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fgdata/Aircraft/c172p/c172p.xml

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sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
<?xml version="1.0"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
<fdm_config name="c172" 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> 2002-01-01 </filecreationdate>
<version> $Id$ </version>
<description> Cessna C-172 </description>
</fileheader>
<metrics>
<wingarea unit="FT2"> 174 </wingarea>
<wingspan unit="FT"> 35.8 </wingspan>
<chord unit="FT"> 4.9 </chord>
<htailarea unit="FT2"> 21.9 </htailarea>
<htailarm unit="FT"> 15.7 </htailarm>
<vtailarea unit="FT2"> 16.5 </vtailarea>
<vtailarm unit="FT"> 0 </vtailarm>
<location name="AERORP" unit="IN">
<x> 43.2 </x>
<y> 0 </y>
<z> 59.4 </z>
</location>
<location name="EYEPOINT" unit="IN">
<x> 37 </x>
<y> 0 </y>
<z> 48 </z>
</location>
<location name="VRP" unit="IN">
<x> 42.6 </x>
<y> 0 </y>
<z> 38.5 </z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 948 </ixx>
<iyy unit="SLUG*FT2"> 1346 </iyy>
<izz unit="SLUG*FT2"> 1967 </izz>
<ixy unit="SLUG*FT2"> -0 </ixy>
<ixz unit="SLUG*FT2"> -0 </ixz>
<iyz unit="SLUG*FT2"> -0 </iyz>
<emptywt unit="LBS"> 1500 </emptywt>
<location name="CG" unit="IN">
<x> 41 </x>
<y> 0 </y>
<z> 36.5 </z>
</location>
Ron Jensen: This is a patch to the c172p fdm to add pointmasses for all four occupant positions and baggage.  The X locations were taken from the c172 type certificate 3A12 dated September 15, 1998.  As the new pointmasses have a weight of 0 they will not affect the current model, however we are extending the FlightGear weight and balance dialog for JSBSim and the pointmasses have to be defined.
2008-09-01 15:14:33 +00:00
<pointmass name="Pilot">
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
<weight unit="LBS"> 180 </weight>
<location name="POINTMASS" unit="IN">
<x> 36 </x>
<y> -14 </y>
<z> 24 </z>
</location>
</pointmass>
Remove some junk characters from the upper half of the ASCII table, and convert a few stray tabs to spaces. This is only a cleanup - no values are changed.
2009-10-17 15:04:44 +00:00
<pointmass name="Co-Pilot">
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="IN">
<x> 36 </x>
<y> 14 </y>
<z> 24 </z>
</location>
</pointmass>
<pointmass name="Left Passenger">
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="IN">
<x> 70 </x>
<y> -14 </y>
<z> 24 </z>
</location>
</pointmass>
<pointmass name="Right Passenger">
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="IN">
<x> 70 </x>
<y> 14 </y>
<z> 24 </z>
</location>
</pointmass>
<pointmass name="Baggage">
<weight unit="LBS"> 0 </weight>
<location name="POINTMASS" unit="IN">
<x> 95 </x>
<y> 0 </y>
<z> 24 </z>
</location>
</pointmass>
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
</mass_balance>
<ground_reactions>
<contact type="BOGEY" name="NOSE">
<location unit="IN">
<x> -6.8 </x>
<y> 0 </y>
Dave Perry: This patch adds main gear rotations about the fuselage attach points that keep the wheels in contact with the ground as the compression increases and decreases. I also rotated the main fairings and wheels 4 degrees so the wheel axles are horizontal sitting on the ground. The left and right main gear struts, wheels, and fairings were adjusted to be mirrored (symetric) in the c172p.ac. I also increased the rpm boundary between the Propeller and Propeller.slow selects.
2009-11-22 22:06:25 +00:00
<z> -19.5</z>
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
</location>
<static_friction> 0.8 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
Dave Perry: This patch adds main gear rotations about the fuselage attach points that keep the wheels in contact with the ground as the compression increases and decreases. I also rotated the main fairings and wheels 4 degrees so the wheel axles are horizontal sitting on the ground. The left and right main gear struts, wheels, and fairings were adjusted to be mirrored (symetric) in the c172p.ac. I also increased the rpm boundary between the Propeller and Propeller.slow selects.
2009-11-22 22:06:25 +00:00
<spring_coeff unit="LBS/FT"> 1800 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 600 </damping_coeff>
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
<max_steer unit="DEG"> 10 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="LEFT_MAIN">
<location unit="IN">
<x> 58.2 </x>
<y> -43 </y>
Dave Perry: This patch adds main gear rotations about the fuselage attach points that keep the wheels in contact with the ground as the compression increases and decreases. I also rotated the main fairings and wheels 4 degrees so the wheel axles are horizontal sitting on the ground. The left and right main gear struts, wheels, and fairings were adjusted to be mirrored (symetric) in the c172p.ac. I also increased the rpm boundary between the Propeller and Propeller.slow selects.
2009-11-22 22:06:25 +00:00
<z> -15.5 </z>
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
</location>
<static_friction> 0.8 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
Dave Perry: This patch adds main gear rotations about the fuselage attach points that keep the wheels in contact with the ground as the compression increases and decreases. I also rotated the main fairings and wheels 4 degrees so the wheel axles are horizontal sitting on the ground. The left and right main gear struts, wheels, and fairings were adjusted to be mirrored (symetric) in the c172p.ac. I also increased the rpm boundary between the Propeller and Propeller.slow selects.
2009-11-22 22:06:25 +00:00
<spring_coeff unit="LBS/FT"> 5400 </spring_coeff>
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
<damping_coeff unit="LBS/FT/SEC"> 1600 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> LEFT </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="RIGHT_MAIN">
<location unit="IN">
<x> 58.2 </x>
<y> 43 </y>
Dave Perry: This patch adds main gear rotations about the fuselage attach points that keep the wheels in contact with the ground as the compression increases and decreases. I also rotated the main fairings and wheels 4 degrees so the wheel axles are horizontal sitting on the ground. The left and right main gear struts, wheels, and fairings were adjusted to be mirrored (symetric) in the c172p.ac. I also increased the rpm boundary between the Propeller and Propeller.slow selects.
2009-11-22 22:06:25 +00:00
<z> -15.5 </z>
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
</location>
<static_friction> 0.8 </static_friction>
<dynamic_friction> 0.5 </dynamic_friction>
<rolling_friction> 0.02 </rolling_friction>
Dave Perry: This patch adds main gear rotations about the fuselage attach points that keep the wheels in contact with the ground as the compression increases and decreases. I also rotated the main fairings and wheels 4 degrees so the wheel axles are horizontal sitting on the ground. The left and right main gear struts, wheels, and fairings were adjusted to be mirrored (symetric) in the c172p.ac. I also increased the rpm boundary between the Propeller and Propeller.slow selects.
2009-11-22 22:06:25 +00:00
<spring_coeff unit="LBS/FT"> 5400 </spring_coeff>
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
<damping_coeff unit="LBS/FT/SEC"> 1600 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> RIGHT </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="TAIL_SKID">
<location unit="IN">
<x> 188 </x>
<y> 0 </y>
<z> 8 </z>
</location>
<static_friction> 0.2 </static_friction>
<dynamic_friction> 0.2 </dynamic_friction>
<rolling_friction> 0.2 </rolling_friction>
<spring_coeff unit="LBS/FT"> 20000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 1000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="LEFT_TIP">
<location unit="IN">
<x> 43.2 </x>
<y> -214.8 </y>
<z> 59.4 </z>
</location>
<static_friction> 0.2 </static_friction>
<dynamic_friction> 0.2 </dynamic_friction>
<rolling_friction> 0.2 </rolling_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="RIGHT_TIP">
<location unit="IN">
<x> 43.2 </x>
<y> 214.8 </y>
<z> 59.4 </z>
</location>
<static_friction> 0.2 </static_friction>
<dynamic_friction> 0.2 </dynamic_friction>
<rolling_friction> 0.2 </rolling_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 2000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
</ground_reactions>
<propulsion>
<engine file="eng_io320">
<location unit="IN">
<x> -19.7 </x>
<y> 0 </y>
<z> 26.6 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0 </pitch>
<yaw> 0 </yaw>
</orient>
<feed>0</feed>
<feed>1</feed>
<thruster file="prop_75in2f">
<location unit="IN">
<x> -37.7 </x>
<y> 0 </y>
<z> 26.6 </z>
</location>
<orient unit="DEG">
<roll> 0.0 </roll>
<pitch> 0.0 </pitch>
<yaw> 0.0 </yaw>
</orient>
<sense> 1 </sense>
<p_factor> 10 </p_factor>
</thruster>
</engine>
<tank type="FUEL"> <!-- Tank number 0 -->
<location unit="IN">
<x> 56 </x>
<y> -112 </y>
<z> 59.4 </z>
</location>
<capacity unit="LBS"> 185 </capacity>
<contents unit="LBS"> 100 </contents>
</tank>
<tank type="FUEL"> <!-- Tank number 1 -->
<location unit="IN">
<x> 56 </x>
<y> 112 </y>
<z> 59.4 </z>
</location>
<capacity unit="LBS"> 185 </capacity>
<contents unit="LBS"> 100 </contents>
</tank>
</propulsion>
<flight_control name="FCS: c172">
<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>0.01745</gain>
<range>
<min>-28</min>
<max>23</max>
</range>
<output>fcs/elevator-pos-rad</output>
</aerosurface_scale>
Jean-Yves Lefort: The attached patch restores normalized control surface positions on the c172p
2006-03-06 21:12:52 +00:00
<aerosurface_scale name="Elevator Position Normalized">
<input>fcs/elevator-pos-deg</input>
<domain>
Remove some junk characters from the upper half of the ASCII table, and convert a few stray tabs to spaces. This is only a cleanup - no values are changed.
2009-10-17 15:04:44 +00:00
<min>-28</min>
<max>23</max>
Jean-Yves Lefort: The attached patch restores normalized control surface positions on the c172p
2006-03-06 21:12:52 +00:00
</domain>
<range>
<min>-1</min>
<max>1</max>
</range>
<output>fcs/elevator-pos-norm</output>
</aerosurface_scale>
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
</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>0.01745</gain>
<range>
<min>-20</min>
<max>15</max>
</range>
<output>fcs/left-aileron-pos-rad</output>
</aerosurface_scale>
Jean-Yves Lefort: The attached patch restores normalized control surface positions on the c172p
2006-03-06 21:12:52 +00:00
<aerosurface_scale name="Left Aileron Position Normalized">
<input>fcs/left-aileron-pos-deg</input>
<domain>
Remove some junk characters from the upper half of the ASCII table, and convert a few stray tabs to spaces. This is only a cleanup - no values are changed.
2009-10-17 15:04:44 +00:00
<min>-20</min>
<max>15</max>
Jean-Yves Lefort: The attached patch restores normalized control surface positions on the c172p
2006-03-06 21:12:52 +00:00
</domain>
<range>
<min>-1</min>
<max>1</max>
</range>
<output>fcs/left-aileron-pos-norm</output>
</aerosurface_scale>
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
<aerosurface_scale name="Right Aileron Control">
<input>fcs/roll-trim-sum</input>
<gain>-0.01745</gain>
<range>
<min>-20</min>
<max>15</max>
</range>
<output>fcs/right-aileron-pos-rad</output>
</aerosurface_scale>
Jean-Yves Lefort: The attached patch restores normalized control surface positions on the c172p
2006-03-06 21:12:52 +00:00
<aerosurface_scale name="Right Aileron Position Normalized">
<input>fcs/right-aileron-pos-deg</input>
<domain>
Remove some junk characters from the upper half of the ASCII table, and convert a few stray tabs to spaces. This is only a cleanup - no values are changed.
2009-10-17 15:04:44 +00:00
<min>-15</min>
<max>20</max>
Jean-Yves Lefort: The attached patch restores normalized control surface positions on the c172p
2006-03-06 21:12:52 +00:00
</domain>
<range>
<min>1</min>
<max>-1</max>
</range>
<output>fcs/right-aileron-pos-norm</output>
</aerosurface_scale>
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
</channel>
<channel name="Yaw">
<summer name="Yaw Trim Sum">
<input>fcs/rudder-cmd-norm</input>
<input>fcs/yaw-trim-cmd-norm</input>
<clipto>
<min>-1</min>
<max>1</max>
</clipto>
</summer>
<aerosurface_scale name="Rudder Control">
<input>fcs/yaw-trim-sum</input>
<gain>0.01745</gain>
<range>
<min>-16</min>
<max>16</max>
</range>
<output>fcs/rudder-pos-rad</output>
</aerosurface_scale>
Jean-Yves Lefort: The attached patch restores normalized control surface positions on the c172p
2006-03-06 21:12:52 +00:00
<aerosurface_scale name="Rudder Position Normalized">
<input>fcs/rudder-pos-deg</input>
<domain>
Remove some junk characters from the upper half of the ASCII table, and convert a few stray tabs to spaces. This is only a cleanup - no values are changed.
2009-10-17 15:04:44 +00:00
<min>-16</min>
<max>16</max>
Jean-Yves Lefort: The attached patch restores normalized control surface positions on the c172p
2006-03-06 21:12:52 +00:00
</domain>
<range>
<min>-1</min>
<max>1</max>
</range>
<output>fcs/rudder-pos-norm</output>
</aerosurface_scale>
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
</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>10</position>
<time>2</time>
</setting>
<setting>
<position>20</position>
<time>1</time>
</setting>
<setting>
<position>30</position>
<time>1</time>
</setting>
</traverse>
<output>fcs/flap-pos-deg</output>
</kinematic>
Sync. w. JSBSim CVS.
2006-03-13 15:27:14 +00:00
<aerosurface_scale name="Flap Position Normalizer">
<input>fcs/flap-pos-deg</input>
<domain>
<min>0</min> <!-- Flaps actual minimum position -->
<max>30</max> <!-- Flaps actual maximum position -->
</domain>
<range>
<min>0</min> <!-- Flaps normalized minimum position -->
<max>1</max> <!-- Flaps normalized maximum position -->
</range>
<output>fcs/flap-pos-norm</output>
Jean-Yves Lefort: The attached patch restores normalized control surface positions on the c172p
2006-03-06 21:12:52 +00:00
</aerosurface_scale>
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
</channel>
</flight_control>
<aerodynamics>
Sync. with JSBSim CVS
2008-08-08 08:56:08 +00:00
<alphalimits unit="RAD">
<min>-0.087</min>
<max>0.28</max>
Sync. w. JSB CVS as of 15/01/2007
2007-01-15 12:50:44 +00:00
</alphalimits>
Sync. with JSBSim CVS
2008-08-08 08:56:08 +00:00
<hysteresis_limits unit="RAD">
<min>0.09</min>
<max>0.36</max>
Sync. w. JSB CVS as of 15/01/2007
2007-01-15 12:50:44 +00:00
</hysteresis_limits>
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
<function name="aero/function/kCDge">
<description>Change_in_drag_due_to_ground_effect</description>
<product>
<table>
<independentVar>aero/h_b-mac-ft</independentVar>
<tableData>
0.0000 0.0480
0.1000 0.5150
0.1500 0.6290
0.2000 0.7090
0.3000 0.8150
0.4000 0.8820
0.5000 0.9280
0.6000 0.9620
0.7000 0.9880
0.8000 1.0000
0.9000 1.0000
1.0000 1.0000
1.1000 1.0000
</tableData>
</table>
</product>
</function>
<function name="aero/function/kCLge">
<description>Change_in_lift_due_to_ground_effect</description>
<product>
<table>
<independentVar>aero/h_b-mac-ft</independentVar>
<tableData>
0.0000 1.2030
0.1000 1.1270
0.1500 1.0900
0.2000 1.0730
0.3000 1.0460
0.4000 1.0550
0.5000 1.0190
0.6000 1.0130
0.7000 1.0080
0.8000 1.0060
0.9000 1.0030
1.0000 1.0020
1.1000 1.0000
</tableData>
</table>
</product>
</function>
<axis name="DRAG">
<function name="aero/coefficient/CDo">
<description>Drag_at_zero_lift</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<value>0.027</value>
</product>
</function>
<function name="aero/coefficient/CDDf">
<description>Delta_drag_due_to_flap_deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCDge</property>
<table>
<independentVar>fcs/flap-pos-deg</independentVar>
<tableData>
0.0000 0.0000
10.0000 0.0070
20.0000 0.0120
30.0000 0.0180
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CDwbh">
<description>Drag_due_to_alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCDge</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
<tableData>
0.0000 10.0000 20.0000 30.0000
-0.0873 0.0041 0.0000 0.0005 0.0014
-0.0698 0.0013 0.0004 0.0025 0.0041
-0.0524 0.0001 0.0023 0.0059 0.0084
-0.0349 0.0003 0.0057 0.0108 0.0141
-0.0175 0.0020 0.0105 0.0172 0.0212
0.0000 0.0052 0.0168 0.0251 0.0299
0.0175 0.0099 0.0248 0.0346 0.0402
0.0349 0.0162 0.0342 0.0457 0.0521
0.0524 0.0240 0.0452 0.0583 0.0655
0.0698 0.0334 0.0577 0.0724 0.0804
0.0873 0.0442 0.0718 0.0881 0.0968
0.1047 0.0566 0.0874 0.1053 0.1148
0.1222 0.0706 0.1045 0.1240 0.1343
0.1396 0.0860 0.1232 0.1442 0.1554
0.1571 0.0962 0.1353 0.1573 0.1690
0.1745 0.1069 0.1479 0.1708 0.1830
0.1920 0.1180 0.1610 0.1849 0.1975
0.2094 0.1298 0.1746 0.1995 0.2126
0.2269 0.1424 0.1892 0.2151 0.2286
0.2443 0.1565 0.2054 0.2323 0.2464
0.2618 0.1727 0.2240 0.2521 0.2667
0.2793 0.1782 0.2302 0.2587 0.2735
0.2967 0.1716 0.2227 0.2507 0.2653
0.3142 0.1618 0.2115 0.2388 0.2531
0.3316 0.1475 0.1951 0.2214 0.2351
0.3491 0.1097 0.1512 0.1744 0.1866
</tableData>
</table>
</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/mag-elevator-pos-rad</property>
<value>0.0000</value>
</product>
</function>
<function name="aero/coefficient/CDbeta">
<description>Drag_due_to_sideslip</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/mag-beta-rad</property>
<value>0.1700</value>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/coefficient/CYb">
<description>Side_force_due_to_beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar lookup="row">aero/beta-rad</independentVar>
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
<tableData>
0.0000 30.0000
-0.3490 0.1370 0.1060
0.0000 0.0000 0.0000
0.3490 -0.1370 -0.1060
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CYda">
<description>Side_force_due_to_aileron</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/left-aileron-pos-rad</property>
<value>0.0000</value>
</product>
</function>
<function name="aero/coefficient/CYdr">
<description>Side_force_due_to_rudder</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>fcs/rudder-pos-rad</property>
<value>0.1870</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 lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
<tableData>
0.0000 30.0000
0.0000 -0.0750 -0.1610
0.0940 -0.1450 -0.2310
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CYr">
<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>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
<tableData>
0.0000 30.0000
0.0000 0.2140 0.1620
0.0940 0.2670 0.2150
</tableData>
</table>
</product>
</function>
</axis>
<axis name="LIFT">
<function name="aero/coefficient/CLwbh">
<description>Lift_due_to_alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCLge</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">aero/stall-hyst-norm</independentVar>
<tableData>
0.0000 1.0000
-0.0900 -0.2200 -0.2200
0.0000 0.2500 0.2500
0.0900 0.7300 0.7300
0.1000 0.8300 0.7800
0.1200 0.9200 0.7900
0.1400 1.0200 0.8100
0.1600 1.0800 0.8200
0.1700 1.1300 0.8300
0.1900 1.1900 0.8500
0.2100 1.2500 0.8600
0.2400 1.3500 0.8800
0.2600 1.4400 0.9000
0.2800 1.4700 0.9200
0.3000 1.4300 0.9500
0.3200 1.3800 0.9900
0.3400 1.3000 1.0500
0.3600 1.1500 1.1500
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CLDf">
<description>Delta_lift_due_to_flap_deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/function/kCLge</property>
<table>
<independentVar>fcs/flap-pos-deg</independentVar>
<tableData>
0.0000 0.0000
10.0000 0.2000
20.0000 0.3000
30.0000 0.3500
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CLDe">
<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>0.4300</value>
</product>
</function>
<function name="aero/coefficient/CLadot">
<description>Lift_due_to_alpha_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/alphadot-rad_sec</property>
<property>aero/ci2vel</property>
<value>1.7000</value>
</product>
</function>
<function name="aero/coefficient/CLq">
<description>Lift_due_to_pitch_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>velocities/q-aero-rad_sec</property>
<property>aero/ci2vel</property>
<value>3.9000</value>
</product>
</function>
</axis>
<axis name="ROLL">
<function name="aero/coefficient/Clb">
<description>Roll_moment_due_to_beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<table>
<independentVar>aero/beta-rad</independentVar>
<tableData>
-0.3490 0.0322
0.0000 0.0000
0.3490 -0.0322
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/Clp">
<description>Roll_moment_due_to_roll_rate_(roll_damping)</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>-0.4840</value>
</product>
</function>
<function name="aero/coefficient/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 lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">fcs/flap-pos-deg</independentVar>
<tableData>
0.0000 30.0000
0.0000 0.0798 0.1246
0.0940 0.1869 0.2317
</tableData>
</table>
</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>0.2290</value>
</product>
</function>
<function name="aero/coefficient/Cldr">
<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>0.0147</value>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/coefficient/Cmo">
<description>Pitching_moment_at_zero_alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<value>0.1000</value>
</product>
</function>
<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>-1.8000</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>-12.4000</value>
</product>
</function>
<function name="aero/coefficient/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>
<value>-7.2700</value>
</product>
</function>
<function name="aero/coefficient/Cmde">
<description>Pitch_moment_due_to_elevator_deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>fcs/elevator-pos-rad</property>
<value>-1.1220</value>
</product>
</function>
<function name="aero/coefficient/Cmdf">
<description>Delta_pitching_moment_due_to_flap_deflection</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<table>
<independentVar>fcs/flap-pos-deg</independentVar>
<tableData>
0.0000 0.0000
10.0000 -0.0654
20.0000 -0.0981
30.0000 -0.1140
</tableData>
</table>
</product>
</function>
</axis>
<axis name="YAW">
<function name="aero/coefficient/Cnb">
<description>Yaw_moment_due_to_beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<table>
<independentVar>aero/beta-rad</independentVar>
<tableData>
-0.3490 -0.0205
0.0000 0.0000
0.3490 0.0205
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/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>
<value>-0.0278</value>
</product>
</function>
<function name="aero/coefficient/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>
<value>-0.0937</value>
</product>
</function>
<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>
<property>fcs/left-aileron-pos-rad</property>
<value>-0.0053</value>
</product>
</function>
<function name="aero/coefficient/Cndr">
<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>-0.0430</value>
</product>
</function>
</axis>
</aerodynamics>
Sync. with JSBSim CVS
2008-08-08 08:56:08 +00:00
<!--
<output name="JSBout172C.csv" type="CSV" rate="60">
<property> aero/qbar-psf </property>
<property> accelerations/udot-ft_sec2 </property>
<property> accelerations/vdot-ft_sec2 </property>
<property> accelerations/wdot-ft_sec2 </property>
<property> accelerations/a-pilot-x-ft_sec2 </property>
<property> accelerations/a-pilot-y-ft_sec2 </property>
<property> accelerations/a-pilot-z-ft_sec2 </property>
<property> accelerations/n-pilot-x-norm </property>
<property> accelerations/n-pilot-y-norm </property>
<property> accelerations/n-pilot-z-norm </property>
<rates> ON </rates>
<velocities> ON </velocities>
<forces> ON </forces>
<moments> ON </moments>
<position> ON </position>
<fcs> OFF </fcs>
<propulsion> OFF </propulsion>
<aerosurfaces> OFF </aerosurfaces>
<fcs> OFF </fcs>
<ground_reactions> OFF </ground_reactions>
</output>
-->
sync. with JSBSim v. 2.0
2006-01-12 15:03:25 +00:00
</fdm_config>
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