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[fg:toms-fgdata.git] / Aircraft / fokker100 / fokker100.xml
1 <?xml version="1.0"?>
2 <?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
3 <fdm_config name="Fokker-100" version="2.0" release="ALPHA"
4    xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
5    xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
6
7  <fileheader>
8   <author> Erik Hofman </author>
9   <filecreationdate>2010-08-08</filecreationdate>
10   <version>$Revision: 1.31 $</version>
11   <description> Fokker-100 commercial airliner </description>
12   <reference title="Butterworth-Heinemann - Civil Jet Aircraft Design (BH)
13         http://www.elsevierdirect.com/companions/9780340741528/appendices/data-a/table-8/table.htm"/>
14   <reference title="Lissys - PIANO aircraft analysis software
15         http://www.lissys.demon.co.uk/f7tx2.html"/>
16   <reference title="Aerodynamic Design of Transport Aircraft
17         http://www.scribd.com/doc/23956816/Aerodynamic-Design-of-Transport-Aircraft"/>
18       <note>
19         This model was created using publicly available data, publicly available
20         technical reports, textbooks, and guesses. It contains no proprietary or
21         restricted data. If this model has been validated at all, it would be
22         only to the extent that it seems to "fly right", and that it possibly
23         complies with published, publicly known, performance data (maximum speed,
24         endurance, etc.). Thus, this model is meant for educational and entertainment
25         purposes only.
26
27         This simulation model is not endorsed by the manufacturer. This model is not
28         to be sold.
29       </note>
30  </fileheader>
31
32 <!--
33   File:     Fokker-100.xml
34   Inputs:
35     name:          Fokker-100
36     type:          two-engine transonic transport
37     max weight:    95013.45 lb
38     wing span:     92.13048 ft
39     length:        106.6325 ft
40     wing area:     1006.5275 sq-ft
41     gear type:     tricycle
42     retractable?:  yes
43     # engines:     2
44     engine type:   turbine
45     engine layout: aft fuselage
46     yaw damper?    yes
47
48   Outputs:
49     wing loading:  94.40 lb/sq-ft
50     CL-alpha:      4.4 per radian
51     CL-0:          0.2
52     CL-max:        1.72
53     CD-0:          0.02
54     K:             0.043
55
56 -->
57
58  <metrics>
59    <wingarea  unit="FT2"> 1006.53 </wingarea>
60    <wingspan  unit="FT" >   92.13 </wingspan>
61    <wing_incidence>          2.00 </wing_incidence>
62    <chord     unit="FT" >   12.4671 </chord>
63    <htailarea unit="FT2">  233.792 </htailarea>
64    <htailarm  unit="FT" >   52.4934 </htailarm>
65    <vtailarea unit="FT2">  132.396 </vtailarea>
66    <vtailarm  unit="FT" >   44.6194 </vtailarm>
67    <location name="AERORP" unit="IN">
68      <x> 699.48 </x> <!-- 668.48 -->
69      <y>   0.00 </y>
70      <z>  38.00 </z>
71    </location>
72    <location name="EYEPOINT" unit="IN">
73      <x> 122.04 </x>
74      <y> -30.00 </y>
75      <z>  88.94 </z>
76    </location>
77    <location name="VRP" unit="IN">
78      <x> 101.65 </x>
79      <y>   0.0  </y>
80      <z>   0.0  </z>
81    </location>
82  </metrics>
83
84  <mass_balance>
85    <ixx unit="SLUG*FT2">    234805 </ixx>
86    <iyy unit="SLUG*FT2">    726720 </iyy>
87    <izz unit="SLUG*FT2">    925012 </izz>
88    <emptywt unit="LBS" >     54217 </emptywt>
89    <location name="CG" unit="IN">
90      <x> 719.81 </x> <!-- 693.81 -->
91      <y>   0.00 </y>
92      <z>  38.12 </z>
93    </location>
94    <pointmass name="pilot">
95      <weight unit="LBS"> 230 </weight>
96      <location name="POINTMASS" unit="IN">
97        <x> 122.04 </x>
98        <y> -30.0 </y>
99        <z>  66.0 </z>
100      </location>
101    </pointmass>
102    <pointmass name="copilot">
103      <weight unit="LBS"> 230 </weight>
104      <location name="POINTMASS" unit="IN">
105        <x> 122.04 </x>
106        <y>  30.0 </y>
107        <z>  66.0 </z>
108      </location>
109    </pointmass>
110    <pointmass name="steward">
111      <weight unit="LBS"> 400 </weight>
112      <location name="POINTMASS" unit="IN">
113        <x>  218 </x>
114        <y>  32.0 </y>
115        <z>  66.0 </z>
116      </location>
117    </pointmass>
118  </mass_balance>
119
120  <ground_reactions>
121
122   <contact type="BOGEY" name="NOSE">
123    <location unit="IN">
124      <x> 172.87 </x>
125      <y>   0.00 </y>
126      <z> -55.73 </z>
127    </location>
128    <static_friction>  0.80 </static_friction>
129    <dynamic_friction> 0.50 </dynamic_friction>
130    <rolling_friction> 0.02 </rolling_friction>
131    <spring_coeff unit="LBS/FT">       7750.03 </spring_coeff>
132    <damping_coeff unit="LBS/FT/SEC">  1600.34 </damping_coeff>
133    <max_steer unit="DEG"> 5.00 </max_steer>
134    <brake_group>NONE</brake_group>
135    <retractable>1</retractable>
136  </contact>
137
138   <contact type="BOGEY" name="LEFT_MAIN">
139    <location unit="IN">
140      <x> 731.93 </x>
141      <y>-101.65 </y>
142      <z> -63.53 </z>
143    </location>
144    <static_friction>  0.80 </static_friction>
145    <dynamic_friction> 0.50 </dynamic_friction>
146    <rolling_friction> 0.02 </rolling_friction>
147    <spring_coeff unit="LBS/FT">      95013.45 </spring_coeff>
148    <damping_coeff unit="LBS/FT/SEC"> 19002.69 </damping_coeff>
149    <max_steer unit="DEG">0</max_steer>
150    <brake_group>LEFT</brake_group>
151    <retractable>1</retractable>
152  </contact>
153
154   <contact type="BOGEY" name="RIGHT_MAIN">
155    <location unit="IN">
156      <x> 731.93 </x>
157      <y> 101.65 </y>
158      <z> -63.53 </z>
159    </location>
160    <static_friction>  0.80 </static_friction>
161    <dynamic_friction> 0.50 </dynamic_friction>
162    <rolling_friction> 0.02 </rolling_friction>
163    <spring_coeff unit="LBS/FT">      95013.45 </spring_coeff>
164    <damping_coeff unit="LBS/FT/SEC"> 19002.69 </damping_coeff>
165    <max_steer unit="DEG">0</max_steer>
166    <brake_group>RIGHT</brake_group>
167    <retractable>1</retractable>
168  </contact>
169
170   <contact type="STRUCTURE" name="LEFT_WING">
171     <location unit="IN">
172      <x> 753.77 </x>
173      <y>-1105.4 </y>
174      <z>   0.0 </z>
175     </location>
176     <static_friction>  0.80 </static_friction>
177     <dynamic_friction> 0.50 </dynamic_friction>
178     <spring_coeff unit="LBS/FT">      95013.45 </spring_coeff>
179     <damping_coeff unit="LBS/FT/SEC"> 19002.69 </damping_coeff>
180  </contact>
181
182   <contact type="STRUCTURE" name="RIGHT_WING">
183     <location unit="IN">
184      <x> 753.77 </x>
185      <y> 1105.4 </y>
186      <z>   0.0  </z>
187     </location>
188     <static_friction>  0.80 </static_friction>
189     <dynamic_friction> 0.50 </dynamic_friction>
190     <spring_coeff unit="LBS/FT">      95013.45 </spring_coeff>
191     <damping_coeff unit="LBS/FT/SEC"> 19002.69 </damping_coeff>
192  </contact>
193
194  </ground_reactions>
195
196  <external_reactions>
197     <force name="pushback" frame="BODY">
198        <location unit="IN">
199           <x>-139</x>
200           <y>0</y>
201           <z>-71</z>
202        </location>
203        <direction>
204           <x>1</x>
205           <y>0</y>
206           <z>0</z>
207        </direction>
208     </force>
209  </external_reactions>
210
211  <propulsion>
212
213    <engine file="Tay-620">
214     <location unit="IN">
215       <x>  922.52 </x>
216       <y> -101.65 </y>
217       <z>   43.53 </z>
218     </location>
219     <orient unit="DEG">
220       <pitch> 0.00 </pitch>
221       <roll>  0.00 </roll>
222       <yaw>   0.00 </yaw>
223     </orient>
224     <feed>0</feed>
225     <thruster file="direct">
226      <location unit="IN">
227        <x>  922.52 </x>
228        <y> -101.65 </y>
229        <z>   43.53 </z>
230      </location>
231      <orient unit="DEG">
232        <pitch> 0.00 </pitch>
233        <roll>  0.00 </roll>
234        <yaw>   0.00 </yaw>
235      </orient>
236     </thruster>
237   </engine>
238
239    <engine file="Tay-620">
240     <location unit="IN">
241       <x>  922.52 </x>
242       <y>  101.65 </y>
243       <z>   43.53 </z>
244     </location>
245     <orient unit="DEG">
246       <pitch> 0.00 </pitch>
247       <roll>  0.00 </roll>
248       <yaw>   0.00 </yaw>
249     </orient>
250     <feed>1</feed>
251     <thruster file="direct">
252      <location unit="IN">
253        <x>  922.52 </x>
254        <y>  101.65 </y>
255        <z>   43.53 </z>
256      </location>
257      <orient unit="DEG">
258        <pitch> 0.00 </pitch>
259        <roll>  0.00 </roll>
260        <yaw>   0.00 </yaw>
261      </orient>
262     </thruster>
263   </engine>
264
265   <tank type="FUEL" number="0">
266      <location unit="IN">
267        <x> 713.81 </x>
268        <y>-190.59 </y>
269        <z>   0.0  </z>
270      </location>
271      <capacity unit="LBS"> 13360.01 </capacity>
272      <contents unit="LBS">  8688.50 </contents>
273   </tank>
274
275   <tank type="FUEL" number="1">
276      <location unit="IN">
277        <x> 713.81 </x>
278        <y> 190.59 </y>
279        <z>   0.0  </z>
280      </location>
281      <capacity unit="LBS"> 13360.01 </capacity>
282      <contents unit="LBS">  8688.50 </contents>
283   </tank>
284 <!--
285   <tank type="FUEL" number="2">
286      <location unit="IN">
287        <x> 703.77 </x>
288        <y>   0.00 </y>
289        <z> -31.99 </z>
290      </location>
291      <capacity unit="LBS"> 1377.01 </capacity>
292      <contents unit="LBS"> 688.50 </contents>
293   </tank>
294 -->
295  </propulsion>
296
297  <system file="pushback"/>
298
299  <flight_control name="FCS: Fokker-100">
300
301   <channel name="Pitch">
302    <summer name="fcs/pitch-trim-sum">
303       <input>fcs/elevator-cmd-norm</input>
304       <input>fcs/pitch-trim-cmd-norm</input>
305       <clipto>
306         <min> -1 </min>
307         <max>  1 </max>
308       </clipto>
309    </summer>
310
311    <aerosurface_scale name="fcs/elevator-control">
312       <input>fcs/pitch-trim-sum</input>
313       <range>
314         <min> -0.35 </min>
315         <max>  0.35 </max>
316       </range>
317       <output>fcs/elevator-pos-rad</output>
318    </aerosurface_scale>
319
320    <aerosurface_scale name="fcs/elevator-normalization">
321       <input>fcs/elevator-pos-rad</input>
322       <domain>
323         <min> -0.35 </min>
324         <max>  0.35 </max>
325       </domain>
326       <range>
327         <min> -1 </min>
328         <max>  1 </max>
329       </range>
330       <output>fcs/elevator-pos-norm</output>
331    </aerosurface_scale>
332
333   </channel>
334
335   <channel name="Roll">
336    <summer name="fcs/roll-trim-sum">
337       <input>fcs/aileron-cmd-norm</input>
338       <input>fcs/roll-trim-cmd-norm</input>
339       <clipto>
340         <min> -1 </min>
341         <max>  1 </max>
342       </clipto>
343    </summer>
344
345    <aerosurface_scale name="fcs/left-aileron-control">
346       <input>fcs/roll-trim-sum</input>
347       <range>
348         <min> -0.35 </min>
349         <max>  0.35 </max>
350       </range>
351       <output>fcs/left-aileron-pos-rad</output>
352    </aerosurface_scale>
353
354    <aerosurface_scale name="fcs/right-aileron-control">
355       <input>fcs/roll-trim-sum</input>
356       <range>
357         <min> -0.35 </min>
358         <max>  0.35 </max>
359       </range>
360       <output>fcs/right-aileron-pos-rad</output>
361    </aerosurface_scale>
362
363    <aerosurface_scale name="fcs/left-aileron-normalization">
364       <input>fcs/left-aileron-pos-rad</input>
365       <domain>
366         <min> -0.35 </min>
367         <max>  0.35 </max>
368       </domain>
369       <range>
370         <min> -1 </min>
371         <max>  1 </max>
372       </range>
373       <output>fcs/left-aileron-pos-norm</output>
374    </aerosurface_scale>
375
376    <aerosurface_scale name="fcs/right-aileron-normalization">
377       <input>fcs/right-aileron-pos-rad</input>
378       <domain>
379         <min> -0.35 </min>
380         <max>  0.35 </max>
381       </domain>
382       <range>
383         <min> -1 </min>
384         <max>  1 </max>
385       </range>
386       <output>fcs/right-aileron-pos-norm</output>
387    </aerosurface_scale>
388
389   </channel>
390
391   <channel name="Yaw">
392    <summer name="fcs/rudder-command-sum">
393       <input>fcs/rudder-cmd-norm</input>
394       <input>fcs/yaw-trim-cmd-norm</input>
395       <clipto>
396         <min> -0.35 </min>
397         <max>  0.35 </max>
398       </clipto>
399    </summer>
400
401    <scheduled_gain name="fcs/yaw-damper-rate">
402       <input>velocities/r-aero-rad_sec</input>
403       <table>
404         <independentVar lookup="row">velocities/ve-kts</independentVar>
405          <tableData>
406             30     0.00
407             60     2.00
408          </tableData>
409       </table>
410    </scheduled_gain>
411
412    <scheduled_gain name="fcs/yaw-damper-beta">
413       <input>aero/beta-rad</input>
414       <table>
415         <independentVar lookup="row">velocities/ve-kts</independentVar>
416         <tableData>
417            30     0.00
418            60     0.00
419         </tableData>
420       </table>
421    </scheduled_gain>
422
423    <summer name="fcs/yaw-damper-sum">
424       <input>fcs/yaw-damper-beta</input>
425       <input>fcs/yaw-damper-rate</input>
426       <clipto>
427         <min> -0.1 </min>
428         <max>  0.1 </max>
429       </clipto>
430    </summer>
431
432    <scheduled_gain name="fcs/yaw-damper-final">
433       <input>fcs/yaw-damper-sum</input>
434       <table>
435         <independentVar lookup="row">velocities/ve-kts</independentVar>
436         <tableData>
437            30         0.0
438            31         1.0
439         </tableData>
440       </table>
441    </scheduled_gain>
442
443    <summer name="fcs/rudder-sum">
444       <input>fcs/rudder-command-sum</input>
445       <input>fcs/yaw-damper-final</input>
446       <clipto>
447         <min> -1 </min>
448         <max>  1 </max>
449       </clipto>
450    </summer>
451
452    <aerosurface_scale name="fcs/rudder-control">
453       <input>fcs/rudder-sum</input>
454       <range>
455         <min> -0.35 </min>
456         <max>  0.35 </max>
457       </range>
458       <output>fcs/rudder-pos-rad</output>
459    </aerosurface_scale>
460
461    <aerosurface_scale name="rcs/rudder-normalization">
462       <input>fcs/rudder-pos-rad</input>
463       <domain>
464         <min> -0.35 </min>
465         <max>  0.35 </max>
466       </domain>
467       <range>
468         <min> -1 </min>
469         <max>  1 </max>
470       </range>
471       <output>fcs/rudder-pos-norm</output>
472    </aerosurface_scale>
473
474   </channel>
475
476   <channel name="Flaps">
477    <kinematic name="fcs/flaps-control">
478      <input>fcs/flap-cmd-norm</input>
479      <traverse>
480        <setting>
481          <position>0</position>
482          <time>0</time>
483        </setting>
484        <setting>
485          <position>8</position>
486          <time>3</time>
487        </setting>
488        <setting>
489          <position>15</position>
490          <time>3</time>
491        </setting>
492        <setting>
493          <position>25</position>
494          <time>4</time>
495        </setting>
496        <setting>
497          <position>42</position>
498          <time>4</time>
499        </setting>
500      </traverse>
501      <output>fcs/flap-pos-deg</output>
502    </kinematic>
503
504    <aerosurface_scale name="fcs/flap-normalization">
505       <input>fcs/flap-pos-deg</input>
506       <domain>
507         <min>0</min>
508         <max>42</max>
509       </domain>
510       <range>
511         <min>0</min>
512         <max>1</max>
513       </range>
514       <output>fcs/flap-pos-norm</output>
515    </aerosurface_scale>
516
517   </channel>
518
519   <channel name="Landing Gear">
520    <kinematic name="fcs/gear-control">
521      <input>gear/gear-cmd-norm</input>
522      <traverse>
523        <setting>
524           <position> 0 </position>
525           <time>     0 </time>
526        </setting>
527        <setting>
528           <position> 1 </position>
529           <time>     5 </time>
530        </setting>
531      </traverse>
532      <output>gear/gear-pos-norm</output>
533    </kinematic>
534
535   </channel>
536
537   <channel name="Speedbrake">
538    <kinematic name="fcs/speedbrake-control">
539      <input>fcs/speedbrake-cmd-norm</input>
540      <traverse>
541        <setting>
542           <position> 0 </position>
543           <time>     0 </time>
544        </setting>
545        <setting>
546           <position> 1 </position>
547           <time>     1 </time>
548        </setting>
549      </traverse>
550      <output>fcs/speedbrake-pos-norm</output>
551    </kinematic>
552   </channel>
553
554
555   <channel name="Spoilers">
556    <kinematic name="fcs/spoiler-control">
557      <input>fcs/spoiler-cmd-norm</input>
558      <traverse>
559         <setting>
560           <position>0</position>
561           <time>0</time>
562         </setting>
563         <setting>
564           <position>1</position>
565           <time>1</time>
566         </setting>
567      </traverse>
568      <output>fcs/spoiler-pos-norm</output>
569    </kinematic>
570   </channel>
571  </flight_control>
572
573     <aerodynamics>  
574
575         <function name="aero/function/kCDge">
576             <description>Change_in_drag_due_to_ground_effect</description>
577             <product>
578                   <table>
579                       <independentVar>aero/h_b-mac-ft</independentVar>
580                       <tableData>
581                           0.0000        0.0350
582                           0.1000        0.4170
583                           0.1500        0.5390
584                           0.2000        0.6240
585                           0.3000        0.7510
586                           0.4000        0.8000
587                           0.5000        0.8960
588                           0.6000        0.9390
589                           0.7000        0.9740
590                           0.8000        0.9810
591                           0.9000        0.9900
592                           1.0000        0.9940
593                           1.1000        1.0000
594                       </tableData>
595                   </table>
596             </product>
597         </function>
598
599         <function name="aero/function/kCLge">
600             <description>Change_in_lift_due_to_ground_effect</description>
601             <product>
602                   <table>
603                       <independentVar>aero/h_b-mac-ft</independentVar>
604                       <tableData>
605                           0.0000        1.3910
606                           0.1000        1.2350
607                           0.1500        1.1670
608                           0.2000        1.1350
609                           0.3000        1.0850
610                           0.4000        1.1020
611                           0.5000        1.0350
612                           0.6000        1.0240
613                           0.7000        1.0150
614                           0.8000        1.0110
615                           0.9000        1.0060
616                           1.0000        1.0040
617                           1.1000        1.0000
618                       </tableData>
619                   </table>
620             </product>
621         </function>
622
623         <function name="aero/function/kCmge">
624             <description>Change_in_pitch_due_to_ground_effect</description>
625             <product>
626                 <table>
627                     <independentVar>aero/h_b-mac-ft</independentVar>
628                     <tableData>
629                           0.0000        1.2030
630                           0.1000        1.1270
631                           0.1500        1.0900
632                           0.2000        1.0730
633                           0.3000        1.0460
634                           0.4000        1.0550
635                           0.5000        1.0190
636                           0.6000        1.0130
637                           0.7000        1.0080
638                           0.8000        1.0060
639                           0.9000        1.0030
640                           1.0000        1.0020
641                           1.1000        1.0000
642                     </tableData>
643                 </table>
644             </product>
645         </function>
646
647
648         <axis name="DRAG">
649             <function name="aero/coefficient/CD0">
650                 <description>Drag_at_zero_lift</description>
651                 <product>
652                     <property>aero/qbar-psf</property>
653                     <property>metrics/Sw-sqft</property>
654                     <property>aero/function/kCDge</property>
655                       <table>
656                           <independentVar>aero/alpha-rad</independentVar>
657                           <tableData>
658                               -1.5700   1.5000
659                               -0.2600   0.0400
660                               0.0000    0.01922
661                               0.2600    0.0400
662                               1.5700    1.5000
663                           </tableData>
664                       </table>
665                 </product>
666             </function>
667             <function name="aero/coefficient/CDi">
668                 <description>Induced_drag</description>
669                 <product>
670                     <property>aero/qbar-psf</property>
671                     <property>metrics/Sw-sqft</property>
672                     <property>aero/function/kCDge</property>
673                     <table>
674                           <independentVar>velocities/mach</independentVar>
675                           <tableData>
676                               0.458     0.04432
677                               0.546     0.02207
678                               0.600     0.01469
679                               0.720     0.00867
680                               0.800     0.00478
681                               0.860     0.00358
682                           </tableData>
683                       </table>
684                 </product>
685             </function>
686             <function name="aero/coefficient/CDDflap">
687                 <description>Drag_due_to_flap_deflection</description>
688                 <product>
689                     <property>aero/qbar-psf</property>
690                     <property>metrics/Sw-sqft</property>
691                     <property>aero/function/kCDge</property>
692                     <table>
693                           <independentVar lookup="row">aero/alpha-rad</independentVar>
694                           <independentVar lookup="column">fcs/flap-pos-deg</independentVar>
695                           <tableData>
696                                      0.000  25.0   42.0
697                               -0.07  0.0000 0.0047 0.0156
698                                0.00  0.0000 0.0070 0.0200
699                                0.03  0.0001 0.0077 0.0225
700                                0.07  0.0005 0.0089 0.0257
701                                0.10  0.0008 0.0129 0.0276
702                                0.14  0.0025 0.0156 0.0313
703                           </tableData>
704                       </table>
705                 </product>
706             </function>
707             <function name="aero/coefficient/CDmach">
708                 <description>Drag_due_to_mach</description>
709                 <product>
710                     <property>aero/qbar-psf</property>
711                     <property>metrics/Sw-sqft</property>
712                       <table>
713                           <independentVar>velocities/mach</independentVar>
714                           <tableData>
715                               0.000     0.00000
716                               0.600     0.00000
717                               0.650     0.00026
718                               0.720     0.00115
719                               0.770     0.00251
720                               0.800     0.00373
721                               0.848     0.01067
722                               0.860     0.01858
723                               1.000     0.02737
724                           </tableData>
725                       </table>
726                 </product>
727             </function>
728             <function name="aero/coefficient/CDgear">
729                 <description>Drag_due_to_gear</description>
730                 <product>
731                     <property>aero/qbar-psf</property>
732                     <property>metrics/Sw-sqft</property>
733                     <property>gear/gear-pos-norm</property>
734                     <value>0.0120</value>
735                 </product>
736             </function>
737             <function name="aero/coefficient/CDsb">
738                 <description>Drag_due_to_speedbrakes</description>
739                 <product>
740                     <property>aero/qbar-psf</property>
741                     <property>metrics/Sw-sqft</property>
742                     <property>fcs/speedbrake-pos-norm</property>
743                     <value>0.1200</value>
744                 </product>
745             </function>
746             <function name="aero/coefficient/CDsp">
747                 <description>Drag_due_to_spoilers</description>
748                 <product>
749                     <property>aero/qbar-psf</property>
750                     <property>metrics/Sw-sqft</property>
751                     <property>fcs/spoiler-pos-norm</property>
752                     <value>0.0280</value>
753                 </product>
754             </function>
755             <function name="aero/coefficient/CDrv">
756                 <description>Drag_due_to_reverse</description>
757                 <product>
758                     <property>aero/qbar-psf</property>
759                     <property>metrics/Sw-sqft</property>
760                     <property>propulsion/engine[0]/reverser-angle-rad</property>
761                     <property>propulsion/engine[1]/reverser-angle-rad</property>
762                     <value>0.0187</value>
763                 </product>
764             </function>
765             <function name="aero/coefficient/CDbeta">
766                 <description>Drag_due_to_sideslip</description>
767                 <product>
768                     <property>aero/qbar-psf</property>
769                     <property>metrics/Sw-sqft</property>
770                       <table>
771                           <independentVar>aero/beta-rad</independentVar>
772                           <tableData>
773                               -1.5700   1.2300
774                               -0.2600   0.0500
775                               0.0000    0.0000
776                               0.2600    0.0500
777                               1.5700    1.2300
778                           </tableData>
779                       </table>
780                 </product>
781             </function>
782             <function name="aero/coefficient/CDde">
783                 <description>Drag_due_to_Elevator_Deflection</description>
784                 <product>
785                     <property>aero/qbar-psf</property>
786                     <property>metrics/Sw-sqft</property>
787                     <property>fcs/mag-elevator-pos-rad</property>
788                     <value>0.0590</value>
789                 </product>
790             </function>
791         </axis>
792
793         <axis name="SIDE">
794             <function name="aero/coefficient/CYb">
795                 <description>Side_force_due_to_beta</description>
796                 <product>
797                     <property>aero/qbar-psf</property>
798                     <property>metrics/Sw-sqft</property>
799                     <property>aero/beta-rad</property>
800                     <value>-1.0000</value>
801                 </product>
802             </function>
803         </axis>
804
805         <axis name="LIFT">
806             <function name="aero/coefficient/CLflaps">
807                 <description>Lift_due_to_flap_deflection</description>
808                 <product>
809                     <property>aero/qbar-psf</property>
810                     <property>metrics/Sw-sqft</property>
811                     <property>aero/function/kCLge</property>
812                       <table>
813                           <independentVar lookup="row">aero/alpha-rad</independentVar>
814                           <independentVar lookup="column">fcs/flap-pos-deg</independentVar>
815                           <tableData>
816                                      0.000  25.0   42.0 
817                                0.00  0.217  0.837  1.269
818                                0.17  1.109  1.701  2.173
819                                0.21  1.270  1.827  2.308
820                                0.24  1.400  1.722  1.908
821                                0.28  1.336  0.707  0.000
822                                0.60  0.600  0.000  0.000
823                           </tableData>
824                       </table>
825                 </product>
826             </function>
827             <function name="aero/coefficient/dCLsp">
828                 <description>Delta_Lift_due_to_spoiler</description>
829                 <product>
830                     <property>aero/qbar-psf</property>
831                     <property>metrics/Sw-sqft</property>
832                     <property>fcs/spoiler-pos-norm</property>
833                     <property>aero/function/kCLge</property>
834                     <value>-0.1200</value>
835                 </product>
836             </function>
837             <function name="aero/coefficient/CLde">
838                 <description>Lift_due_to_Elevator_Deflection</description>
839                 <product>
840                     <property>aero/qbar-psf</property>
841                     <property>metrics/Sw-sqft</property>
842                     <property>fcs/elevator-pos-rad</property>
843                     <value>0.2000</value>
844                 </product>
845             </function>
846         </axis>
847
848         <axis name="ROLL">
849             <function name="aero/coefficient/Clb">
850                 <description>Roll_moment_due_to_beta</description>
851                 <product>
852                     <property>aero/qbar-psf</property>
853                     <property>metrics/Sw-sqft</property>
854                     <property>metrics/bw-ft</property>
855                     <property>aero/beta-rad</property>
856                     <value>-0.1000</value>
857                 </product>
858             </function>
859             <function name="aero/coefficient/Clp">
860                 <description>Roll_moment_due_to_roll_rate</description>
861                 <product>
862                     <property>aero/qbar-psf</property>
863                     <property>metrics/Sw-sqft</property>
864                     <property>metrics/bw-ft</property>
865                     <property>aero/bi2vel</property>
866                     <property>velocities/p-aero-rad_sec</property>
867                     <value>-0.4000</value>
868                 </product>
869             </function>
870             <function name="aero/coefficient/Clr">
871                 <description>Roll_moment_due_to_yaw_rate</description>
872                 <product>
873                     <property>aero/qbar-psf</property>
874                     <property>metrics/Sw-sqft</property>
875                     <property>metrics/bw-ft</property>
876                     <property>aero/bi2vel</property>
877                     <property>velocities/r-aero-rad_sec</property>
878                     <value>0.1500</value>
879                 </product>
880             </function>
881             <function name="aero/coefficient/Clda">
882                 <description>Roll_moment_due_to_aileron</description>
883                 <product>
884                     <property>aero/qbar-psf</property>
885                     <property>metrics/Sw-sqft</property>
886                     <property>metrics/bw-ft</property>
887                     <table>
888                           <independentVar lookup="row">velocities/mach</independentVar>
889                           <independentVar lookup="column">fcs/left-aileron-pos-rad</independentVar>
890                           <tableData>
891                                     -0.349 -0.1745 0.000  0.1745 0.349
892                                0.00 -0.043 -0.022  0.000  0.022  0.043
893                                0.60 -0.043 -0.022  0.000  0.022  0.043
894                                0.65 -0.037 -0.022  0.000  0.022  0.037
895                                0.70 -0.027 -0.022  0.000  0.023  0.027
896                                0.75 -0.027 -0.019  0.000  0.019  0.027
897                                0.88 -0.026 -0.019  0.000  0.019  0.026
898                           </tableData>
899                       </table>
900                 </product>
901             </function>
902             <function name="aero/coefficient/Cldr">
903                 <description>Roll_moment_due_to_rudder</description>
904                 <product>
905                     <property>aero/qbar-psf</property>
906                     <property>metrics/Sw-sqft</property>
907                     <property>metrics/bw-ft</property>
908                     <property>fcs/rudder-pos-rad</property>
909                     <value>0.0100</value>
910                 </product>
911             </function>
912         </axis>
913
914         <axis name="PITCH">
915             <function name="aero/coefficient/Cmo">
916                 <description>Pitching_moment_at_zero_alpha</description>
917                 <product>
918                     <property>aero/qbar-psf</property>
919                     <property>metrics/Sw-sqft</property>
920                     <property>metrics/cbarw-ft</property>
921                     <property>aero/function/kCmge</property>
922                     <value>-0.000737</value>
923                 </product>
924             </function>
925             <function name="aero/coefficient/Cmalpha">
926                 <description>Pitch_moment_due_to_alpha</description>
927                 <product>
928                     <property>aero/qbar-psf</property>
929                     <property>metrics/Sw-sqft</property>
930                     <property>metrics/cbarw-ft</property>
931                     <property>aero/alpha-rad</property>
932                     <value>-0.6000</value>
933                 </product>
934             </function>
935             <function name="aero/coefficient/Cmde">
936                 <description>Pitch_moment_due_to_elevator</description>
937                 <product>
938                     <property>aero/qbar-psf</property>
939                     <property>metrics/Sw-sqft</property>
940                     <property>metrics/cbarw-ft</property>
941                     <property>fcs/elevator-pos-rad</property>
942                       <table>
943                           <independentVar>velocities/mach</independentVar>
944                           <tableData>
945                               0.0000    -1.2000
946                               2.0000    -0.3000
947                           </tableData>
948                       </table>
949                 </product>
950             </function>
951             <function name="aero/coefficient/Cmq">
952                 <description>Pitch_moment_due_to_pitch_rate</description>
953                 <product>
954                     <property>aero/qbar-psf</property>
955                     <property>metrics/Sw-sqft</property>
956                     <property>metrics/cbarw-ft</property>
957                     <property>aero/ci2vel</property>
958                     <property>velocities/q-aero-rad_sec</property>
959                     <value>-31.0000</value>
960                 </product>
961             </function>
962             <function name="aero/coefficient/Cmadot">
963                 <description>Pitch_moment_due_to_alpha_rate</description>
964                 <product>
965                     <property>aero/qbar-psf</property>
966                     <property>metrics/Sw-sqft</property>
967                     <property>metrics/cbarw-ft</property>
968                     <property>aero/ci2vel</property>
969                     <property>aero/alphadot-rad_sec</property>
970                     <value>-16.0000</value>
971                 </product>
972             </function>
973         </axis>
974
975         <axis name="YAW">
976             <function name="aero/coefficient/Cnb">
977                 <description>Yaw_moment_due_to_beta</description>
978                 <product>
979                     <property>aero/qbar-psf</property>
980                     <property>metrics/Sw-sqft</property>
981                     <property>metrics/bw-ft</property>
982                     <property>aero/beta-rad</property>
983                     <value>0.1200</value>
984                 </product>
985             </function>
986             <function name="aero/coefficient/Cnr">
987                 <description>Yaw_moment_due_to_yaw_rate</description>
988                 <product>
989                     <property>aero/qbar-psf</property>
990                     <property>metrics/Sw-sqft</property>
991                     <property>metrics/bw-ft</property>
992                     <property>aero/bi2vel</property>
993                     <property>velocities/r-aero-rad_sec</property>
994                     <value>-0.1500</value>
995                 </product>
996             </function>
997             <function name="aero/coefficient/Cndr">
998                 <description>Yaw_moment_due_to_rudder</description>
999                 <product>
1000                     <property>aero/qbar-psf</property>
1001                     <property>metrics/Sw-sqft</property>
1002                     <property>metrics/bw-ft</property>
1003                     <property>fcs/rudder-pos-rad</property>
1004                     <value>-0.1000</value>
1005                 </product>
1006             </function>
1007             <function name="aero/coefficient/Cnda">
1008                 <description>Adverse_yaw</description>
1009                 <product>
1010                     <property>aero/qbar-psf</property>
1011                     <property>metrics/Sw-sqft</property>
1012                     <property>metrics/bw-ft</property>
1013                     <property>fcs/left-aileron-pos-rad</property>
1014                     <value>0.0000</value>
1015                 </product>
1016             </function>
1017         </axis>
1018     </aerodynamics>
1019 </fdm_config>