>