Merge branch 'master' of gitorious.org:fg/fgdata
[fg:toms-fgdata.git] / Aircraft / tu154b / tu154b.xml
1 <?xml version="1.0"?>
2 <?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
3 <fdm_config name="tu154b" version="2.0" release="PRODUCTION"
4     xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
5     xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
6
7 <!-- For FG-devel -->
8
9     <fileheader>
10         <author> Yurik V. Nikiforoff </author>
11         <filecreationdate> 2009-05-23 </filecreationdate>
12         <description>TU-154b airliner</description>
13         <version> 3.0 </version>
14     </fileheader>
15
16     <metrics>
17         <wingarea unit="M2"> 200 </wingarea>
18         <wingspan unit="M"> 37.55 </wingspan>
19         <chord unit="M"> 5.285 </chord>
20         <wing_incidence unit="DEG"> 3.0 </wing_incidence>
21         <htailarea unit="M2"> 40.55 </htailarea>
22         <htailarm unit="M"> 30 </htailarm>
23         <vtailarea unit="M2"> 31.7 </vtailarea>
24         <vtailarm unit="M"> 21.64 </vtailarm>
25         <location name="AERORP" unit="M">
26             <x> 27.211 </x>
27             <y> 0 </y>
28             <z> 0 </z>
29         </location>
30         <location name="EYEPOINT" unit="M">
31             <x> 3.35 </x>
32             <y> -0.76 </y>
33             <z> 1.9 </z>
34         </location>
35         <location name="VRP" unit="M">
36             <x> 26.0 </x>
37             <y> 0 </y>
38             <z> 0.0 </z>
39         </location>
40     </metrics>
41
42     <mass_balance>
43         <ixx unit="KG*M2">1.3e+06</ixx>
44         <iyy unit="KG*M2">4.36916e+06</iyy>
45         <izz unit="KG*M2">5.92493e+06</izz>
46         <ixz unit="KG*M2">0</ixz>
47         <iyz unit="KG*M2">0</iyz>
48         <ixy unit="KG*M2">0</ixy>
49         <emptywt unit="KG">54000</emptywt>
50         <location name="CG" unit="M">
51             <x>26.68</x>
52             <y>0</y>
53             <z>1.8</z>
54         </location>
55
56         <pointmass name="Crew">
57             <weight unit="KG">320</weight>
58             <location unit="M">
59                 <x>3.847</x>
60                 <y>0</y>
61                 <z>0</z>
62             </location>
63         </pointmass>
64
65         <pointmass name="Pax1">
66             <weight unit="KG">3000</weight>
67             <location unit="M">
68                 <x>12.0</x>
69                 <y>0</y>
70                 <z>0</z>
71             </location>
72         </pointmass>       
73         
74         <pointmass name="Pax2">
75             <weight unit="KG">3000</weight>
76             <location unit="M">
77                 <x>20.0</x>
78 <!--<x>5.84</x>-->
79 <!--<x>0.5</x>-->
80                 <y>0</y>
81                 <z>0</z>
82             </location>
83         </pointmass>
84
85         <pointmass name="Pax3">
86             <weight unit="KG">3000</weight>
87             <location unit="M">
88                 <x>30.0</x>
89                 <y>0</y>
90                 <z>0</z>
91             </location>
92         </pointmass>       
93
94         <!--Luggage-->
95
96         <pointmass name="Luggage_1">
97             <weight unit="KG">0</weight>
98             <location unit="M">
99                 <x>13.022</x>
100                 <y>0</y>
101                 <z>0</z>
102             </location>
103         </pointmass>       
104         <pointmass name="Luggage_2">
105             <weight unit="KG">0</weight>
106             <location unit="M">
107                 <x>14.022</x>
108                 <y>0</y>
109                 <z>0</z>
110             </location>
111         </pointmass>       
112         <pointmass name="Luggage_3">
113             <weight unit="KG">200</weight>
114             <location unit="M">
115                 <x>16.022</x>
116                 <y>0</y>
117                 <z>0</z>
118             </location>
119         </pointmass>       
120         <pointmass name="Luggage_4">
121             <weight unit="KG">200</weight>
122             <location unit="M">
123                 <x>19.022</x>
124                 <y>0</y>
125                 <z>0</z>
126             </location>
127         </pointmass>       
128         <pointmass name="Luggage_5">
129             <weight unit="KG">300</weight>
130             <location unit="M">
131                 <x>27.272</x>
132                 <y>0</y>
133                 <z>0</z>
134             </location>
135         </pointmass>       
136         <pointmass name="Luggage_6">
137             <weight unit="KG">300</weight>
138             <location unit="M">
139                 <x>29.772</x>
140                 <y>0</y>
141                 <z>0</z>
142             </location>
143         </pointmass>       
144         <pointmass name="Luggage_7">
145             <weight unit="KG">0</weight>
146             <location unit="M">
147                 <x>31.722</x>
148                 <y>0</y>
149                 <z>0</z>
150             </location>
151         </pointmass>       
152     </mass_balance>
153
154     <ground_reactions>
155         <contact type="BOGEY" name="NOSE">
156             <location unit="M">
157                 <x> 6.0 </x>
158                 <y> 0.0 </y>
159                 <z> -2.67 </z>
160             </location>
161             <static_friction> 0.9 </static_friction>
162             <dynamic_friction> 0.8 </dynamic_friction>
163             <rolling_friction> 0.02 </rolling_friction>
164             <spring_coeff unit="N/M"> 800000 </spring_coeff><!--800000-->
165             <damping_coeff unit="N/M/SEC"> 150000 </damping_coeff><!--150000-->
166             <max_steer unit="DEG"> 63.0 </max_steer>
167             <brake_group> NONE </brake_group>
168             <retractable> 1 </retractable>
169         </contact>
170         <contact type="BOGEY" name="LEFT_MAIN">
171             <location unit="M">
172                 <x> 26.82 </x>
173                 <y> -5.75 </y>
174                 <z> -2.5 </z>
175             </location>
176             <static_friction> 1.0 </static_friction>
177             <dynamic_friction> 0.5 </dynamic_friction>
178             <rolling_friction> 0.02 </rolling_friction><!--0.02-->
179             <spring_coeff unit="N/M"> 1.7e+06 </spring_coeff><!--1.7e+06 -->
180             <damping_coeff unit="N/M/SEC"> 100000 </damping_coeff>
181             <max_steer unit="DEG"> 0 </max_steer>
182             <brake_group> LEFT </brake_group>
183             <retractable> 1 </retractable>
184         </contact>
185         <contact type="BOGEY" name="RIGHT_MAIN">
186             <location unit="M">
187                 <x> 26.82 </x>
188                 <y> 5.75 </y>
189                 <z> -2.5 </z>
190             </location>
191             <static_friction> 1.0 </static_friction>
192             <dynamic_friction> 0.5 </dynamic_friction>
193             <rolling_friction> 0.02 </rolling_friction>
194             <spring_coeff unit="N/M"> 1.7e+06 </spring_coeff>
195             <!--<spring_coeff unit="N/M"> 3.1536e+06 </spring_coeff>-->
196             <!--<damping_coeff unit="N/M/SEC"> 630720 </damping_coeff>-->
197             <damping_coeff unit="N/M/SEC"> 100000 </damping_coeff><!--100000-->
198             <max_steer unit="DEG"> 0 </max_steer>
199             <brake_group> RIGHT </brake_group>
200             <retractable> 1 </retractable>
201         </contact>
202         <contact type="STRUCTURE" name="FRONT">
203             <location unit="M">
204                 <x> 3.5 </x>
205                 <y> 0.0 </y>
206                 <z> -0.2 </z>
207             </location>
208             <static_friction> 0.8 </static_friction>
209             <dynamic_friction> 0.5 </dynamic_friction>
210             <rolling_friction> 0 </rolling_friction>
211             <spring_coeff unit="N/M"> 3e+06 </spring_coeff>
212             <damping_coeff unit="N/M/SEC"> 630720 </damping_coeff>
213             <max_steer unit="DEG"> 0 </max_steer>
214             <brake_group> NONE </brake_group>
215             <retractable> 0 </retractable>
216         </contact>
217         <contact type="STRUCTURE" name="LEFT_WING">
218             <location unit="M">
219                 <x> 26.82 </x>
220                 <y> -18.7 </y>
221                 <z> -0.5 </z>
222             </location>
223             <static_friction> 0.8 </static_friction>
224             <dynamic_friction> 0.5 </dynamic_friction>
225             <rolling_friction> 0 </rolling_friction>
226             <spring_coeff unit="N/M"> 3e+06 </spring_coeff>
227             <damping_coeff unit="N/M/SEC"> 630720 </damping_coeff>
228             <max_steer unit="DEG"> 0 </max_steer>
229             <brake_group> NONE </brake_group>
230             <retractable> 0 </retractable>
231         </contact>
232         <contact type="STRUCTURE" name="RIGHT_WING">
233             <location unit="M">
234                 <x> 26.82 </x>
235                 <y> 18.7 </y>
236                 <z> -0.5 </z>
237             </location>
238             <static_friction> 0.8 </static_friction>
239             <dynamic_friction> 0.5 </dynamic_friction>
240             <rolling_friction> 0 </rolling_friction>
241             <spring_coeff unit="N/M"> 3e+06 </spring_coeff>
242             <damping_coeff unit="N/M/SEC"> 630720 </damping_coeff>
243             <max_steer unit="DEG"> 0 </max_steer>
244             <brake_group> NONE </brake_group>
245             <retractable> 0 </retractable>
246         </contact>
247         <contact type="STRUCTURE" name="TAIL">
248             <location unit="M">
249                 <x> 41 </x>
250                 <y> 0 </y>
251                 <z> 1 </z>
252             </location>
253             <static_friction> 0.8 </static_friction>
254             <dynamic_friction> 0.5 </dynamic_friction>
255             <rolling_friction> 0 </rolling_friction>
256             <spring_coeff unit="N/M"> 3e+06 </spring_coeff>
257             <damping_coeff unit="N/M/SEC"> 630720 </damping_coeff>
258             <max_steer unit="DEG"> 0 </max_steer>
259             <brake_group> NONE </brake_group>
260             <retractable> 0 </retractable>
261         </contact>
262     </ground_reactions>
263     
264     
265     <propulsion>
266
267         <engine file="nk-8-2u">
268             <location unit="M">
269                 <x> 34 </x>
270                 <y> -3.13 </y>
271                 <z> 1.78 </z>
272             </location>
273             <orient unit="DEG">
274                 <roll> 0 </roll>
275                 <pitch> 0 </pitch>
276                 <yaw> 0 </yaw>
277             </orient>
278             <feed>0</feed>
279             <thruster file="direct">
280                 <location unit="M">
281                     <x> 37.27 </x>
282                     <y> -3.03 </y>
283                     <z> 1.7 </z>
284                 </location>
285                 <orient unit="DEG">
286                     <roll> 0 </roll>
287                     <pitch> -2 </pitch>
288                     <yaw> 0 </yaw>
289                 </orient>
290             </thruster>
291         </engine>
292         <engine file="nk-8-2u">
293             <location unit="M">
294                 <x> 38 </x>
295                 <y> 0 </y>
296                 <z> 2.3 </z>
297             </location>
298             <orient unit="DEG">
299                 <roll> 0 </roll>
300                 <pitch> 0 </pitch>
301                 <yaw> 0 </yaw>
302             </orient>
303             <feed>0</feed>
304             <thruster file="direct">
305                 <location unit="M">
306                     <x> 41.6 </x>
307                     <y> 0 </y>
308                     <z> 2.26 </z>
309                 </location>
310                 <orient unit="DEG">
311                     <roll> 0 </roll>
312                     <pitch> -2 </pitch>
313                     <yaw> 0 </yaw>
314                 </orient>
315             </thruster>
316         </engine>
317         <engine file="nk-8-2u">
318             <location unit="M">
319                 <x> 34 </x>
320                 <y> 3.13 </y>
321                 <z> 1.78 </z>
322             </location>
323             <orient unit="DEG">
324                 <roll> 0 </roll>
325                 <pitch> 0 </pitch>
326                 <yaw> 0 </yaw>
327             </orient>
328             <feed>0</feed>
329             <thruster file="direct">
330                 <location unit="M">
331                     <x> 37.27 </x>
332                     <y> 3.03 </y>
333                     <z> 1.7 </z>
334                 </location>
335                 <orient unit="DEG">
336                     <roll> 0 </roll>
337                     <pitch> -2 </pitch>
338                     <yaw> 0 </yaw>
339                 </orient>
340             </thruster>
341         </engine>
342         <engine file="tsa-6a">
343           <location unit="M">
344             <x> 32 </x>
345             <y> 0 </y>
346             <z> 2.3 </z>
347           </location>
348           <orient unit="DEG">
349             <roll> 0 </roll>
350             <pitch> 0 </pitch>
351             <yaw> 0 </yaw>
352           </orient>
353           <feed>0</feed>
354           <thruster file="direct">
355             <location unit="M">
356               <x> 32 </x>
357               <y> 0 </y>
358               <z> 2.26 </z>
359             </location>
360             <orient unit="DEG">
361               <roll> 0 </roll>
362               <pitch> 0 </pitch>
363               <yaw> 90 </yaw>
364             </orient>
365           </thruster>
366         </engine>
367         <tank type="FUEL">
368             <location unit="M">
369                 <x> 25 </x>
370                 <y> 0 </y>
371                 <z> 0 </z>
372             </location>
373             <capacity unit="KG">3300</capacity>
374             <contents unit="KG">3300</contents>
375         </tank>
376         <tank type="FUEL">
377             <location unit="M">
378                 <x> 24 </x>
379                 <y> -4 </y>
380                 <z> 0 </z>
381             </location>
382             <capacity unit="KG">9500</capacity>
383             <contents unit="KG">2200</contents>
384         </tank>
385         <tank type="FUEL">
386             <location unit="M">
387                 <x> 27.5 </x>
388                 <y> -10 </y>
389                 <z> 0 </z>
390             </location>
391             <capacity unit="KG">5425</capacity>
392             <contents unit="KG">1000</contents>
393         </tank>
394         <tank type="FUEL">
395             <location unit="M">
396                 <x> 24 </x>
397                 <y> 4 </y>
398                 <z> 0 </z>
399             </location>
400             <capacity unit="KG">9500</capacity>
401             <contents unit="KG">2200</contents>
402         </tank>
403         <tank type="FUEL">
404             <location unit="M">
405                 <x> 27.5 </x>
406                 <y> 10 </y>
407                 <z> 0 </z>
408             </location>
409             <capacity unit="KG">5425</capacity>
410             <contents unit="KG">1000</contents>
411         </tank>
412         <tank type="FUEL">
413             <location unit="M">
414                 <x> 21 </x>
415                 <y> 0 </y>
416                 <z> 0 </z>
417             </location>
418             <capacity unit="KG">6600</capacity>
419 <!--            <contents unit="KG">3000</contents>-->
420             <contents unit="KG">5000</contents>
421         </tank>
422     </propulsion>
423     
424     <flight_control name="tu154b">
425 <!--      
426         <property>fcs/stab-auto-cmd</property>
427         <property>fcs/stabilizer-cmd-norm</property>
428         -->
429         <property>fcs/met</property>
430         <channel name="Pitch">
431                 
432             <aerosurface_scale name="fcs/met-trimmer">
433                 <input>fcs/pitch-trim-cmd-norm</input>
434                 <domain>
435                         <min>-1</min> 
436                         <max>1</max>
437                 </domain>
438                 <range>
439                         <min>-0.5</min>
440                         <max>0.6</max>
441                 </range>
442                 <output>fcs/met</output>
443             </aerosurface_scale>
444
445             <summer name="Pitch Trim Sum">
446               <input>fcs/elevator-cmd-norm</input>
447               <input>fcs/met</input>
448               <clipto>
449                 <min>-1</min>
450                 <max>1</max>
451               </clipto>
452             </summer>
453             
454             <switch name="fcs/pitch-ra-56-hydropower">
455               <default value="0.0"/>
456               <test value="fcs/absu-pitch">
457                 hs/ra-56-pitch-serviceable > 0
458               </test>
459             </switch>
460
461             <summer name="Pitch Absu Sum">
462               <input>fcs/pitch-trim-sum</input>
463               <input>fcs/pitch-ra-56-hydropower</input>
464               <clipto>
465                 <min>-1</min>
466                 <max>1</max>
467               </clipto>
468             </summer>
469             
470             <switch name="fcs/pitch-hydropower">
471               <default value="fcs/elevator-pos-static"/>
472               <test value="fcs/pitch-absu-sum">
473                 hs/busters-serviceable > 0
474               </test>
475             </switch>
476
477             <aerosurface_scale name="Elevator Control">
478               <input>fcs/pitch-hydropower</input>
479               <range>
480                 <min>-0.506</min>
481                 <max>0.28</max>
482               </range>
483               <output>fcs/elevator-pos-rad</output>
484             </aerosurface_scale>
485             
486             <aerosurface_scale name="Elevator Normalizer">
487               <input>fcs/elevator-pos-rad</input>
488               <domain>
489                 <min>-1</min> 
490                 <max>1</max>
491               </domain>
492               <range>
493                 <min>-1</min>
494                 <max>1</max>
495               </range>
496               <output>fcs/elevator-pos-norm</output>
497             </aerosurface_scale>
498
499         </channel>
500
501         <channel name="Roll">
502
503             <summer name="Roll Trim Sum">
504               <input>fcs/aileron-cmd-norm</input>
505               <input>fcs/roll-trim-cmd-norm</input>
506               <clipto>
507                 <min>-1</min>
508                 <max>1</max>
509               </clipto>
510             </summer>
511             
512             <switch name="fcs/roll-ra-56-hydropower">
513               <default value="0.0"/>
514               <test value="fcs/absu-roll">
515                 hs/ra-56-roll-serviceable > 0
516               </test>
517             </switch>
518
519             <summer name="Roll Absu Sum">
520               <input>fcs/roll-trim-sum</input>
521               <input>fcs/roll-ra-56-hydropower</input>
522               <clipto>
523                 <min>-1</min>
524                 <max>1</max>
525               </clipto>
526             </summer>
527             
528             <switch name="fcs/roll-hydropower">
529               <default value="fcs/aileron-pos-static"/>
530               <test value="fcs/roll-absu-sum">
531                 hs/busters-serviceable > 0
532               </test>
533             </switch>
534
535             <aerosurface_scale name="Left Aileron Control">
536               <input>fcs/roll-hydropower</input>
537               <range>
538                 <min>-0.35</min>
539                 <max>0.35</max>
540               </range>
541               <output>fcs/left-aileron-pos-rad</output>
542             </aerosurface_scale>
543
544             <aerosurface_scale name="Right Aileron Control">
545               <input>-fcs/roll-hydropower</input>
546               <range>
547                 <min>-0.35</min>
548                 <max>0.35</max>
549               </range>
550               <output>fcs/right-aileron-pos-rad</output>
551             </aerosurface_scale>
552             
553             <aerosurface_scale name="Aileron Normalizer">
554               <input>fcs/left-aileron-pos-rad</input>
555               <domain>
556                 <min>-1</min> 
557                 <max>1</max>
558               </domain>
559               <range>
560                 <min>-1</min>
561                 <max>1</max>
562               </range>
563               <output>fcs/left-aileron-pos-norm</output>
564             </aerosurface_scale>
565
566         </channel>
567
568         <channel name="Yaw">
569
570             <summer name="Rudder Command Sum">
571               <input>fcs/rudder-cmd-norm</input>
572               <input>fcs/yaw-trim-cmd-norm</input>
573             </summer>
574             
575             <switch name="fcs/yaw-ra-56-hydropower">
576               <default value="0.0"/>
577               <test value="fcs/absu-yaw">
578                 hs/ra-56-yaw-serviceable > 0
579               </test>
580             </switch>
581
582             <summer name="Rudder Sum">
583               <input>fcs/rudder-command-sum</input>
584               <input>fcs/yaw-ra-56-hydropower</input>
585             </summer>
586             
587             <switch name="fcs/yaw-hydropower">
588               <default value="fcs/rudder-pos-static"/>
589               <test value="fcs/rudder-sum">
590                 hs/busters-serviceable > 0
591               </test>
592             </switch>
593
594             <aerosurface_scale name="Rudder Control">
595               <input>fcs/yaw-hydropower</input>
596               <range>
597                 <min>-0.35</min>
598                 <max>0.35</max>
599               </range>
600               <output>fcs/rudder-pos-rad</output>
601             </aerosurface_scale>
602             
603             <aerosurface_scale name="Rudder Normalizer">
604               <input>fcs/rudder-pos-rad</input>
605               <domain>
606                 <min>-1</min> 
607                 <max>1</max>
608               </domain>
609               <range>
610                 <min>-1</min>
611                 <max>1</max>
612               </range>
613               <output>fcs/rudder-pos-norm</output>
614             </aerosurface_scale>
615
616         </channel>
617
618         <channel name="Flaps">
619           
620           <switch name="fcs/flap-cmd-switched">
621             <default value="fcs/flap-cmd-static"/>
622             <test value="fcs/flap-cmd-norm">
623               hs/flaps-serviceable > 0
624             </test>
625           </switch>
626
627             <kinematic name="Flaps Control">
628              <input>fcs/flap-cmd-switched</input>
629               <traverse>
630                 <setting>
631                   <position>0</position>
632                   <time>0</time>
633                 </setting>
634                 <setting>
635                   <position>15</position>
636                   <time>7</time>
637                 </setting>
638                 <setting>
639                   <position>28</position>
640                   <time>8</time>
641                 </setting>
642                 <setting>
643                   <position>45</position>
644                   <time>12</time>
645                 </setting>
646               </traverse>
647               <output>fcs/flap-pos-deg</output>
648             </kinematic>
649             
650             <aerosurface_scale name="Flap Position Normalizer">
651               <input>fcs/flap-pos-deg</input>
652               <domain>
653                 <min>0</min>  <!-- Flaps actual minimum position -->
654                 <max>45</max>  <!-- Flaps actual maximum position -->
655               </domain>
656               <range>
657                 <min>0</min>  <!-- Flaps normalized minimum position -->
658                 <max>1</max>  <!-- Flaps normalized maximum position -->
659               </range>
660               <output>fcs/flap-pos-norm</output>
661             </aerosurface_scale>
662         </channel>
663
664         <channel name="Landing Gear">
665           
666           <switch name="gear/gear-cmd-switched">
667             <default value="gear/gear-cmd-static"/>
668             <test value="gear/gear-cmd-norm">
669               hs/hs1-busters-ok > 0
670             </test>
671           </switch>
672
673             <kinematic name="Gear Control">
674               <input>gear/gear-cmd-norm</input>
675               <!--<input>gear/gear-cmd-switched</input>-->
676               <traverse>
677                 <setting>
678                   <position>0</position>
679                   <time>0</time>
680                 </setting>
681                 <setting>
682                   <position>1</position>
683                   <time>7</time>
684                 </setting>
685               </traverse>
686               <output>gear/gear-pos-norm</output>
687             </kinematic>
688
689         </channel>
690
691         <channel name="Speedbrake">
692
693           
694           <pure_gain name="Speedbrake outer">
695             <input>fcs/spoiler-cmd-norm</input>
696             <gain>0.4</gain>
697           </pure_gain>
698
699           
700           <switch name="Wow">
701             <default value="0.0"/>
702             <test value="1.0">
703               forces/fbz-gear-lbs lt -1000
704             </test>
705           </switch>
706           
707           <switch name="revers on ground">
708             <default value="0.0"/>
709             <test value="fcs/wow">
710               propulsion/engine[0]/reverser-angle-rad gt 0.1
711             </test>
712           </switch>
713
714           <switch name="rejected takeoff">
715             <default value="0.0"/>
716             <test value="1.0">
717               fcs/flap-pos-deg gt 10
718               fcs/revers-on-ground gt 0
719             </test>
720           </switch>
721
722           <switch name="normal landing">
723             <default value="0.0"/>
724             <test value="1.0">
725               fcs/flap-pos-deg gt 30
726               fcs/revers-on-ground gt 0.5
727               fcs/throttle-cmd-norm[0] lt fcs/revers-1-limit
728               fcs/throttle-cmd-norm[1] lt fcs/revers-1-limit
729               fcs/throttle-cmd-norm[2] lt fcs/revers-1-limit
730               fcs/throttle-cmd-norm[0] gt fcs/revers-2-limit
731               fcs/throttle-cmd-norm[1] gt fcs/revers-2-limit
732               fcs/throttle-cmd-norm[2] gt fcs/revers-2-limit
733             </test>
734           </switch>
735           
736           <summer name="Speedbrake cmd">
737             <input>fcs/speedbrake-outer</input>
738             <input>fcs/rejected-takeoff</input>
739             <input>fcs/normal-landing</input>
740             <clipto>
741               <min>0.0</min>
742               <max>1.0</max>
743             </clipto>
744           </summer>
745           
746           <switch name="fcs/speedbrake-cmd-switched">
747             <default value="fcs/speedbrake-cmd-static"/>
748             <test value="fcs/speedbrake-cmd">
749               hs/hs1-busters-ok > 0
750             </test>
751           </switch>
752           
753           
754             <kinematic name="Speedbrake Control">
755               <input>fcs/speedbrake-cmd-switched</input>
756               <traverse>
757                 <setting>
758                   <position>0</position>
759                   <time>0</time>
760                 </setting>
761                 <setting>
762                   <position>1</position>
763                   <time>0.5</time>
764                 </setting>
765               </traverse>
766               <output>fcs/speedbrake-pos-norm</output>
767             </kinematic>
768
769         </channel>
770
771         <channel name="Stabilizer">
772
773           <scheduled_gain name="Stabilizer Auto Pos">
774             <input>fcs/stab-auto-cmd</input>
775             <table>
776               <independentVar> fcs/flap-pos-deg </independentVar>
777               <tableData>
778                 0             0
779                 28            0.2727
780                 45            0.5454
781               </tableData>
782             </table>
783             <clipto>
784               <min>0.0</min>
785               <max>1.0</max>
786             </clipto>
787           </scheduled_gain>     
788           
789           <switch name="Stabilizer Cmd">
790             <default value="fcs/stabilizer-auto-pos"/>
791             <test value="fcs/stab-manu-cmd">
792               fcs/stab-manu-switch eq 1.0
793             </test>
794           </switch>
795           
796             <kinematic name="Stabilizer Control">
797             <input>fcs/stabilizer-cmd</input>
798 <!--<input>fcs/stabilizer-cmd-norm</input>-->
799               <traverse>
800                 <setting>
801                   <position>0.0</position>
802                   <time>0</time>
803                 </setting>
804                 <setting>
805                   <position>0.09602</position>
806                   <time>15</time>
807                 </setting>
808               </traverse>
809             </kinematic>
810             
811             <summer name="Stabilizer rad">
812               <bias>0.02618</bias>
813               <input>fcs/stabilizer-control</input>
814               <output>fcs/stabilizer-pos-rad</output>
815             </summer>
816     
817             <aerosurface_scale name="Stabilizer Normalizer">
818               <input>fcs/stabilizer-pos-rad</input>
819               <domain>
820                 <min>-1</min> 
821                 <max>1</max>
822               </domain>
823               <range>
824                 <min>-1</min>
825                 <max>1</max>
826               </range>
827               <output>fcs/right-aileron-pos-norm</output>
828             </aerosurface_scale>
829
830         </channel>
831         
832         <channel name="Brake">
833 <!--Left-->
834           <summer name="gear/left-brake-cmd-norm">
835             <input>gear/brake-left</input>
836             <input>gear/brake-parking</input>
837             <clipto>
838               <min>0.0</min>
839               <max>1.0</max>
840             </clipto>
841           </summer>
842           
843           <pure_gain name="gear/left-brake-cmd">
844             <input>gear/left-brake-cmd-norm</input>
845   <!--You can change current static friction here, for model of ice condition etc. -->
846             <gain>gear/static-friction</gain> <!--default: 0.6 --> 
847           </pure_gain>
848 <!--Check hydro power for brake-->
849           <switch name="gear/left-brake-cmd-switched">
850             <default value="0.0"/>
851             <test value="gear/left-brake-cmd">
852               hs/hs1-busters-ok > 0
853             </test>
854             <output>fcs/left-brake-cmd-norm</output>
855           </switch>
856 <!--Right-->
857           <summer name="gear/right-brake-cmd-norm">
858             <input>gear/brake-right</input>
859             <input>gear/brake-parking</input>
860             <clipto>
861               <min>0.0</min>
862               <max>1.0</max>
863             </clipto>
864           </summer>
865           
866           <pure_gain name="gear/right-brake-cmd">
867             <input>gear/right-brake-cmd-norm</input>
868             <gain>gear/static-friction</gain>
869           </pure_gain>
870           
871           <switch name="gear/right-brake-cmd-switched">
872             <default value="0.0"/>
873             <test value="gear/right-brake-cmd">
874               hs/hs1-busters-ok > 0
875             </test>
876             <output>fcs/right-brake-cmd-norm</output>
877           </switch>
878           
879         </channel>
880
881         <channel name="Steering">
882           
883           <switch name="gear/steering-switched">
884             <default value="hs/hs2-busters-ok"/>
885             <test value="gear/steering">
886               systems/electrical-ok == 1
887             </test>
888           </switch>
889           
890           <switch name="gear/nose-wheel-steering-switched">
891             <default value="hs/hs2-busters-ok"/>
892             <test value="gear/nose-wheel-steering">
893               systems/electrical-ok == 1
894             </test>
895           </switch>
896           
897           <scheduled_gain name="gear/steering-cmd-norm">
898             <input>-fcs/rudder-cmd-norm</input>
899             <table>
900               <independentVar> gear/steering-switched </independentVar>
901               <tableData>
902                 10            0.158
903                 63            1.0
904               </tableData>
905             </table>
906           </scheduled_gain>     
907           
908           <pure_gain name="gear/steering-cmd-norm-switched">
909             <input>gear/steering-cmd-norm</input>
910             <gain>gear/nose-wheel-steering-switched</gain>
911           </pure_gain>
912           
913           <pure_gain name="gear/steering-cmd-norm-switched-deg">
914             <input>gear/steering-cmd-norm-switched</input>
915             <gain>63.0</gain>
916             <output>fcs/steer-pos-deg</output>
917           </pure_gain>
918
919         </channel>
920
921     </flight_control>
922     
923     <system file="fdm_globals"/>
924     <system file="engines"/>
925     <system file="hydrosystems"/>
926     <system file="instrumentation"/>
927     <system file="nvu"/>
928     <system file="pushback"/>
929     <autopilot file="Systems/absu154"/>
930 <!--    <autopilot file="absu154"/>-->
931     
932     <aerodynamics>
933 <!--    
934         <function name="aero/function/fly_fuel">
935           <product>
936           <sum>
937             <table name="fly_fuel_t">
938                 <independentVar lookup="column">tu154/systems/flight/fl</independentVar>
939                 <independentVar lookup="row">tu154/systems/flight/dist</independentVar>
940                 <tableData>
941                           9600    10200   10800   11400   12100
942                   500     5.5     5.45    5.35    5.35    5.45
943                   1000    8.95    8.5     8.4     8.25    8.3
944                   1500    12.2    11.6    11.5    11.25   11.15
945                   1600    12.8    12.3    12.1    11.85   11.7
946                   1700    13.5    13      12.75   12.5    12.3
947                   1800    14.1    13.65   13.35   13.1    12.85
948                   1900    14.8    14.3    14      13.75   13.45
949                   2000    15.4    15      14.6    14.35   14.05
950                   2100    16.15   15.65   15.25   15      14.75
951                   2200    16.9    16.2    15.85   15.55   15.35
952                   2300    17.5    17      16.5    16.2    15.9
953                   2400    18      17.7    17.1    16.85   16.5
954                   2500    18.8    18.15   17.8    17.55   17.2
955                   2600    19.6    19      18.5    18.2    17.8
956                   2700    20.2    19.6    19.2    18.85   18.4
957                   2800    20.6    20.25   19.65   19.5    19.1
958                   2900    21.15   21      20.45   10.1    19.75
959                   3000    21.7    21.15   20.8    20.75   20.45
960                   3100    21.5    21.8    21.5    21.1    21
961                   3200    22.05   22.35   21.5    21.7    21.3
962                   3300    22.6    23      22.55   22.25   21.85
963                   3400    23.1    23.5    23      22.8    22.35
964                   3500    23.75   24.15   23.6    23.3    22.95
965                   3600    24.25   24.7    24.1    23.85   23.55
966                   3700    24.8    25.36   24.7    24.35   24.05
967                   3800    25.4    25.9    25.3    23.95   24.6
968                   3900    25.9    26.5    25.8    25.45   25.1
969                   4000    26.4    27      26.3    25.95   25.6
970                   4100    27      27.6    26.9    26.55   26.1
971                   4200    27.55   28.2    27.35   27.1    26.6
972                   4300    28.1    28.8    28      27.6    27.05
973                   4400    28.6    29.3    28.5    28.2    27.55
974                   4500    29.2    29.9    29.2    28.7    28.1
975                   4600    29.75   30.45   29.9    29.15   28.6
976                   4700    30.3    31      30.4    29.65   29.15
977                   4800    30.8    31.35   31      30.2    29.65
978                   4900    31.35   32.2    31.5    30.65   30.15
979                   5000    31.85   32.7    31.9    31.15   30.55
980                 </tableData>
981             </table>
982             <value>7</value>
983           </sum>
984           <value>1</value>
985           </product>
986         </function>-->
987       <function name="aero/function/CAX">
988         <product>
989           <difference>
990             <product>
991               <property>inertia/cg-x-in</property>
992               <value>0.0254</value>
993             </product>
994             <value>24.04</value>
995           </difference>
996           <value>18.9215</value>
997         </product>
998       </function>
999
1000         <function name="aero/function/auasp">
1001             <table name="alpha_max">
1002                 <independentVar lookup="row">velocities/mach</independentVar>
1003                 <independentVar lookup="column">fcs/flap-pos-deg</independentVar>
1004                 <tableData>
1005                                0             15            28            45            
1006                   0.4           12            13            12            12            
1007                   0.6           12            13            12            12            
1008                   0.7           8.8           13            12            12            
1009                   0.8           7.8           13            12            12            
1010                   0.85          7.2           13            12            12            
1011                   0.9           6.6           13            12            12            
1012                 </tableData>
1013             </table>
1014         </function>
1015         <function name="aero/function/cmf">
1016             <description>Mach and flaps parameter</description>
1017             <sum>
1018                 <property>fcs/flap-pos-deg</property>
1019                 <product>
1020                     <property>velocities/mach</property>
1021                     <value>-1</value>
1022                 </product>
1023             </sum>
1024         </function>
1025         <function name="aero/function/cy">
1026             <description>Lift due to alpha</description>
1027             <table name="Cy">
1028                 <independentVar lookup="row">aero/alpha-wing-rad</independentVar>
1029                 <independentVar lookup="column">aero/function/cmf</independentVar>
1030                 <tableData>
1031                                -0.95         -0.8          -0.5          0.2           28            45            
1032                   -0.06981      -0.65         -0.65         -0.65         -0.65         0             0.25          
1033                   0             -0.22         -0.2          -0.25         -0.25         0.4           0.65          
1034                   0.04887       0.05          0.1           0.05          0             0.65          0.93          
1035                   0.08727       0.24          0.36          0.3           0.2           0.87          1.15          
1036                   0.1658        0.62          0.8           0.78          0.6           1.3           1.58          
1037                   0.2618        0.78          1             1.19          1.05          1.78          2.08          
1038                   0.2792        0.78          1.01          1.25          1.11          1.85          2.13          
1039                   0.2967        0.75          0.95          1.28          1.18          1.9           2.08          
1040                   0.3316        0.56          0.78          1.25          1.26          1.85          1.7           
1041                   0.3665        0.3           0.5           1.18          1.3           1.7           1.4           
1042                   0.384         0.18          0.35          1.1           1.27          1.6           1.3           
1043                   0.4363        -0.2          -0.1          0.9           1.13          1.3           1             
1044                 </tableData>
1045             </table>
1046         </function>
1047         <axis name="LIFT" unit="LBS">
1048             <function name="aero/coefficient/CLalpha">
1049                 <description>Lift_due_to_alpha</description>
1050                 <product>
1051                     <property>aero/qbar-psf</property>
1052                     <property>metrics/Sw-sqft</property>
1053                     <property>aero/function/cy</property>
1054                 </product>
1055             </function>
1056             <function name="aero/coefficient/dCLsb">
1057                 <description>Delta_Lift_due_to_speedbrake</description>
1058                 <product>
1059                     <property>aero/qbar-psf</property>
1060                     <property>metrics/Sw-sqft</property>
1061                     <property>fcs/speedbrake-pos-norm</property>
1062                     <value>-0.65</value>
1063                 </product>
1064             </function>
1065             <function name="aero/coefficient/CLde">
1066                 <description>Lift_due_to_Elevator_Deflection</description>
1067                 <product>
1068                     <property>aero/qbar-psf</property>
1069                     <property>metrics/Sw-sqft</property>
1070                     <property>fcs/elevator-pos-rad</property>
1071                     <value>0.2</value>
1072                 </product>
1073             </function>
1074             <function name="aero/coefficient/dCLg">
1075                 <description>Delta_Lift_due_to_gear</description>
1076                 <product>
1077                     <property>aero/qbar-psf</property>
1078                     <property>metrics/Sw-sqft</property>
1079                     <property>gear/gear-pos-norm</property>
1080                     <value>-0.06</value>
1081                 </product>
1082             </function>
1083             <function name="aero/coefficient/CLground">
1084                 <description>Lift near ground</description>
1085                 <product>
1086                     <table name="Delta lift due ground reaction">
1087                         <independentVar>position/h-agl-ft</independentVar>
1088                         <tableData>
1089                           0             0.13        
1090                           10            0.1         
1091                           27            0           
1092                         </tableData>
1093                     </table>
1094                     <property>aero/qbar-psf</property>
1095                     <property>metrics/Sw-sqft</property>
1096                 </product>
1097             </function>
1098             
1099         </axis>
1100         <axis name="DRAG" unit="LBS">
1101             <function name="aero/coefficient/CDx">
1102                 <description>Drag_due_to_Cy</description>
1103                 <product>
1104                     <property>aero/qbar-psf</property>
1105                     <property>metrics/Sw-sqft</property>
1106                     <table name="Cx">
1107                         <independentVar lookup="row">aero/function/cy</independentVar>
1108                         <independentVar lookup="column">aero/function/cmf</independentVar>
1109                         <tableData>
1110                                        -0.95         -0.9          -0.6          0.2           28            45            
1111                           -0.25         0.032         0.028         0.025         0.025         0.11          0.2           
1112                           0             0.04          0.028         0.025         0.022         0.11          0.2           
1113                           0.25          0.05          0.037         0.027         0.025         0.11          0.2           
1114                           0.5           0.3           0.07          0.034         0.032         0.113         0.2           
1115                           0.75          1.7           0.3           0.049         0.05          0.125         0.202         
1116                           1             2.5           1             0.08          0.095         0.14          0.21          
1117                           1.05          2.6           1.2           0.1           0.12          0.145         0.212         
1118                           1.25          2.9           2             0.35          0.27          0.17          0.227         
1119                           1.5           3             2.5           1             0.6           0.205         0.263         
1120                           1.7           3             2.5           2             1             0.24          0.3           
1121                         </tableData>
1122                     </table>
1123                 </product>
1124             </function>
1125             <function name="aero/coefficient/CDgear">
1126                 <description>Drag_due_to_gear</description>
1127                 <product>
1128                     <property>aero/qbar-psf</property>
1129                     <property>metrics/Sw-sqft</property>
1130                     <property>gear/gear-pos-norm</property>
1131                     <value>0.0155</value>
1132                 </product>
1133             </function>
1134             <function name="aero/coefficient/CDsb">
1135                 <description>Drag_due_to_speedbrakes</description>
1136                 <product>
1137                     <property>aero/qbar-psf</property>
1138                     <property>metrics/Sw-sqft</property>
1139                     <property>fcs/speedbrake-pos-norm</property>
1140                     <value>0.019</value>
1141                 </product>
1142             </function>
1143             <function name="aero/coefficient/CDbeta">
1144                 <description>Drag_due_to_sideslip</description>
1145                 <product>
1146                     <property>aero/qbar-psf</property>
1147                     <property>metrics/Sw-sqft</property>
1148                     <table>
1149                         <independentVar>aero/beta-rad</independentVar>
1150                         <tableData>
1151                           -1.57         1.23        
1152                           -0.26         0.05        
1153                           0             0           
1154                           0.26          0.05        
1155                           1.57          1.23        
1156                         </tableData>
1157                     </table>
1158                 </product>
1159             </function>
1160             <function name="aero/coefficient/CDde">
1161                 <description>Drag_due_to_Elevator_Deflection</description>
1162                 <product>
1163                     <property>aero/qbar-psf</property>
1164                     <property>metrics/Sw-sqft</property>
1165                     <abs>
1166                       <property>fcs/elevator-pos-norm</property>
1167                     </abs>
1168                     <value>0.01</value>
1169                 </product>
1170             </function>
1171             <function name="aero/coefficient/CDground">
1172                 <description>Drag near ground</description>
1173                 <product>
1174                     <table name="Delta drag due ground reaction">
1175                         <independentVar>position/h-agl-ft</independentVar>
1176                         <tableData>
1177                           0             -0.01       
1178                           10            -0.008      
1179                           27            0           
1180                         </tableData>
1181                     </table>
1182                     <property>aero/qbar-psf</property>
1183                     <property>metrics/Sw-sqft</property>
1184                 </product>
1185             </function>
1186         </axis>
1187         <axis name="SIDE" unit="LBS">
1188             <function name="aero/coefficient/CYb">
1189                 <description>Side_force_due_to_beta</description>
1190                 <product>
1191                     <property>aero/qbar-psf</property>
1192                     <property>metrics/Sw-sqft</property>
1193                     <property>aero/beta-rad</property>
1194                     <table name="side force due flaps">
1195                         <independentVar>fcs/flap-pos-deg</independentVar>
1196                         <tableData>
1197                           0             -0.859      
1198                           28            -1.031      
1199                           45            -1.146      
1200                         </tableData>
1201                     </table>
1202                 </product>
1203             </function>
1204             <function name="aero/coefficient/CYr">
1205                 <description>Side_force_due_rudder</description>
1206                 <product>
1207                     <property>aero/qbar-psf</property>
1208                     <property>metrics/Sw-sqft</property>
1209                     <property>fcs/rudder-pos-rad</property>
1210                     <value>-0.1776</value>
1211                 </product>
1212             </function>
1213         </axis>
1214         <axis name="ROLL" unit="LBS*FT">
1215             <function name="aero/coefficient/Clb">
1216                 <description>Roll_moment_due_to_beta</description>
1217                 <product>
1218                     <property>aero/qbar-psf</property>
1219                     <property>metrics/Sw-sqft</property>
1220                     <property>metrics/bw-ft</property>
1221                     <property>aero/beta-rad</property>
1222                     <table name="Roll due beta">
1223                         <independentVar lookup="row">aero/alpha-wing-rad</independentVar>
1224                         <independentVar lookup="column">fcs/flap-pos-deg</independentVar>
1225                         <tableData>
1226                                        0             28            45            
1227                           0             -0.00135      -0.003        -0.0034       
1228                           0.08727       -0.0017       -0.0033       -0.00375      
1229                           0.17453       -0.0019       -0.0036       -0.004        
1230                           0.2678        -0.0025       -0.0037       -0.0048       
1231                         </tableData>
1232                     </table>
1233                 </product>
1234             </function>
1235             <function name="aero/coefficient/Clp">
1236                 <description>Roll_moment_due_to_roll_rate</description>
1237                 <product>
1238                     <property>aero/qbar-psf</property>
1239                     <property>metrics/Sw-sqft</property>
1240                     <property>metrics/bw-ft</property>
1241                     <property>aero/bi2vel</property>
1242                     <property>velocities/p-aero-rad_sec</property>
1243                     <value>-0.5</value>
1244                 </product>
1245             </function>
1246             <function name="aero/coefficient/Clr">
1247                 <description>Roll_moment_due_to_yaw_rate</description>
1248                 <product>
1249                     <property>aero/qbar-psf</property>
1250                     <property>metrics/Sw-sqft</property>
1251                     <property>metrics/bw-ft</property>
1252                     <property>aero/bi2vel</property>
1253                     <property>velocities/r-aero-rad_sec</property>
1254                     <value>0.15</value>
1255                 </product>
1256             </function>
1257             <function name="aero/coefficient/Clda">
1258                 <description>Roll_moment_due_to_aileron</description>
1259                 <product>
1260                     <property>aero/qbar-psf</property>
1261                     <property>metrics/Sw-sqft</property>
1262                     <property>metrics/bw-ft</property>
1263                     <property>fcs/left-aileron-pos-rad</property>
1264                     <table>
1265                         <independentVar>velocities/mach</independentVar>
1266                         <tableData>
1267                           0.15          0.0659      
1268                           0.5           0.0595      
1269                           1             0.03438     
1270                         </tableData>
1271                     </table>
1272                     <value>1.4</value>
1273                 </product>
1274             </function>
1275             <function name="aero/coefficient/Cldr">
1276                 <description>Roll_moment_due_to_rudder</description>
1277                 <product>
1278                     <property>aero/qbar-psf</property>
1279                     <property>metrics/Sw-sqft</property>
1280                     <property>metrics/bw-ft</property>
1281                     <property>fcs/rudder-pos-rad</property>
1282                     <value>-0.01719</value>
1283                 </product>
1284             </function>
1285         </axis>
1286         <axis name="PITCH" unit="LBS*FT">
1287             <function name="aero/coefficient/Cmalpha">
1288                 <description>Pitch_moment_due_to_alpha</description>
1289                 <product>
1290                     <property>aero/qbar-psf</property>
1291                     <property>metrics/Sw-sqft</property>
1292                     <property>metrics/cbarw-ft</property>
1293                     <table name="Ma">
1294                         <independentVar lookup="row">aero/alpha-wing-rad</independentVar>
1295                         <independentVar lookup="column">fcs/flap-pos-deg</independentVar>
1296                         <tableData>
1297                                        0             15            28            45            
1298                           -0.06981      0.275         0.15          0             -0.14         
1299                           0             0.183         0.05          -0.08         -0.213        
1300                           0.06981       0.08          -0.05         -0.18         -0.29         
1301                           0.2618        -0.16         -0.27         -0.375        -0.453        
1302                           0.349         -0.212        -0.325        -0.425        -0.45         
1303                           0.3665        -0.21         -0.32         -0.412        -0.452        
1304                           0.384         -0.19         -0.3          -0.4          -0.425        
1305                         </tableData>
1306                     </table>
1307                     <value>1.25</value>
1308                 </product>
1309             </function>
1310             <function name="aero/coefficient/Cmcg">
1311                 <description>Pitch_moment_due_to_CG_position</description>
1312                 <product>
1313                     <property>aero/qbar-psf</property>
1314                     <property>metrics/Sw-sqft</property>
1315                     <property>metrics/cbarw-ft</property>
1316                     <property>aero/function/cy</property>
1317                     <product>
1318                         <sum>
1319                             <description>CG due 25%MAC</description>
1320                             <property>inertia/cg-x-in</property>
1321                             <value>-998.43</value>
1322                         </sum>
1323                         <value>0.012</value><!--0.0048-->
1324                     </product>
1325                     <value>1</value>
1326                 </product>
1327             </function>
1328             <function name="aero/coefficient/Cmde">
1329                 <description>Pitch_moment_due_to_elevator</description>
1330                 <product>
1331                     <property>aero/qbar-psf</property>
1332                     <property>metrics/Sw-sqft</property>
1333                     <property>metrics/cbarw-ft</property>
1334                     <table name="mme">
1335                         <independentVar>velocities/mach</independentVar>
1336                         <tableData>
1337                           0.4           1           
1338                           0.5           1           
1339                           0.7           1           
1340                           0.786         0.97        
1341                           0.87          0.8461      
1342                           0.9           0.7692      
1343                           0.95          0.5384      
1344                         </tableData>
1345                     </table>
1346                     <table name="cyh">
1347                         <independentVar lookup="row">fcs/elevator-pos-rad</independentVar>
1348                         <independentVar lookup="column">velocities/mach</independentVar>
1349                         <tableData>
1350                                        0             2             
1351                           -0.524        -1            -0.5          
1352                           -0.349        -0.85         -0.49         
1353                           -0.174        -0.5         -0.4          
1354                           0             0             0             
1355                           0.174         0.5          0.4           
1356                           0.349         0.85          0.49          
1357                           0.524         1             0.5           
1358                         </tableData>
1359                     </table>
1360                     <value>-0.7</value><!--0.48-->
1361                 </product>
1362             </function>
1363             <function name="aero/coefficient/Cmq">
1364                 <description>Pitch_moment_due_to_pitch_rate</description>
1365                 <product>
1366                     <property>aero/qbar-psf</property>
1367                     <property>metrics/Sw-sqft</property>
1368                     <property>metrics/cbarw-ft</property>
1369                     <property>aero/ci2vel</property>
1370                     <property>velocities/q-aero-rad_sec</property>
1371                     <value>-15</value>
1372                 </product>
1373             </function>
1374             <function name="aero/coefficient/Cmadot">
1375                 <description>Pitch_moment_due_to_alpha_rate</description>
1376                 <product>
1377                     <property>aero/qbar-psf</property>
1378                     <property>metrics/Sw-sqft</property>
1379                     <property>metrics/cbarw-ft</property>
1380                     <property>aero/ci2vel</property>
1381                     <property>aero/alphadot-rad_sec</property>
1382                     <value>-4</value>
1383                 </product>
1384             </function>
1385             <function name="aero/coefficient/Cstab">
1386                 <description>Pitch moment due to stabilizer position</description>
1387                 <product>
1388                     <property>aero/qbar-psf</property>
1389                     <property>metrics/Sw-sqft</property>
1390                     <property>metrics/cbarw-ft</property>
1391                     <table name="mms">
1392                         <independentVar>velocities/mach</independentVar>
1393                         <tableData>
1394                           0.4           1           
1395                           0.7           1.083       
1396                           0.87          1.2083      
1397                           0.9           1.25        
1398                           0.95          1.1875      
1399                         </tableData>
1400                     </table>
1401                     <table name="cys">
1402                         <independentVar lookup="row">fcs/stabilizer-pos-rad</independentVar>
1403                         <independentVar lookup="column">velocities/mach</independentVar>
1404                         <tableData>
1405                                        0             2             
1406                           -0.524        3.2           1.6           
1407                           -0.349        3.2           1.6           
1408                           -0.174        2.08          1.28          
1409                           0             0             0             
1410                           0.174         -2.08         -1.28         
1411                           0.349         -3.2          -1.6          
1412                           0.524         -3.2          -1.6          
1413                         </tableData>
1414                     </table>
1415                     <value>-0.47</value>
1416                 </product>
1417             </function>
1418         </axis>
1419         <axis name="YAW" unit="LBS*FT">
1420             <function name="aero/coefficient/Cnb">
1421                 <description>Yaw_moment_due_to_beta</description>
1422                 <product>
1423                     <property>aero/qbar-psf</property>
1424                     <property>metrics/Sw-sqft</property>
1425                     <property>metrics/bw-ft</property>
1426                     <property>aero/beta-rad</property>
1427                     <table name="Yaw moment due flaps and Mach">
1428                         <independentVar lookup="row">fcs/flap-pos-deg</independentVar>
1429                         <independentVar lookup="column">velocities/mach</independentVar>
1430                         <tableData>
1431                                        0.1           0.9           
1432                           0             -0.15         -0.218        
1433                           28            -0.2          -0.2934       
1434                           45            -0.24         -0.3518       
1435                         </tableData>
1436                     </table>
1437                     <value>-1</value>
1438                 </product>
1439             </function>
1440             <function name="aero/coefficient/Cnr">
1441                 <description>Yaw_moment_due_to_yaw_rate</description>
1442                 <product>
1443                     <property>aero/qbar-psf</property>
1444                     <property>metrics/Sw-sqft</property>
1445                     <property>metrics/bw-ft</property>
1446                     <property>aero/bi2vel</property>
1447                     <property>velocities/r-aero-rad_sec</property>
1448                     <value>-0.15</value>
1449                 </product>
1450             </function>
1451             <function name="aero/coefficient/Cndr">
1452                 <description>Yaw_moment_due_to_rudder</description>
1453                 <product>
1454                     <property>aero/qbar-psf</property>
1455                     <property>metrics/Sw-sqft</property>
1456                     <property>metrics/bw-ft</property>
1457                     <property>fcs/rudder-pos-rad</property>
1458                     <value>-0.0745</value>
1459                 </product>
1460             </function>
1461         </axis>
1462     </aerodynamics>
1463     
1464     <external_reactions>
1465       <force name="pushback" frame="BODY">
1466         <location unit="IN">
1467         <x>  -139 </x>
1468         <y>    0.0 </y>
1469         <z>  -71.0 </z>
1470         </location>
1471         <direction>
1472         <x>1</x>
1473         <y>0</y>
1474         <z>0</z>
1475         </direction>
1476       </force>
1477    </external_reactions>
1478 <!--    
1479     <output name="tu-fldata.csv" type="CSV" rate="1">
1480         <simulation> OFF </simulation>
1481         <atmosphere> OFF </atmosphere>
1482         <massprops> OFF </massprops>
1483         <aerosurfaces> ON </aerosurfaces>
1484         <rates> OFF </rates>
1485         <velocities> ON </velocities>
1486         <forces> OFF </forces>
1487         <moments> OFF </moments>
1488         <position> ON </position>
1489         <coefficients> OFF </coefficients>
1490         <ground_reactions> OFF </ground_reactions>
1491         <fcs> OFF </fcs>
1492         <propulsion> ON </propulsion>
1493         <property>velocities/v-down-fps</property>
1494         <property>velocities/vc-fps</property>
1495         <property>fcs/flap-pos-deg</property>
1496         <property>ap/speed-pid</property>
1497         <property>ap/speed-error-switched</property>
1498         <property>instrumentation/pnp-heading</property>
1499         <property>ap/gs-trigger</property>
1500         <property>ap/gs-pid</property>
1501         <property>ap/gs-error-switched</property>
1502         <property>ap/gs-error</property>
1503     </output>
1504     -->
1505   </fdm_config>