Prevent negative drag
[fg:toms-fgdata.git] / Aircraft / fkdr1 / dr1.xml
1 <?xml version="1.0"?>
2 <?xml-stylesheet type="text/xsl" href="http://jsbsim.sourceforge.net/JSBSim.xsl"?>
3 <fdm_config name="Fokker Dr.1" 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> Ron Jensen, Erik Hofman, Aeromatic v 0.9 </author>
9   <filecreationdate> 2008-07-26 </filecreationdate>
10   <version>$Revison: $</version>
11   <description> Models a Fokker Dr.1. </description>
12  </fileheader>
13
14 <!--
15   File:     Fokker Dr.1.xml
16   Inputs:
17     name:          Fokker Dr.1
18     type:          WW1 type
19     max weight:    1292.13 lb
20     wing span:     23.6232 ft
21     length:        18.93137 ft
22     wing area:     201.3055 sq-ft
23     gear type:     taildragger
24     retractable?:  no
25     # engines:     1
26     engine type:   piston
27     engine layout: forward fuselage
28     yaw damper?    no
29
30   Outputs:
31     wing loading:  6.42 lb/sq-ft
32     CL-alpha:      5 per radian
33     CL-0:          0.25
34     CL-max:        1.4
35     CD-0:          0.0323
36     K:             0.04
37
38 -->
39
40  <metrics>
41    <wingarea  unit="FT2">  201.31 </wingarea>
42    <wingspan  unit="FT" >   23.62 </wingspan>
43    <wing_incidence>          2.00 </wing_incidence>
44    <chord     unit="FT" >    8.52 </chord>
45    <htailarea unit="FT2">   32.21 </htailarea>
46    <htailarm  unit="FT" >    9.84 </htailarm>
47    <vtailarea unit="FT2">   20.13 </vtailarea>
48    <vtailarm  unit="FT" >    9.47 </vtailarm>
49    <location name="AERORP" unit="IN">
50      <x>   0.00</x>
51      <y>   0.00 </y>
52      <z>   0.00 </z>
53    </location>
54    <location name="EYEPOINT" unit="IN">
55      <x>  29.53 </x>
56      <y> -18.00 </y>
57      <z>  45.00 </z>
58    </location>
59    <location name="VRP" unit="IN">
60      <x>0</x>
61      <y>0</y>
62      <z>0</z>
63    </location>
64  </metrics>
65
66  <mass_balance>
67    <ixx unit="SLUG*FT2">    368.55 </ixx>
68    <iyy unit="SLUG*FT2">    522.24 </iyy>
69    <izz unit="SLUG*FT2">    731.37 </izz>
70    <emptywt unit="LBS" >       775 </emptywt>
71    <location name="CG" unit="IN">
72      <x>   0.00 </x>
73      <y>   0.00 </y>
74      <z>  -5.68 </z>
75    </location>
76  </mass_balance>
77
78  <ground_reactions>
79
80   <contact type="BOGEY" name="LEFT_MAIN">
81    <location unit="IN">
82      <x>  -8.5 </x>
83      <y> -30.59 </y>
84      <z> -69.60 </z>
85    </location>
86    <static_friction>  0.80 </static_friction>
87    <dynamic_friction> 0.50 </dynamic_friction>
88    <rolling_friction> 0.02 </rolling_friction>
89    <spring_coeff unit="LBS/FT">      1000 </spring_coeff>
90    <damping_coeff unit="LBS/FT/SEC">  500 </damping_coeff>
91    <max_steer unit="DEG">0</max_steer>
92    <brake_group>NONE</brake_group>
93    <retractable>FIXED</retractable>
94  </contact>
95
96   <contact type="BOGEY" name="RIGHT_MAIN">
97    <location unit="IN">
98      <x>  -8.5 </x>
99      <y>  30.59 </y>
100      <z> -69.60 </z>
101    </location>
102    <static_friction>  0.80 </static_friction>
103    <dynamic_friction> 0.50 </dynamic_friction>
104    <rolling_friction> 0.02 </rolling_friction>
105    <spring_coeff unit="LBS/FT">       1000 </spring_coeff>
106    <damping_coeff unit="LBS/FT/SEC">   500 </damping_coeff>
107    <max_steer unit="DEG">0</max_steer>
108    <brake_group>NONE</brake_group>
109    <retractable>FIXED</retractable>
110  </contact>
111
112   <contact type="BOGEY" name="TAIL">
113    <location unit="IN">
114      <x> 157.48 </x>
115      <y>   0.00 </y>
116      <z> -26.85 </z>
117    </location>
118    <static_friction>  0.80 </static_friction>
119    <dynamic_friction> 0.50 </dynamic_friction>
120    <rolling_friction> 0.02 </rolling_friction>
121    <spring_coeff unit="LBS/FT">       200 </spring_coeff>
122    <damping_coeff unit="LBS/FT/SEC">  100 </damping_coeff>
123    <max_steer unit="DEG"> 0.00 </max_steer>
124    <brake_group>NONE</brake_group>
125    <retractable>FIXED</retractable>
126  </contact>
127
128   <contact type="STRUCTURE" name="LEFT_WING">
129     <location unit="IN">
130      <x>   22.4 </x>
131      <y> -108.8 </y>
132      <z>  -34.8 </z>
133     </location>
134     <static_friction>  0.80 </static_friction>
135     <dynamic_friction> 0.50 </dynamic_friction>
136     <spring_coeff unit="LBS/FT">        300 </spring_coeff>
137     <damping_coeff unit="LBS/FT/SEC">   150 </damping_coeff>
138  </contact>
139
140   <contact type="STRUCTURE" name="RIGHT_WING">
141     <location unit="IN">
142      <x>   22.4 </x>
143      <y>  108.8 </y>
144      <z>  -34.8 </z>
145     </location>
146     <static_friction>  0.80 </static_friction>
147     <dynamic_friction> 0.50 </dynamic_friction>
148     <spring_coeff unit="LBS/FT">        300 </spring_coeff>
149     <damping_coeff unit="LBS/FT/SEC">   150 </damping_coeff>
150  </contact>
151
152  </ground_reactions>
153
154  <propulsion>
155
156    <engine file="Oberursel-UrII">
157     <location unit="IN">
158       <x> -25.00 </x>
159       <y> -15.80 </y>
160       <z>   0.00 </z>
161     </location>
162     <orient unit="DEG">
163       <pitch> 0.00 </pitch>
164       <roll>   0.00 </roll>
165       <yaw>   0.00 </yaw>
166     </orient>
167     <feed>0</feed>
168     <thruster file="Dr1_propeller">
169      <location unit="IN">
170        <x> -36.36 </x>
171        <y> -15.80 </y>
172        <z>   0.00 </z>
173      </location>
174      <orient unit="DEG">
175        <pitch> 0.00 </pitch>
176        <roll>   0.00 </roll>
177        <yaw>   0.00 </yaw>
178      </orient>
179     </thruster>
180   </engine>
181
182   <tank type="FUEL" number="0">
183      <location unit="IN">
184        <x>   0.04 </x>
185        <y>   0.00 </y>
186        <z>  -5.68 </z>
187      </location>
188      <capacity unit="LBS"> 100.00 </capacity>
189      <contents unit="LBS">  50.00 </contents>
190   </tank>
191
192  </propulsion>
193
194  <flight_control name="FCS: Fokker Dr.1">
195
196   <channel name="Pitch">
197    <summer name="Pitch Trim Sum">
198       <input>fcs/elevator-cmd-norm</input>
199       <input>fcs/pitch-trim-cmd-norm</input>
200       <clipto>
201         <min> -1 </min>
202         <max>  1 </max>
203       </clipto>
204    </summer>
205
206    <aerosurface_scale name="Elevator Control">
207       <input>fcs/pitch-trim-sum</input>
208       <range>
209         <min> -0.35 </min>
210         <max>  0.35 </max>
211       </range>
212       <output>fcs/elevator-pos-rad</output>
213    </aerosurface_scale>
214
215    <aerosurface_scale name="elevator normalization">
216       <input>fcs/elevator-pos-rad</input>
217       <domain>
218         <min> -0.31 </min>
219         <max>  0.26 </max>
220       </domain>
221       <range>
222         <min> -1 </min>
223         <max>  1 </max>
224       </range>
225       <output>fcs/elevator-pos-norm</output>
226    </aerosurface_scale>
227
228   </channel>
229
230   <channel name="Roll">
231    <summer name="Roll Trim Sum">
232       <input>fcs/aileron-cmd-norm</input>
233       <input>fcs/roll-trim-cmd-norm</input>
234       <clipto>
235         <min> -1 </min>
236         <max>  1 </max>
237       </clipto>
238    </summer>
239
240    <aerosurface_scale name="Left Aileron Control">
241       <input>fcs/roll-trim-sum</input>
242       <range>
243         <min> -0.30 </min>
244         <max>  0.30 </max>
245       </range>
246       <output>fcs/left-aileron-pos-rad</output>
247    </aerosurface_scale>
248
249    <aerosurface_scale name="Right Aileron Control">
250       <input>fcs/roll-trim-sum</input>
251       <range>
252         <min> -0.30 </min>
253         <max>  0.30 </max>
254       </range>
255       <output>fcs/right-aileron-pos-rad</output>
256    </aerosurface_scale>
257
258    <aerosurface_scale name="left aileron normalization">
259       <input>fcs/left-aileron-pos-rad</input>
260       <domain>
261         <min> -0.30 </min>
262         <max>  0.30 </max>
263       </domain>
264       <range>
265         <min> -1 </min>
266         <max>  1 </max>
267       </range>
268       <output>fcs/left-aileron-pos-norm</output>
269    </aerosurface_scale>
270
271    <aerosurface_scale name="right aileron normalization">
272       <input>fcs/right-aileron-pos-rad</input>
273       <domain>
274         <min> -0.30 </min>
275         <max>  0.30 </max>
276       </domain>
277       <range>
278         <min> -1 </min>
279         <max>  1 </max>
280       </range>
281       <output>fcs/right-aileron-pos-norm</output>
282    </aerosurface_scale>
283
284   </channel>
285
286   <channel name="Yaw">
287    <summer name="Rudder Command Sum">
288       <input>fcs/rudder-cmd-norm</input>
289       <input>fcs/yaw-trim-cmd-norm</input>
290       <clipto>
291         <min> -0.35 </min>
292         <max>  0.35 </max>
293       </clipto>
294    </summer>
295
296    <aerosurface_scale name="Rudder Control">
297       <input>fcs/rudder-command-sum</input>
298       <range>
299         <min> -0.44 </min>
300         <max>  0.44 </max>
301       </range>
302       <output>fcs/rudder-pos-rad</output>
303    </aerosurface_scale>
304
305    <aerosurface_scale name="rudder normalization">
306       <input>fcs/rudder-pos-rad</input>
307       <domain>
308         <min> -0.44 </min>
309         <max>  0.44 </max>
310       </domain>
311       <range>
312         <min> -1 </min>
313         <max>  1 </max>
314       </range>
315       <output>fcs/rudder-pos-norm</output>
316    </aerosurface_scale>
317
318   </channel>
319
320  </flight_control>
321
322  <aerodynamics>
323
324   <axis name="LIFT">
325     <!--
326        CLadot:  0.759 (/rad)
327        CLq:     1.245 (/rad)
328      -->
329
330     <function name="aero/coefficient/CLalpha">
331       <description>Lift_due_to_alpha</description>
332       <product>
333           <property>aero/qbar-psf</property>
334           <property>metrics/Sw-sqft</property>
335           <table>
336             <independentVar lookup="row">aero/alpha-deg</independentVar>
337             <tableData>
338                 -180.000000    0
339                 -167.283800    0.507559
340                 -165.091352    0.503240
341                 -160.267966    0.460043
342                 -158.075518    0.451404
343                 -155.883069    0.460043
344                 -150.182704    0.498920
345                 -140.535932    0.498920
346                 -124.311815    0.451404
347                 -113.349574    0.356371
348                 -103.702801    0.239741
349                 -94.056029     0.084233
350                 -85.000000     -0.053212
351                 -83.000000     -0.075185
352                 -79.000000     -0.119132
353                 -75.000000     -0.163079
354                 -71.000000     -0.207027
355                 -67.000000     -0.250974
356                 -63.000000     -0.294921
357                 -59.000000     -0.330791
358                 -55.000000     -0.362833
359                 -51.000000     -0.394875
360                 -49.000000     -0.410896
361                 -45.000000     -0.442939
362                 -43.000000     -0.458960
363                 -41.000000     -0.474981
364                 -39.000000     -0.492972
365                 -35.000000     -0.530579
366                 -31.000000     -0.568186
367                 -29.000000     -0.586989
368                 -27.000000     -0.605792
369                 -25.000000     -0.620705
370                 -23.000000     -0.633666
371                 -21.000000     -0.619398
372                 -19.000000     -0.593683
373                 -17.000000     -0.562693
374                 -15.000000     -0.531727
375                 -13.000000     -0.506665
376                 -11.000000     -0.430152
377                 -9.000000      -0.305751
378                 -7.000000      -0.181350
379                 -5.000000      -0.056949
380                 -3.000000       0.067354
381                 -1.000000       0.191575
382                 1.000000        0.315796
383                 3.000000        0.440017
384                 5.000000        0.564237
385                 7.000000        0.689083
386                 9.000000        0.814508
387                 11.000000       0.927432
388                 13.000000       1.016563
389                 15.000000       1.074647
390                 17.000000       1.044252
391                 19.000000       0.916713
392                 21.000000       0.742705
393                 23.000000       0.655686
394                 25.000000       0.615506
395                 27.000000       0.592442
396                 29.000000       0.569378
397                 31.000000       0.552969
398                 33.000000       0.542580
399                 35.000000       0.532191
400                 37.000000       0.521802
401                 39.000000       0.511413
402                 41.000000       0.499081
403                 43.000000       0.486002
404                 45.000000       0.472923
405                 47.000000       0.459843
406                 49.000000       0.446764
407                 51.000000       0.433685
408                 53.000000       0.420605
409                 55.000000       0.406311
410                 57.000000       0.388495
411                 59.000000       0.370678
412                 61.000000       0.352862
413                 63.000000       0.335045
414                 65.000000       0.317229
415                 67.000000       0.299343
416                 69.000000       0.276179
417                 71.000000       0.253014
418                 73.000000       0.229849
419                 75.000000       0.206684
420                 77.000000       0.183520
421                 79.000000       0.160355
422                 81.000000       0.135592
423                 83.000000       0.105045
424                 85.000000       0.074498
425                 90.548112       0.002160
426                 104.141291      -0.218143
427                 122.119367      -0.399568
428                 136.589525      -0.455724
429                 150.621194      -0.451404
430                 155.883069      -0.416847
431                 157.637028      -0.412527
432                 159.390987      -0.425486
433                 163.775883      -0.455724
434                 165.968331      -0.468683
435                 167.722290      -0.447084
436                 180.000000      0
437             </tableData>
438           </table>
439       </product>
440     </function>
441
442     <function name="aero/coefficient/CLde">
443        <description>Lift_due_to_Elevator_Deflection</description>
444        <product>
445            <property>aero/qbar-psf</property>
446            <property>metrics/Sw-sqft</property>
447            <property>fcs/elevator-pos-rad</property>
448            <value>0.2</value>
449        </product>
450     </function>
451
452   </axis>
453
454   <axis name="DRAG">
455     <!--
456        CDo:     0.0323  [x]
457        CDde:    0.0136  [x]
458        CDK:     0.0922
459      -->
460     <function name="aero/coefficient/CD0">
461        <description>Drag_at_zero_lift</description>
462        <product>
463           <property>aero/qbar-psf</property>
464           <property>metrics/Sw-sqft</property>
465           <value>0.0323</value>
466        </product>
467     </function>
468
469     <function name="aero/coefficient/CDi">
470        <description>Induced_drag</description>
471          <product>
472            <property>aero/qbar-psf</property>
473            <property>metrics/Sw-sqft</property>
474            <property>aero/cl-squared</property>
475            <table>
476             <independentVar lookup="row">aero/alpha-deg</independentVar>
477             <tableData>
478                 -180.000000     0.036717
479                 -169.914738     0.062635
480                 -150.182704     0.153348
481                 -122.119367     0.265659
482                 -84.847747      0.408207
483                 -45.383678      0.533477
484                 -43.000000      0.527482
485                 -41.000000      0.530885
486                 -39.000000      0.534288
487                 -37.000000      0.528571
488                 -35.000000      0.513248
489                 -33.000000      0.497924
490                 -31.000000      0.482600
491                 -29.000000      0.467276
492                 -27.000000      0.451953
493                 -25.000000      0.416920
494                 -23.000000      0.374764
495                 -21.000000      0.332608
496                 -19.000000      0.290452
497                 -17.000000      0.238177
498                 -15.000000      0.175336
499                 -13.000000      0.085176
500                 -11.000000      0.029907
501                 -9.000000       0.002152
502                 -7.000000       0.001623
503                 -5.000000       0.001818
504                 -3.000000       0.002013
505                 -1.000000       0.002207
506                 1.000000        0.002402
507                 3.000000        0.002597
508                 5.000000        0.002792
509                 7.000000        0.002986
510                 9.000000        0.003181
511                 11.000000       0.003376
512                 13.000000       0.013600
513                 15.000000       0.032951
514                 17.000000       0.060633
515                 19.000000       0.092297
516                 21.000000       0.123961
517                 23.000000       0.157220
518                 25.000000       0.200529
519                 27.000000       0.243839
520                 29.000000       0.287148
521                 31.000000       0.330457
522                 33.000000       0.364475
523                 35.000000       0.398403
524                 37.000000       0.432331
525                 39.000000       0.466259
526                 41.000000       0.500187
527                 43.000000       0.533927
528                 45.000000       0.551580
529                 47.000000       0.569232
530                 49.000000       0.586885
531                 51.000000       0.604537
532                 53.000000       0.622189
533                 55.000000       0.638904
534                 57.000000       0.645843
535                 59.000000       0.652782
536                 61.000000       0.655156
537                 63.000000       0.645551
538                 65.000000       0.635947
539                 67.000000       0.625216
540                 69.000000       0.603688
541                 71.000000       0.582160
542                 73.000000       0.560632
543                 75.000000       0.539104
544                 77.000000       0.508452
545                 79.147381       0.481641
546                 100.633374      0.334773
547                 132.643118      0.192225
548                 160.706456      0.079914
549                 180.000000      0.036717
550             </tableData>
551           </table>
552          </product>
553     </function>
554
555     <function name="aero/coefficient/CDbeta">
556        <description>Drag_due_to_sideslip</description>
557        <product>
558           <property>aero/qbar-psf</property>
559           <property>metrics/Sw-sqft</property>
560           <table>
561             <independentVar lookup="row">aero/beta-rad</independentVar>
562             <tableData>
563               -1.57    1.230
564               -0.26    0.050
565                0.00    0.000
566                0.26    0.050
567                1.57    1.230
568             </tableData>
569           </table>
570        </product>
571     </function>
572
573     <function name="aero/coefficient/CDde">
574        <description>Drag_due_to_Elevator_Deflection</description>
575        <product>
576            <property>aero/qbar-psf</property>
577            <property>metrics/Sw-sqft</property>
578            <property>fcs/mag-elevator-pos-rad</property>
579            <value>0.0136</value>
580        </product>
581     </function>
582
583   </axis>
584
585   <axis name="SIDE">
586     <!--
587        CYbeta:  -0.3855 (/rad)  [x]
588        CYda:    0
589        CYdr:    0.094 (/rad)    [x]
590        CYp:     -0.01 (/rad)    [x]
591        CYr:     0.1047 (/rad)   [x]
592      -->
593
594     <function name="aero/coefficient/CYb">
595        <description>Side_force_due_to_beta</description>
596        <product>
597            <property>aero/qbar-psf</property>
598            <property>metrics/Sw-sqft</property>
599            <property>aero/beta-rad</property>
600            <value>-0.3855</value>
601        </product>
602     </function>
603
604     <function name="aero/coefficient/CYdr">
605        <description>Side_force_due_to_rudder</description>
606        <product>
607            <property>aero/qbar-psf</property>
608            <property>metrics/Sw-sqft</property>
609            <property>fcs/rudder-pos-rad</property>
610            <value>0.094</value>
611        </product>
612     </function>
613
614     <function name="aero/coefficient/CYp">
615        <description>Side_force_due_to_roll_rate</description>
616        <product>
617            <property>aero/qbar-psf</property>
618            <property>metrics/Sw-sqft</property>
619            <property>aero/bi2vel</property>
620            <property>velocities/p-aero-rad_sec</property>
621            <value>-0.01</value>
622        </product>
623     </function>
624
625     <function name="aero/coefficient/CYr">
626         <description>Side_force_due_to_yaw_rate</description>
627         <product>
628             <property>aero/qbar-psf</property>
629             <property>metrics/Sw-sqft</property>
630             <property>aero/bi2vel</property>
631             <property>velocities/r-aero-rad_sec</property>
632             <value>0.1047</value>
633         </product>
634     </function>
635
636   </axis>
637
638   <axis name="ROLL">
639     <!--
640        Clbeta:  -0.02 (/rad)    [x]
641        Clda:    -0.087 (/rad)   [x]
642        Cldr:    0.005 (/rad)    [x]
643        Clp:     -0.193 (/rad)   [x]
644        Clr:     0.0458 (/rad)   [x]
645     -->
646
647     <function name="aero/coefficient/Clb">
648        <description>Roll_moment_due_to_beta</description>
649        <product>
650            <property>aero/qbar-psf</property>
651            <property>metrics/Sw-sqft</property>
652            <property>metrics/bw-ft</property>
653            <property>aero/beta-rad</property>
654            <value>-0.02</value>
655        </product>
656     </function>
657
658     <function name="aero/coefficient/Clp">
659        <description>Roll_moment_due_to_roll_rate</description>
660        <product>
661            <property>aero/qbar-psf</property>
662            <property>metrics/Sw-sqft</property>
663            <property>metrics/bw-ft</property>
664            <property>aero/bi2vel</property>
665            <property>velocities/p-aero-rad_sec</property>
666            <value>-0.193</value>
667        </product>
668     </function>
669
670     <function name="aero/coefficient/Clr">
671        <description>Roll_moment_due_to_yaw_rate</description>
672        <product>
673            <property>aero/qbar-psf</property>
674            <property>metrics/Sw-sqft</property>
675            <property>metrics/bw-ft</property>
676            <property>aero/bi2vel</property>
677            <property>velocities/r-aero-rad_sec</property>
678            <value>0.458</value>
679        </product>
680     </function>
681
682     <function name="aero/coefficient/Clda">
683        <description>Roll_moment_due_to_aileron</description>
684        <product>
685           <property>aero/qbar-psf</property>
686           <property>metrics/Sw-sqft</property>
687           <property>metrics/bw-ft</property>
688           <property>fcs/left-aileron-pos-rad</property>
689           <value>0.087</value>
690        </product>
691     </function>
692
693     <function name="aero/coefficient/Cldr">
694        <description>Roll_moment_due_to_rudder</description>
695        <product>
696            <property>aero/qbar-psf</property>
697            <property>metrics/Sw-sqft</property>
698            <property>metrics/bw-ft</property>
699            <property>fcs/rudder-pos-rad</property>
700            <value>0.005</value>
701        </product>
702     </function>
703
704   </axis>
705
706   <axis name="PITCH">
707     <!--
708        Cmadot:  -1.122 (/rad)   [x]
709        Cmq:     -1.839 (/rad)   [x]
710     -->
711
712     <function name="aero/coefficient/Cmalpha">
713        <description>Pitch_moment_due_to_alpha</description>
714        <product>
715            <property>aero/qbar-psf</property>
716            <property>metrics/Sw-sqft</property>
717            <property>metrics/cbarw-ft</property>
718            <table>
719             <independentVar lookup="row">aero/alpha-deg</independentVar>
720             <tableData>
721                 180.000000     0.002160
722                 -155.444580    0.049676
723                 -127.381242    0.088553
724                 -84.847747     0.118790
725                 -83.000000     0.111578
726                 -81.000000     0.109529
727                 -79.000000     0.107307
728                 -77.000000     0.104574
729                 -75.000000     0.101924
730                 -73.000000     0.099422
731                 -71.000000     0.097083
732                 -69.000000     0.094282
733                 -67.000000     0.091509
734                 -65.000000     0.088937
735                 -63.000000     0.086618
736                 -61.000000     0.084993
737                 -59.000000     0.084405
738                 -57.000000     0.084065
739                 -55.000000     0.083979
740                 -53.000000     0.084150
741                 -51.000000     0.084585
742                 -49.000000     0.085133
743                 -47.000000     0.084831
744                 -45.000000     0.084135
745                 -43.000000     0.083629
746                 -41.000000     0.083319
747                 -39.000000     0.082857
748                 -37.000000     0.081386
749                 -35.000000     0.078832
750                 -33.000000     0.076293
751                 -31.000000     0.073780
752                 -29.000000     0.070542
753                 -27.000000     0.066352
754                 -25.000000     0.059782
755                 -23.000000     0.052199
756                 -21.000000     0.048019
757                 -19.000000     0.036628
758                 -17.000000     0.008613
759                 -15.000000     -0.021966
760                 -13.000000     -0.051723
761                 -11.000000     -0.061373
762                 -9.000000      -0.055043
763                 -7.000000      -0.042039
764                 -5.000000      -0.030525
765                 -3.000000      -0.020684
766                 -1.000000      -0.012551
767                 1.000000       -0.006150
768                 3.000000       -0.001511
769                 5.000000       0.001345
770                 7.000000       0.002421
771                 9.000000       0.001690
772                 11.000000      -0.001231
773                 13.000000      -0.004202
774                 15.000000      -0.006967
775                 17.000000      -0.015326
776                 19.000000      -0.039137
777                 21.000000      -0.053761
778                 23.000000      -0.057517
779                 25.000000      -0.059092
780                 27.000000      -0.059484
781                 29.000000      -0.057321
782                 31.000000      -0.055292
783                 33.000000      -0.055424
784                 35.000000      -0.055607
785                 37.000000      -0.055193
786                 39.000000      -0.054363
787                 41.000000      -0.053475
788                 43.000000      -0.052650
789                 45.000000      -0.054951
790                 47.000000      -0.057268
791                 49.000000      -0.059612
792                 51.000000      -0.061994
793                 53.000000      -0.063932
794                 55.000000      -0.065632
795                 57.000000      -0.068524
796                 59.000000      -0.071343
797                 61.000000      -0.074801
798                 63.000000      -0.079945
799                 65.000000      -0.084862
800                 67.000000      -0.089696
801                 69.000000      -0.094872
802                 71.000000      -0.099632
803                 73.000000      -0.103974
804                 75.000000      -0.107735
805                 77.000000      -0.111800
806                 79.000000      -0.115339
807                 81.000000      -0.117895
808                 83.000000      -0.116303
809                 85.724726      -0.110151
810                 121.680877     -0.079914
811                 154.567600     -0.041037
812                 180.000000     0.002160
813             </tableData>
814            </table>
815        </product>
816     </function>
817
818     <function name="aero/coefficient/Cmde">
819        <description>Pitch_moment_due_to_elevator</description>
820        <product>
821           <property>aero/qbar-psf</property>
822           <property>metrics/Sw-sqft</property>
823           <property>metrics/cbarw-ft</property>
824           <table>
825             <independentVar lookup="row">aero/alpha-deg</independentVar>
826             <independentVar lookup="column">fcs/elevator-pos-rad</independentVar>
827             <tableData>
828                        -0.35        0           0.35
829               -180.000  0.015374    0.000000    -0.015374
830               -163.145  0.100936    0.081551    0.065508
831               -161.555  0.105615    0.084893    0.063503
832               -159.965  0.103610    0.082219    0.057487
833               -157.420  0.096257    0.076203    0.052807
834               -155.512  0.092914    0.072193    0.056150
835               -153.604  0.100267    0.075535    0.080214
836               -146.608  0.129011    0.106283    0.121658
837               -137.703  0.162433    0.139706    0.145053
838               -124.028  0.187834    0.162433    0.154412
839               -104.947  0.194519    0.172460    0.155080
840               -91.227   0.195800    0.173500    0.153400
841               -71.329   0.193000    0.165200    0.130500
842               -53.688   0.186900    0.150800    0.105100
843               -41.556   0.180900    0.135600    0.071000
844               -34.678   0.176100    0.120200    0.076400
845               -30.176   0.173500    0.113200    0.088700
846               -25.540   0.176700    0.130300    0.084000
847               -22.669   0.171600    0.132500    0.064600
848               -16.566   0.151400    0.117400    0.015500
849               -1.000    0.098300    0.000400    -0.099000
850               6.800     0.042300   -0.040000    -0.136000
851               14.848    -0.015500  -0.117400    -0.151400
852               21.533    -0.064600  -0.132500    -0.171600
853               24.758    -0.084000  -0.130300    -0.176700
854               28.255    -0.088700  -0.113200    -0.173500
855               30.402    -0.076400  -0.120200    -0.176100
856               38.547    -0.071000  -0.135600    -0.180900
857               54.266    -0.105100  -0.150800    -0.186900
858               69.499    -0.130500  -0.165200    -0.193000
859               89.241    -0.153400  -0.173500    -0.195800
860               113.534   -0.154412  -0.172460    -0.194519
861               128.481   -0.145053  -0.162433    -0.187834
862               139.611   -0.121658  -0.139706    -0.162433
863               150.424   -0.080214  -0.106283    -0.129011
864               155.830   -0.056150  -0.075535    -0.100267
865               157.739   -0.052807  -0.072193    -0.092914
866               159.647   -0.057487  -0.076203    -0.096257
867               161.555   -0.063503  -0.082219    -0.103610
868               163.145   -0.065508  -0.084893    -0.105615
869               165.053   -0.059492  -0.081551    -0.100936
870               180.000   0.015374    0.000000    -0.015374
871             </tableData>
872           </table>
873        </product>
874     </function>
875
876     <function name="aero/coefficient/Cmq">
877        <description>Pitch_moment_due_to_pitch_rate</description>
878        <product>
879            <property>aero/qbar-psf</property>
880            <property>metrics/Sw-sqft</property>
881            <property>metrics/cbarw-ft</property>
882            <property>aero/ci2vel</property>
883            <property>velocities/q-aero-rad_sec</property>
884            <value>-1.839</value>
885        </product>
886     </function>
887
888     <function name="aero/coefficient/Cmadot">
889        <description>Pitch_moment_due_to_alpha_rate</description>
890        <product>
891            <property>aero/qbar-psf</property>
892            <property>metrics/Sw-sqft</property>
893            <property>metrics/cbarw-ft</property>
894            <property>aero/ci2vel</property>
895            <property>aero/alphadot-rad_sec</property>
896            <value>-1.122</value>
897        </product>
898     </function>
899
900   </axis>
901
902   <axis name="YAW">
903     <!--
904        Cnbeta:  0.096 (/rad)    [x]
905        Cnda:    0.0552 (/rad)   [x]
906        Cndr:    -0.0502 (/rad)  [x]
907        Cnp:     -0.0109 (/rad)  [x]
908        Cnr:     -0.082 (/rad)   [x]
909      -->
910
911     <function name="aero/coefficient/Cnb">
912        <description>Yaw_moment_due_to_beta</description>
913        <product>
914            <property>aero/qbar-psf</property>
915            <property>metrics/Sw-sqft</property>
916            <property>metrics/bw-ft</property>
917            <property>aero/beta-rad</property>
918            <value>0.096</value>
919        </product>
920     </function>
921
922     <function name="aero/coefficient/Cnp">
923         <description>Yaw_moment_due_to_roll_rate</description>
924         <product>
925             <property>aero/qbar-psf</property>
926             <property>metrics/Sw-sqft</property>
927             <property>metrics/bw-ft</property>
928             <property>aero/bi2vel</property>
929             <property>velocities/p-aero-rad_sec</property>
930             <value>-0.0109</value>
931         </product>
932     </function>
933
934     <function name="aero/coefficient/Cnr">
935        <description>Yaw_moment_due_to_yaw_rate</description>
936        <product>
937            <property>aero/qbar-psf</property>
938            <property>metrics/Sw-sqft</property>
939            <property>metrics/bw-ft</property>
940            <property>aero/bi2vel</property>
941            <property>velocities/r-aero-rad_sec</property>
942            <value>-0.082</value>
943        </product>
944     </function>
945
946     <function name="aero/coefficient/Cndr">
947        <description>Yaw_moment_due_to_rudder</description>
948        <product>
949            <property>aero/qbar-psf</property>
950            <property>metrics/Sw-sqft</property>
951            <property>metrics/bw-ft</property>
952            <property>fcs/rudder-pos-rad</property>
953            <value>-0.0502</value>
954        </product>
955     </function>
956
957     <function name="aero/coefficient/Cnda">
958        <description>Adverse_yaw</description>
959        <product>
960            <property>aero/qbar-psf</property>
961            <property>metrics/Sw-sqft</property>
962            <property>metrics/bw-ft</property>
963            <property>fcs/left-aileron-pos-rad</property>
964            <value>0.0552</value>
965        </product>
966     </function>
967
968   </axis>
969
970  </aerodynamics>
971
972 </fdm_config>