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">53000</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">4000</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">4000</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">4000</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         <pointmass name="Gear shift">
 153             <weight unit="KG">1000</weight>
 154             <location unit="M">
 155                 <x>26.68</x>
 156                 <y>0</y>
 157                 <z>1.8</z>
 158             </location>
 159         </pointmass>
 160     </mass_balance>
 161
 162     <ground_reactions>
 163         <contact type="BOGEY" name="NOSE">
 164             <location unit="M">
 165                 <x> 6.0 </x>
 166                 <y> 0.0 </y>
 167                 <z> -2.7 </z>
 168             </location>
 169             <static_friction> 0.6 </static_friction>
 170             <dynamic_friction> 0.8 </dynamic_friction>
 171             <rolling_friction> 0.02 </rolling_friction>
 172             <spring_coeff unit="N/M"> 800000 </spring_coeff><!--800000-->
 173             <damping_coeff unit="N/M/SEC"> 150000 </damping_coeff><!--150000-->
 174             <max_steer unit="DEG"> 63.0 </max_steer>
 175             <brake_group> NONE </brake_group>
 176             <retractable> 1 </retractable>
 177         </contact>
 178         <contact type="BOGEY" name="LEFT_MAIN">
 179             <location unit="M">
 180                 <x> 26.82 </x>
 181                 <y> -5.75 </y>
 182                 <z> -2.5 </z>
 183             </location>
 184             <static_friction> 0.6 </static_friction>
 185             <dynamic_friction> 0.5 </dynamic_friction>
 186             <rolling_friction> 0.02 </rolling_friction><!--0.02-->
 187             <spring_coeff unit="N/M"> 1.7e+06 </spring_coeff><!--1.7e+06 -->
 188             <damping_coeff unit="N/M/SEC"> 100000 </damping_coeff>
 189             <max_steer unit="DEG"> 0 </max_steer>
 190             <brake_group> LEFT </brake_group>
 191             <retractable> 1 </retractable>
 192         </contact>
 193         <contact type="BOGEY" name="RIGHT_MAIN">
 194             <location unit="M">
 195                 <x> 26.82 </x>
 196                 <y> 5.75 </y>
 197                 <z> -2.5 </z>
 198             </location>
 199             <static_friction> 0.6 </static_friction>
 200             <dynamic_friction> 0.5 </dynamic_friction>
 201             <rolling_friction> 0.02 </rolling_friction>
 202             <spring_coeff unit="N/M"> 1.7e+06 </spring_coeff>
 203             <!--<spring_coeff unit="N/M"> 3.1536e+06 </spring_coeff>-->
 204             <!--<damping_coeff unit="N/M/SEC"> 630720 </damping_coeff>-->
 205             <damping_coeff unit="N/M/SEC"> 100000 </damping_coeff><!--100000-->
 206             <max_steer unit="DEG"> 0 </max_steer>
 207             <brake_group> RIGHT </brake_group>
 208             <retractable> 1 </retractable>
 209         </contact>
 210         <contact type="STRUCTURE" name="FRONT">
 211             <location unit="M">
 212                 <x> 3.5 </x>
 213                 <y> 0.0 </y>
 214                 <z> -0.2 </z>
 215             </location>
 216             <static_friction> 0.8 </static_friction>
 217             <dynamic_friction> 0.5 </dynamic_friction>
 218             <rolling_friction> 0 </rolling_friction>
 219             <spring_coeff unit="N/M"> 3e+06 </spring_coeff>
 220             <damping_coeff unit="N/M/SEC"> 630720 </damping_coeff>
 221             <max_steer unit="DEG"> 0 </max_steer>
 222             <brake_group> NONE </brake_group>
 223             <retractable> 0 </retractable>
 224         </contact>
 225         <contact type="STRUCTURE" name="LEFT_WING">
 226             <location unit="M">
 227                 <x> 26.82 </x>
 228                 <y> -18.7 </y>
 229                 <z> -0.5 </z>
 230             </location>
 231             <static_friction> 0.8 </static_friction>
 232             <dynamic_friction> 0.5 </dynamic_friction>
 233             <rolling_friction> 0 </rolling_friction>
 234             <spring_coeff unit="N/M"> 3e+06 </spring_coeff>
 235             <damping_coeff unit="N/M/SEC"> 630720 </damping_coeff>
 236             <max_steer unit="DEG"> 0 </max_steer>
 237             <brake_group> NONE </brake_group>
 238             <retractable> 0 </retractable>
 239         </contact>
 240         <contact type="STRUCTURE" name="RIGHT_WING">
 241             <location unit="M">
 242                 <x> 26.82 </x>
 243                 <y> 18.7 </y>
 244                 <z> -0.5 </z>
 245             </location>
 246             <static_friction> 0.8 </static_friction>
 247             <dynamic_friction> 0.5 </dynamic_friction>
 248             <rolling_friction> 0 </rolling_friction>
 249             <spring_coeff unit="N/M"> 3e+06 </spring_coeff>
 250             <damping_coeff unit="N/M/SEC"> 630720 </damping_coeff>
 251             <max_steer unit="DEG"> 0 </max_steer>
 252             <brake_group> NONE </brake_group>
 253             <retractable> 0 </retractable>
 254         </contact>
 255         <contact type="STRUCTURE" name="TAIL">
 256             <location unit="M">
 257                 <x> 41 </x>
 258                 <y> 0 </y>
 259                 <z> 1 </z>
 260             </location>
 261             <static_friction> 0.8 </static_friction>
 262             <dynamic_friction> 0.5 </dynamic_friction>
 263             <rolling_friction> 0 </rolling_friction>
 264             <spring_coeff unit="N/M"> 3e+06 </spring_coeff>
 265             <damping_coeff unit="N/M/SEC"> 630720 </damping_coeff>
 266             <max_steer unit="DEG"> 0 </max_steer>
 267             <brake_group> NONE </brake_group>
 268             <retractable> 0 </retractable>
 269         </contact>
 270     </ground_reactions>
 271
 272
 273     <propulsion>
 274
 275         <engine file="nk-8-2u">
 276             <location unit="M">
 277                 <x> 34 </x>
 278                 <y> -3.13 </y>
 279                 <z> 1.78 </z>
 280             </location>
 281             <orient unit="DEG">
 282                 <roll> 0 </roll>
 283                 <pitch> 0 </pitch>
 284                 <yaw> 0 </yaw>
 285             </orient>
 286             <feed>0</feed>
 287             <thruster file="direct">
 288                 <location unit="M">
 289                     <x> 37.27 </x>
 290                     <y> -3.03 </y>
 291                     <z> 1.7 </z>
 292                 </location>
 293                 <orient unit="DEG">
 294                     <roll> 0 </roll>
 295                     <pitch> 2 </pitch>
 296                     <yaw> -6.5 </yaw>
 297                 </orient>
 298             </thruster>
 299         </engine>
 300         <engine file="nk-8-2u">
 301             <location unit="M">
 302                 <x> 38 </x>
 303                 <y> 0 </y>
 304                 <z> 2.3 </z>
 305             </location>
 306             <orient unit="DEG">
 307                 <roll> 0 </roll>
 308                 <pitch> 0 </pitch>
 309                 <yaw> 0 </yaw>
 310             </orient>
 311             <feed>0</feed>
 312             <thruster file="direct">
 313                 <location unit="M">
 314                     <x> 41.6 </x>
 315                     <y> 0 </y>
 316                     <z> 2.26 </z>
 317                 </location>
 318                 <orient unit="DEG">
 319                     <roll> 0 </roll>
 320                     <pitch> -2.5 </pitch>
 321                     <yaw> 0 </yaw>
 322                 </orient>
 323             </thruster>
 324         </engine>
 325         <engine file="nk-8-2u">
 326             <location unit="M">
 327                 <x> 34 </x>
 328                 <y> 3.13 </y>
 329                 <z> 1.78 </z>
 330             </location>
 331             <orient unit="DEG">
 332                 <roll> 0 </roll>
 333                 <pitch> 0 </pitch>
 334                 <yaw> 0 </yaw>
 335             </orient>
 336             <feed>0</feed>
 337             <thruster file="direct">
 338                 <location unit="M">
 339                     <x> 37.27 </x>
 340                     <y> 3.03 </y>
 341                     <z> 1.7 </z>
 342                 </location>
 343                 <orient unit="DEG">
 344                     <roll> 0 </roll>
 345                     <pitch> 2 </pitch>
 346                     <yaw> 6.5 </yaw>
 347                 </orient>
 348             </thruster>
 349         </engine>
 350         <engine file="tsa-6a">
 351           <location unit="M">
 352             <x> 32 </x>
 353             <y> 0 </y>
 354             <z> 2.3 </z>
 355           </location>
 356           <orient unit="DEG">
 357             <roll> 0 </roll>
 358             <pitch> 0 </pitch>
 359             <yaw> 0 </yaw>
 360           </orient>
 361           <feed>0</feed>
 362           <thruster file="direct">
 363             <location unit="M">
 364               <x> 32 </x>
 365               <y> 0 </y>
 366               <z> 2.26 </z>
 367             </location>
 368             <orient unit="DEG">
 369               <roll> 0 </roll>
 370               <pitch> 0 </pitch>
 371               <yaw> 90 </yaw>
 372             </orient>
 373           </thruster>
 374         </engine>
 375         <tank type="FUEL">
 376             <location unit="M">
 377                 <x> 25 </x>
 378                 <y> 0 </y>
 379                 <z> 0 </z>
 380             </location>
 381             <capacity unit="KG">3300</capacity>
 382             <contents unit="KG">3300</contents>
 383         </tank>
 384         <tank type="FUEL">
 385             <location unit="M">
 386                 <x> 24 </x>
 387                 <y> -4 </y>
 388                 <z> 0 </z>
 389             </location>
 390             <capacity unit="KG">9500</capacity>
 391             <contents unit="KG">2200</contents>
 392         </tank>
 393         <tank type="FUEL">
 394             <location unit="M">
 395                 <x> 27.5 </x>
 396                 <y> -10 </y>
 397                 <z> 0 </z>
 398             </location>
 399             <capacity unit="KG">5425</capacity>
 400             <contents unit="KG">1000</contents>
 401         </tank>
 402         <tank type="FUEL">
 403             <location unit="M">
 404                 <x> 24 </x>
 405                 <y> 4 </y>
 406                 <z> 0 </z>
 407             </location>
 408             <capacity unit="KG">9500</capacity>
 409             <contents unit="KG">2200</contents>
 410         </tank>
 411         <tank type="FUEL">
 412             <location unit="M">
 413                 <x> 27.5 </x>
 414                 <y> 10 </y>
 415                 <z> 0 </z>
 416             </location>
 417             <capacity unit="KG">5425</capacity>
 418             <contents unit="KG">1000</contents>
 419         </tank>
 420         <tank type="FUEL">
 421             <location unit="M">
 422                 <x> 21 </x>
 423                 <y> 0 </y>
 424                 <z> 0 </z>
 425             </location>
 426             <capacity unit="KG">6600</capacity>
 427 <!--            <contents unit="KG">3000</contents>-->
 428             <contents unit="KG">5000</contents>
 429         </tank>
 430     </propulsion>
 431
 432     <flight_control name="tu154b">
 433 <!--
 434         <property>fcs/stab-auto-cmd</property>
 435         <property>fcs/stabilizer-cmd-norm</property>
 436         -->
 437         <!--<property>fcs/met</property>-->
 438         <channel name="Pitch">
 439 <!--Modified by yurik nov 2013-->
 440 <!--
 441             <aerosurface_scale name="fcs/met-trimmer">
 442                 <input>fcs/pitch-trim-cmd-norm</input>
 443                 <domain>
 444                         <min>-1</min>
 445                         <max>1</max>
 446                 </domain>
 447                 <range>
 448                         <min>-0.5</min>
 449                         <max>0.6</max>
 450                 </range>
 451                 <output>fcs/met</output>
 452             </aerosurface_scale>
 453 -->
 454             <summer name="Pitch Trim Sum">
 455               <input>fcs/elevator-cmd-norm</input>
 456               <!--<input>fcs/met</input>--> <!--By Yurik-->
 457               <input>ap/pitch/met</input>
 458               <clipto>
 459                 <min>-1</min>
 460                 <max>1</max>
 461               </clipto>
 462             </summer>
 463
 464             <switch name="fcs/pitch-ra-56-hydropower">
 465               <default value="0.0"/>
 466               <test value="fcs/absu-pitch">
 467                 hs/ra-56-pitch-serviceable > 0
 468               </test>
 469             </switch>
 470
 471             <summer name="Pitch Absu Sum">
 472               <input>fcs/pitch-trim-sum</input>
 473               <input>fcs/pitch-ra-56-hydropower</input>
 474               <clipto>
 475                 <min>-1</min>
 476                 <max>1</max>
 477               </clipto>
 478             </summer>
 479
 480             <switch name="fcs/pitch-hydropower">
 481               <default value="fcs/elevator-pos-static"/>
 482               <test value="fcs/pitch-absu-sum">
 483                 hs/busters-serviceable > 0
 484               </test>
 485             </switch>
 486
 487             <aerosurface_scale name="Elevator Control">
 488               <input>fcs/pitch-hydropower</input>
 489               <range>
 490                 <min>-0.506</min>
 491                 <max>0.28</max>
 492               </range>
 493               <output>fcs/elevator-pos-rad</output>
 494             </aerosurface_scale>
 495
 496             <aerosurface_scale name="Elevator Normalizer">
 497               <input>fcs/elevator-pos-rad</input>
 498               <domain>
 499                 <min>-1</min>
 500                 <max>1</max>
 501               </domain>
 502               <range>
 503                 <min>-1</min>
 504                 <max>1</max>
 505               </range>
 506               <output>fcs/elevator-pos-norm</output>
 507             </aerosurface_scale>
 508
 509         </channel>
 510
 511         <channel name="Roll">
 512
 513             <summer name="Roll Trim Sum">
 514               <input>fcs/aileron-cmd-norm</input>
 515               <input>fcs/roll-trim-cmd-norm</input>
 516               <clipto>
 517                 <min>-1</min>
 518                 <max>1</max>
 519               </clipto>
 520             </summer>
 521
 522             <switch name="fcs/roll-ra-56-hydropower">
 523               <default value="0.0"/>
 524               <test value="fcs/absu-roll">
 525                 hs/ra-56-roll-serviceable > 0
 526               </test>
 527             </switch>
 528
 529             <summer name="Roll Absu Sum">
 530               <input>fcs/roll-trim-sum</input>
 531               <input>fcs/roll-ra-56-hydropower</input>
 532               <clipto>
 533                 <min>-1</min>
 534                 <max>1</max>
 535               </clipto>
 536             </summer>
 537
 538             <switch name="fcs/roll-hydropower">
 539               <default value="fcs/aileron-pos-static"/>
 540               <test value="fcs/roll-absu-sum">
 541                 hs/busters-serviceable > 0
 542               </test>
 543             </switch>
 544
 545             <aerosurface_scale name="Left Aileron Control">
 546               <input>fcs/roll-hydropower</input>
 547               <range>
 548                 <min>-0.35</min>
 549                 <max>0.35</max>
 550               </range>
 551               <output>fcs/left-aileron-pos-rad</output>
 552             </aerosurface_scale>
 553
 554             <aerosurface_scale name="Right Aileron Control">
 555               <input>-fcs/roll-hydropower</input>
 556               <range>
 557                 <min>-0.35</min>
 558                 <max>0.35</max>
 559               </range>
 560               <output>fcs/right-aileron-pos-rad</output>
 561             </aerosurface_scale>
 562
 563             <aerosurface_scale name="Aileron Normalizer">
 564               <input>fcs/left-aileron-pos-rad</input>
 565               <domain>
 566                 <min>-1</min>
 567                 <max>1</max>
 568               </domain>
 569               <range>
 570                 <min>-1</min>
 571                 <max>1</max>
 572               </range>
 573               <output>fcs/left-aileron-pos-norm</output>
 574             </aerosurface_scale>
 575
 576         </channel>
 577
 578         <channel name="Yaw">
 579
 580             <summer name="Rudder Command Sum">
 581               <input>fcs/rudder-cmd-norm</input>
 582               <input>fcs/yaw-trim-cmd-norm</input>
 583             </summer>
 584
 585             <switch name="fcs/yaw-ra-56-hydropower">
 586               <default value="0.0"/>
 587               <test value="fcs/absu-yaw">
 588                 hs/ra-56-yaw-serviceable > 0
 589               </test>
 590             </switch>
 591
 592             <summer name="Rudder Sum">
 593               <input>fcs/rudder-command-sum</input>
 594               <input>fcs/yaw-ra-56-hydropower</input>
 595             </summer>
 596
 597             <switch name="fcs/yaw-hydropower">
 598               <default value="fcs/rudder-pos-static"/>
 599               <test value="fcs/rudder-sum">
 600                 hs/busters-serviceable > 0
 601               </test>
 602             </switch>
 603
 604             <aerosurface_scale name="Rudder Control">
 605               <input>fcs/yaw-hydropower</input>
 606               <range>
 607                 <min>-0.4363</min>
 608                 <max>0.4363</max>
 609               </range>
 610               <output>fcs/rudder-pos-rad</output>
 611             </aerosurface_scale>
 612
 613             <aerosurface_scale name="Rudder Normalizer">
 614               <input>fcs/rudder-pos-rad</input>
 615               <domain>
 616                 <min>-1</min>
 617                 <max>1</max>
 618               </domain>
 619               <range>
 620                 <min>-1</min>
 621                 <max>1</max>
 622               </range>
 623               <output>fcs/rudder-pos-norm</output>
 624             </aerosurface_scale>
 625
 626         </channel>
 627
 628         <channel name="Flaps">
 629
 630           <switch name="fcs/flap-cmd-switched">
 631             <default value="fcs/flap-cmd-static"/>
 632             <test value="fcs/flap-cmd-norm">
 633               hs/flaps-serviceable > 0
 634             </test>
 635           </switch>
 636
 637             <kinematic name="Flaps Control">
 638              <input>fcs/flap-cmd-switched</input>
 639               <traverse>
 640                 <setting>
 641                   <position>0</position>
 642                   <time>0</time>
 643                 </setting>
 644                 <setting>
 645                   <position>15</position>
 646                   <time>7</time>
 647                 </setting>
 648                 <setting>
 649                   <position>28</position>
 650                   <time>8</time>
 651                 </setting>
 652                 <setting>
 653                   <position>45</position>
 654                   <time>12</time>
 655                 </setting>
 656               </traverse>
 657               <output>fcs/flap-pos-deg</output>
 658             </kinematic>
 659
 660             <aerosurface_scale name="Flap Position Normalizer">
 661               <input>fcs/flap-pos-deg</input>
 662               <domain>
 663                 <min>0</min>  <!-- Flaps actual minimum position -->
 664                 <max>45</max>  <!-- Flaps actual maximum position -->
 665               </domain>
 666               <range>
 667                 <min>0</min>  <!-- Flaps normalized minimum position -->
 668                 <max>1</max>  <!-- Flaps normalized maximum position -->
 669               </range>
 670               <output>fcs/flap-pos-norm</output>
 671             </aerosurface_scale>
 672         </channel>
 673
 674         <channel name="Landing Gear">
 675
 676           <switch name="gear/gear-cmd-switched">
 677             <default value="gear/gear-cmd-static"/>
 678             <test value="gear/gear-cmd-norm">
 679               hs/hs1-busters-ok > 0
 680             </test>
 681           </switch>
 682
 683             <kinematic name="Gear Control">
 684               <input>gear/gear-cmd-norm</input>
 685               <!--<input>gear/gear-cmd-switched</input>-->
 686               <traverse>
 687                 <setting>
 688                   <position>0</position>
 689                   <time>0</time>
 690                 </setting>
 691                 <setting>
 692                   <position>1</position>
 693                   <time>7</time>
 694                 </setting>
 695               </traverse>
 696               <output>gear/gear-pos-norm</output>
 697             </kinematic>
 698
 699         </channel>
 700
 701         <channel name="Speedbrake">
 702
 703
 704           <pure_gain name="Speedbrake outer">
 705             <input>fcs/spoiler-cmd-norm</input>
 706             <gain>0.4</gain>
 707           </pure_gain>
 708
 709
 710           <switch name="Wow">
 711             <default value="0.0"/>
 712             <test value="1.0">
 713               forces/fbz-gear-lbs lt -1000
 714             </test>
 715           </switch>
 716
 717           <switch name="revers on ground">
 718             <default value="0.0"/>
 719             <test value="fcs/wow">
 720               propulsion/engine[0]/reverser-angle-rad gt 0.1
 721             </test>
 722           </switch>
 723
 724           <switch name="rejected takeoff">
 725             <default value="0.0"/>
 726             <test value="1.0">
 727               fcs/flap-pos-deg gt 10
 728               fcs/revers-on-ground gt 0
 729             </test>
 730           </switch>
 731
 732           <switch name="normal landing">
 733             <default value="0.0"/>
 734             <test value="1.0">
 735               fcs/flap-pos-deg gt 30
 736               fcs/revers-on-ground gt 0.5
 737               fcs/throttle-cmd-norm[0] lt fcs/revers-1-limit
 738               fcs/throttle-cmd-norm[1] lt fcs/revers-1-limit
 739               fcs/throttle-cmd-norm[2] lt fcs/revers-1-limit
 740               fcs/throttle-cmd-norm[0] gt fcs/revers-2-limit
 741               fcs/throttle-cmd-norm[1] gt fcs/revers-2-limit
 742               fcs/throttle-cmd-norm[2] gt fcs/revers-2-limit
 743             </test>
 744           </switch>
 745
 746           <summer name="Speedbrake cmd">
 747             <input>fcs/speedbrake-outer</input>
 748             <input>fcs/rejected-takeoff</input>
 749             <input>fcs/normal-landing</input>
 750             <clipto>
 751               <min>0.0</min>
 752               <max>1.0</max>
 753             </clipto>
 754           </summer>
 755
 756           <switch name="fcs/speedbrake-cmd-switched">
 757             <default value="fcs/speedbrake-cmd-static"/>
 758             <test value="fcs/speedbrake-cmd">
 759               hs/hs1-busters-ok > 0
 760             </test>
 761           </switch>
 762
 763
 764             <kinematic name="Speedbrake Control">
 765               <input>fcs/speedbrake-cmd-switched</input>
 766               <traverse>
 767                 <setting>
 768                   <position>0</position>
 769                   <time>0</time>
 770                 </setting>
 771                 <setting>
 772                   <position>1</position>
 773                   <time>0.5</time>
 774                 </setting>
 775               </traverse>
 776               <output>fcs/speedbrake-pos-norm</output>
 777             </kinematic>
 778
 779         </channel>
 780
 781         <channel name="Stabilizer">
 782
 783           <scheduled_gain name="Stabilizer Auto Pos">
 784             <input>fcs/stab-auto-cmd</input>
 785             <table>
 786               <independentVar> fcs/flap-pos-deg </independentVar>
 787               <tableData>
 788                 0             0
 789                 28            0.2727
 790                 45            0.5454
 791               </tableData>
 792             </table>
 793             <clipto>
 794               <min>0.0</min>
 795               <max>1.0</max>
 796             </clipto>
 797           </scheduled_gain>
 798
 799           <switch name="Stabilizer Cmd">
 800             <default value="fcs/stabilizer-auto-pos"/>
 801             <test value="fcs/stab-manu-cmd">
 802               fcs/stab-manu-switch eq 1.0
 803             </test>
 804           </switch>
 805
 806             <kinematic name="Stabilizer Control">
 807             <input>fcs/stabilizer-cmd</input>
 808 <!--<input>fcs/stabilizer-cmd-norm</input>-->
 809               <traverse>
 810                 <setting>
 811                   <position>0.0</position>
 812                   <time>0</time>
 813                 </setting>
 814                 <setting>
 815                   <position>0.09602</position>
 816                   <time>15</time>
 817                 </setting>
 818               </traverse>
 819             </kinematic>
 820
 821             <summer name="Stabilizer rad">
 822               <bias>0.02618</bias>
 823               <input>fcs/stabilizer-control</input>
 824               <output>fcs/stabilizer-pos-rad</output>
 825             </summer>
 826
 827             <aerosurface_scale name="Stabilizer Normalizer">
 828               <input>fcs/stabilizer-pos-rad</input>
 829               <domain>
 830                 <min>-1</min>
 831                 <max>1</max>
 832               </domain>
 833               <range>
 834                 <min>-1</min>
 835                 <max>1</max>
 836               </range>
 837               <output>fcs/right-aileron-pos-norm</output>
 838             </aerosurface_scale>
 839
 840         </channel>
 841
 842         <channel name="Brake">
 843 <!--Left-->
 844 <!--Check hydro power for brake-->
 845           <switch name="gear/left-brake-cmd-switched">
 846             <default value="0.0"/>
 847             <test logic="OR" value="gear/brake-left">
 848               hs/hs1-busters-ok > 0
 849               gear/brake-parking > 0
 850             </test>
 851             <output>fcs/left-brake-cmd-norm</output>
 852           </switch>
 853 <!--Right-->
 854
 855           <switch name="gear/right-brake-cmd-switched">
 856             <default value="0.0"/>
 857             <test logic="OR" value="gear/brake-right">
 858               hs/hs1-busters-ok > 0
 859               gear/brake-parking > 0
 860             </test>
 861             <output>fcs/right-brake-cmd-norm</output>
 862           </switch>
 863
 864         </channel>
 865
 866         <channel name="Steering">
 867
 868           <fcs_function name="gear/steering-free-cmd-norm">
 869             <function>
 870               <sum>
 871                 <property>gear/steering-cmd-norm</property>
 872                 <product>
 873                   <property>gear/unit[0]/wheel-speed-fps</property>
 874                   <sum>
 875                     <property>gear/unit[0]/side_friction_coeff</property>
 876                     <property>gear/unit[0]/rolling_friction_coeff</property>
 877                   </sum>
 878                   <property>gear/unit[0]/compression-ft</property>
 879                   <value>0.01</value>
 880                 </product>
 881               </sum>
 882             </function>
 883             <clipto>
 884               <min>-1</min>
 885               <max>1</max>
 886             </clipto>
 887           </fcs_function>
 888
 889           <fcs_function name="gear/rudder-cmd-scaled">
 890             <function>
 891               <product>
 892                 <property>fcs/rudder-cmd-norm</property>
 893                 <value>0.015873</value>
 894                 <property>gear/steering</property>
 895               </product>
 896             </function>
 897           </fcs_function>
 898
 899           <switch name="gear/steering-cmd-norm">
 900             <test value="0">
 901               gear/unit[0]/WOW == 0
 902               gear/steering-cmd-norm lt 0.25
 903               gear/steering-cmd-norm gt -0.25
 904             </test>
 905             <test value="gear/steering-cmd-norm">
 906               gear/unit[0]/WOW == 0
 907             </test>
 908             <test value="-gear/rudder-cmd-scaled">
 909               gear/nose-wheel-steering == 1
 910               systems/electrical-ok == 1
 911               hs/hs2-busters-ok == 1
 912             </test>
 913             <default value="gear/steering-free-cmd-norm"/>
 914           </switch>
 915
 916           <kinematic name="gear/steer-pos-deg">
 917             <input>gear/steering-cmd-norm</input>
 918             <traverse>
 919               <setting>
 920                 <position>-63</position>
 921                 <time>0</time>
 922               </setting>
 923               <setting>
 924                 <position>63</position>
 925                 <time>3</time>
 926               </setting>
 927             </traverse>
 928           </kinematic>
 929
 930           <!-- <output> in <kinematic> doesn't seem to work here. -->
 931           <pure_gain name="gear/steer-pos-deg-workaround">
 932             <input>gear/steer-pos-deg</input>
 933             <gain>1</gain>
 934             <output>fcs/steer-pos-deg</output>
 935           </pure_gain>
 936
 937         </channel>
 938
 939         <channel name="Landing Gear Weight Shift">
 940
 941           <fcs_function name="aero/function/weight-shift-gears">
 942                 <function>
 943                   <sum>
 944                     <product>
 945                         <property>gear/gear-pos-norm</property>
 946                         <value>-192.91</value>
 947                     </product>
 948                     <value>1243.30</value>
 949                   </sum>
 950                 </function>
 951                 <output> inertia/pointmass-location-X-inches[11] </output>
 952             </fcs_function>
 953
 954         </channel>
 955
 956     </flight_control>
 957
 958     <system file="fdm_globals"/>
 959     <system file="engines"/>
 960     <system file="hydrosystems"/>
 961     <system file="instrumentation"/>
 962     <system file="nvu"/>
 963     <system file="pushback"/>
 964     <autopilot file="Systems/absu154"/>
 965
 966
 967     <aerodynamics>
 968
 969       <function name="aero/function/CAX">
 970         <product>
 971           <difference>
 972             <product>
 973               <property>inertia/cg-x-in</property>
 974               <value>0.0254</value>
 975             </product>
 976             <value>24.04</value>
 977           </difference>
 978           <value>18.9215</value>
 979         </product>
 980       </function>
 981
 982         <function name="aero/function/auasp">
 983             <table name="alpha_max">
 984                 <independentVar lookup="row">velocities/mach</independentVar>
 985                 <independentVar lookup="column">fcs/flap-pos-deg</independentVar>
 986                 <tableData>
 987                                0             15            28            45
 988                   0.4           12            13            12            12
 989                   0.6           12            13            12            12
 990                   0.7           8.8           13            12            12
 991                   0.8           7.8           13            12            12
 992                   0.85          7.2           13            12            12
 993                   0.9           6.6           13            12            12
 994                 </tableData>
 995             </table>
 996         </function>
 997         <function name="aero/function/cmf">
 998             <description>Mach and flaps parameter</description>
 999             <sum>
1000                 <property>fcs/flap-pos-deg</property>
1001                 <product>
1002                     <property>velocities/mach</property>
1003                     <value>-1</value>
1004                 </product>
1005             </sum>
1006         </function>
1007         <function name="aero/function/cy">
1008             <description>Lift due to alpha</description>
1009             <table name="Cy">
1010                 <independentVar lookup="row">aero/alpha-wing-rad</independentVar>
1011                 <independentVar lookup="column">aero/function/cmf</independentVar>
1012                 <tableData>
1013                                -0.95         -0.8          -0.5          -0.2           28            45
1014                   -0.06981      -0.65         -0.65         -0.65         -0.65         0             0.25
1015                   0             -0.22         -0.2          -0.25         -0.25         0.4           0.65
1016                   0.04887       0.05          0.1           0.05          0             0.65          0.93
1017                   0.08727       0.24          0.36          0.3           0.2           0.87          1.15
1018                   0.1658        0.62          0.8           0.78          0.6           1.3           1.58
1019                   0.2618        0.78          1             1.19          1.05          1.78          2.08
1020                   0.2792        0.78          1.01          1.25          1.11          1.85          2.13
1021                   0.2967        0.75          0.95          1.28          1.18          1.9           2.08
1022                   0.3316        0.56          0.78          1.25          1.26          1.85          1.7
1023                   0.3665        0.3           0.5           1.18          1.3           1.7           1.4
1024                   0.384         0.18          0.35          1.1           1.27          1.6           1.3
1025                   0.4363        -0.2          -0.1          0.9           1.13          1.3           1
1026                 </tableData>
1027             </table>
1028         </function>
1029
1030         <axis name="LIFT" unit="LBS">
1031             <function name="aero/coefficient/CLalpha">
1032                 <description>Lift_due_to_alpha</description>
1033                 <product>
1034                     <property>aero/qbar-psf</property>
1035                     <property>metrics/Sw-sqft</property>
1036                     <property>aero/function/cy</property>
1037                 </product>
1038             </function>
1039             <function name="aero/coefficient/dCLsb">
1040                 <description>Delta_Lift_due_to_speedbrake</description>
1041                 <product>
1042                     <property>aero/qbar-psf</property>
1043                     <property>metrics/Sw-sqft</property>
1044                     <property>fcs/speedbrake-pos-norm</property>
1045                     <value>-0.65</value>
1046                 </product>
1047             </function>
1048             <function name="aero/coefficient/CLde">
1049                 <description>Lift_due_to_Elevator_Deflection</description>
1050                 <product>
1051                     <property>aero/qbar-psf</property>
1052                     <property>metrics/Sw-sqft</property>
1053                     <property>fcs/elevator-pos-rad</property>
1054                     <value>0.2</value>
1055                 </product>
1056             </function>
1057             <function name="aero/coefficient/dCLg">
1058                 <description>Delta_Lift_due_to_gear</description>
1059                 <product>
1060                     <property>aero/qbar-psf</property>
1061                     <property>metrics/Sw-sqft</property>
1062                     <property>gear/gear-pos-norm</property>
1063                     <value>-0.06</value>
1064                 </product>
1065             </function>
1066             <function name="aero/coefficient/CLground">
1067                 <description>Lift near ground</description>
1068                 <product>
1069                     <table name="Delta lift due ground reaction">
1070                         <independentVar>position/h-agl-ft</independentVar>
1071                         <tableData>
1072                           0             0.13
1073                           10            0.1
1074                           27            0
1075                         </tableData>
1076                     </table>
1077                     <property>aero/qbar-psf</property>
1078                     <property>metrics/Sw-sqft</property>
1079                 </product>
1080             </function>
1081
1082         </axis>
1083         <axis name="DRAG" unit="LBS">
1084 <!--
1085             <function name="aero/coefficient/CDx">
1086                 <description>Drag_due_to_Cy</description>
1087                 <product>
1088                     <property>aero/qbar-psf</property>
1089                     <property>metrics/Sw-sqft</property>
1090                     <table name="Cx">
1091                         <independentVar lookup="row">aero/function/cy</independentVar>
1092                         <independentVar lookup="column">aero/function/cmf</independentVar>
1093                         <tableData>
1094                                        -0.95         -0.9          -0.6          -0.2           28            45
1095                           -0.25         0.032         0.028         0.025         0.025         0.11          0.2
1096                           0             0.04          0.028         0.025         0.022         0.11          0.2
1097                           0.25          0.05          0.037         0.027         0.025         0.11          0.2
1098                           0.5           0.3           0.07          0.034         0.032         0.113         0.2
1099                           0.75          1.7           0.3           0.049         0.05          0.125         0.202
1100                           1             2.5           1             0.08          0.095         0.14          0.21
1101                           1.05          2.6           1.2           0.1           0.12          0.145         0.212
1102                           1.25          2.9           2             0.35          0.27          0.17          0.227
1103                           1.5           3             2.5           1             0.6           0.205         0.263
1104                           1.7           3             2.5           2             1             0.24          0.3
1105                         </tableData>
1106                     </table>
1107                 </product>
1108             </function>-->
1109
1110  <!--           <function name="aero/coefficient/CDx">
1111                 <description>Drag_due_to_alpha</description>
1112                 <product>
1113                     <property>aero/qbar-psf</property>
1114                     <property>metrics/Sw-sqft</property>
1115                     <table name="Cx">
1116                         <independentVar lookup="row">aero/alpha-wing-rad</independentVar>
1117                         <independentVar lookup="column">aero/function/cmf</independentVar>
1118                         <tableData>
1119                           -1             -0.95         -0.85       -0.7          -0.2           28            45
1120                 -4.0     -0.06981       0.08            0.048     0.045         0.04            0.122           0.203
1121                 0.0       0             0.05            0.03      0.028         0.025           0.114           0.2
1122                 2.8       0.04887       0.044           0.026     0.025         0.022           0.118           0.207
1123                 5.0       0.08727       0.05            0.03      0.03          0.025           0.133           0.225
1124                 9.0       0.1658        0.08            0.048     0.045         0.04            0.172           0.266
1125                 15.0      0.2618        0.2             0.1       0.097         0.091           0.25            0.35
1126                 16.0      0.2792        0.222           0.12      0.111         0.106           0.26            0.36
1127                 17.0      0.2967        0.24            0.14      0.120         0.115           0.27            0.37
1128                 19.0      0.3316        0.29            0.17      0.145         0.14            0.29            0.39
1129                 21.0      0.3665        0.36            0.21      0.18          0.174           0.31            0.41
1130                 22.0      0.384         0.4             0.24      0.197         0.19            0.32            0.42
1131                 25.0      0.4363        0.5             0.3       0.25          0.24            0.38            0.48
1132                         </tableData>
1133                     </table>
1134                 </product>
1135             </function>
1136  -->
1137
1138
1139             <function name="aero/coefficient/CDx">
1140                 <description>Drag_due_to_alpha</description>
1141                 <product>
1142                     <property>aero/qbar-psf</property>
1143                     <property>metrics/Sw-sqft</property>
1144                     <table name="Cx">
1145                         <independentVar lookup="row">aero/alpha-wing-rad</independentVar>
1146                         <independentVar lookup="column">aero/function/cmf</independentVar>
1147                         <tableData>
1148                                        -0.95         -0.85       -0.7          -0.2           28            45
1149                          -0.06981       0.08            0.048     0.045         0.04            0.122           0.203
1150                           0             0.05            0.03      0.028         0.025           0.114           0.2
1151                           0.04887       0.044           0.026     0.025         0.022           0.118           0.207
1152                           0.08727       0.05            0.03      0.03          0.025           0.133           0.225
1153                           0.1658        0.08            0.048     0.045         0.04            0.172           0.266
1154                           0.2618        0.2             0.1       0.097         0.091           0.25            0.35
1155                           0.2792        0.222           0.12      0.111         0.106           0.26            0.36
1156                           0.2967        0.24            0.14      0.120         0.115           0.27            0.37
1157                           0.3316        0.29            0.17      0.145         0.14            0.29            0.39
1158                           0.3665        0.36            0.21      0.18          0.174           0.31            0.41
1159                           0.384         0.4             0.24      0.197         0.19            0.32            0.42
1160                           0.4363        0.5             0.3       0.25          0.24            0.38            0.48
1161                         </tableData>
1162                     </table>
1163                     <value>0.92</value>
1164                 </product>
1165             </function>
1166
1167
1168
1169             <function name="aero/coefficient/CDgear">
1170                 <description>Drag_due_to_gear</description>
1171                 <product>
1172                     <property>aero/qbar-psf</property>
1173                     <property>metrics/Sw-sqft</property>
1174                     <property>gear/gear-pos-norm</property>
1175                     <table name="Gear drag due to mach">
1176                         <independentVar>velocities/mach</independentVar>
1177                         <tableData>
1178                           0.2    0.0155
1179                           0.3    0.0157
1180                           0.4    0.0164
1181                           0.5    0.0176
1182                           0.6    0.0197
1183                           0.7    0.0233
1184                           0.8    0.0301
1185                           0.9    0.0468
1186                         </tableData>
1187                     </table>
1188                 </product>
1189             </function>
1190             <function name="aero/coefficient/CDsb">
1191                 <description>Drag_due_to_speedbrakes</description>
1192                 <product>
1193                     <property>aero/qbar-psf</property>
1194                     <property>metrics/Sw-sqft</property>
1195                     <property>fcs/speedbrake-pos-norm</property>
1196                     <value>0.019</value>
1197                 </product>
1198             </function>
1199             <function name="aero/coefficient/CDbeta">
1200                 <description>Drag_due_to_sideslip</description>
1201                 <product>
1202                     <property>aero/qbar-psf</property>
1203                     <property>metrics/Sw-sqft</property>
1204                     <table>
1205                         <independentVar>aero/beta-rad</independentVar>
1206                         <tableData>
1207                           -1.57         1.23
1208                           -0.26         0.05
1209                           0             0
1210                           0.26          0.05
1211                           1.57          1.23
1212                         </tableData>
1213                     </table>
1214                 </product>
1215             </function>
1216             <function name="aero/coefficient/CDde">
1217                 <description>Drag_due_to_Elevator_Deflection</description>
1218                 <product>
1219                     <property>aero/qbar-psf</property>
1220                     <property>metrics/Sw-sqft</property>
1221                     <abs>
1222                       <property>fcs/elevator-pos-norm</property>
1223                     </abs>
1224                     <value>0.01</value>
1225                 </product>
1226             </function>
1227             <function name="aero/coefficient/CDground">
1228                 <description>Drag near ground</description>
1229                 <product>
1230                     <table name="Delta drag due ground reaction">
1231                         <independentVar>position/h-agl-ft</independentVar>
1232                         <tableData>
1233                           0             -0.01
1234                           10            -0.008
1235                           27            0
1236                         </tableData>
1237                     </table>
1238                     <property>aero/qbar-psf</property>
1239                     <property>metrics/Sw-sqft</property>
1240                 </product>
1241             </function>
1242         </axis>
1243         <axis name="SIDE" unit="LBS">
1244             <function name="aero/coefficient/CYb">
1245                 <description>Side_force_due_to_beta</description>
1246                 <product>
1247                     <property>aero/qbar-psf</property>
1248                     <property>metrics/Sw-sqft</property>
1249                     <property>aero/beta-rad</property>
1250                     <table name="side force due flaps">
1251                         <independentVar>fcs/flap-pos-deg</independentVar>
1252                         <tableData>
1253                           0             -0.859
1254                           28            -1.031
1255                           45            -1.146
1256                         </tableData>
1257                     </table>
1258                 </product>
1259             </function>
1260             <function name="aero/coefficient/CYr">
1261                 <description>Side_force_due_rudder</description>
1262                 <product>
1263                     <property>aero/qbar-psf</property>
1264                     <property>metrics/Sw-sqft</property>
1265                     <property>fcs/rudder-pos-rad</property>
1266                     <value>-0.1776</value>
1267                 </product>
1268             </function>
1269         </axis>
1270         <axis name="ROLL" unit="LBS*FT">
1271             <function name="aero/coefficient/Clb">
1272                 <description>Roll_moment_due_to_beta</description>
1273                 <product>
1274                     <property>aero/qbar-psf</property>
1275                     <property>metrics/Sw-sqft</property>
1276                     <property>metrics/bw-ft</property>
1277                     <property>aero/beta-rad</property>
1278                     <table name="Roll due beta">
1279                         <independentVar lookup="row">aero/alpha-wing-rad</independentVar>
1280                         <independentVar lookup="column">fcs/flap-pos-deg</independentVar>
1281                         <tableData>
1282                                        0             28            45
1283                           0             -0.00135      -0.003        -0.0034
1284                           0.08727       -0.0017       -0.0033       -0.00375
1285                           0.17453       -0.0019       -0.0036       -0.004
1286                           0.2678        -0.0025       -0.0037       -0.0048
1287                         </tableData>
1288                     </table>
1289                 </product>
1290             </function>
1291             <function name="aero/coefficient/Clp">
1292                 <description>Roll_moment_due_to_roll_rate</description>
1293                 <product>
1294                     <property>aero/qbar-psf</property>
1295                     <property>metrics/Sw-sqft</property>
1296                     <property>metrics/bw-ft</property>
1297                     <property>aero/bi2vel</property>
1298                     <property>velocities/p-aero-rad_sec</property>
1299                     <value>-0.5</value>
1300                 </product>
1301             </function>
1302             <function name="aero/coefficient/Clr">
1303                 <description>Roll_moment_due_to_yaw_rate</description>
1304                 <product>
1305                     <property>aero/qbar-psf</property>
1306                     <property>metrics/Sw-sqft</property>
1307                     <property>metrics/bw-ft</property>
1308                     <property>aero/bi2vel</property>
1309                     <property>velocities/r-aero-rad_sec</property>
1310                     <value>0.15</value>
1311                 </product>
1312             </function>
1313             <function name="aero/coefficient/Clda">
1314                 <description>Roll_moment_due_to_aileron</description>
1315                 <product>
1316                     <property>aero/qbar-psf</property>
1317                     <property>metrics/Sw-sqft</property>
1318                     <property>metrics/bw-ft</property>
1319                     <property>fcs/left-aileron-pos-rad</property>
1320                     <table>
1321                         <independentVar>velocities/mach</independentVar>
1322                         <tableData>
1323                           0.15          0.0659
1324                           0.5           0.0595
1325                           1             0.03438
1326                         </tableData>
1327                     </table>
1328                     <value>1.4</value>
1329                 </product>
1330             </function>
1331             <function name="aero/coefficient/Cldr">
1332                 <description>Roll_moment_due_to_rudder</description>
1333                 <product>
1334                     <property>aero/qbar-psf</property>
1335                     <property>metrics/Sw-sqft</property>
1336                     <property>metrics/bw-ft</property>
1337                     <property>fcs/rudder-pos-rad</property>
1338                     <value>-0.01719</value>
1339                 </product>
1340             </function>
1341         </axis>
1342         <axis name="PITCH" unit="LBS*FT">
1343             <function name="aero/coefficient/Cmalpha">
1344                 <description>Pitch_moment_due_to_alpha</description>
1345                 <product>
1346                     <property>aero/qbar-psf</property>
1347                     <property>metrics/Sw-sqft</property>
1348                     <property>metrics/cbarw-ft</property>
1349                     <table name="Ma">
1350                         <independentVar lookup="row">aero/alpha-wing-rad</independentVar>
1351                         <independentVar lookup="column">fcs/flap-pos-deg</independentVar>
1352                         <tableData>
1353                                        0             15            28            45
1354                           -0.06981      0.275         0.15          0             -0.14
1355                           0             0.183         0.05          -0.08         -0.213
1356                           0.06981       0.08          -0.05         -0.18         -0.29
1357                           0.2618        -0.16         -0.27         -0.375        -0.453
1358                           0.349         -0.212        -0.325        -0.425        -0.45
1359                           0.3665        -0.21         -0.32         -0.412        -0.452
1360                           0.384         -0.19         -0.3          -0.4          -0.425
1361                         </tableData>
1362                     </table>
1363                     <value>1.25</value>
1364                 </product>
1365             </function>
1366             <function name="aero/coefficient/Cmcg">
1367                 <description>Pitch_moment_due_to_CG_position</description>
1368                 <product>
1369                     <property>aero/qbar-psf</property>
1370                     <property>metrics/Sw-sqft</property>
1371                     <property>metrics/cbarw-ft</property>
1372                     <property>aero/function/cy</property>
1373                     <product>
1374                         <sum>
1375                             <description>CG due 25%MAC</description>
1376                             <property>inertia/cg-x-in</property>
1377                             <value>-998.43</value>
1378                         </sum>
1379                         <value>0.012</value><!--0.0048-->
1380                     </product>
1381                     <value>1</value>
1382                 </product>
1383             </function>
1384             <function name="aero/coefficient/Cmde">
1385                 <description>Pitch_moment_due_to_elevator</description>
1386                 <product>
1387                     <property>aero/qbar-psf</property>
1388                     <property>metrics/Sw-sqft</property>
1389                     <property>metrics/cbarw-ft</property>
1390                     <table name="mme">
1391                         <independentVar>velocities/mach</independentVar>
1392                         <tableData>
1393                           0.4           1
1394                           0.5           1
1395                           0.7           1
1396                           0.786         0.97
1397                           0.87          0.8461
1398                           0.9           0.7692
1399                           0.95          0.5384
1400                         </tableData>
1401                     </table>
1402                     <table name="cyh">
1403                         <independentVar lookup="row">fcs/elevator-pos-rad</independentVar>
1404                         <independentVar lookup="column">velocities/mach</independentVar>
1405                         <tableData>
1406                                        0             2
1407                           -0.524        -1            -0.5
1408                           -0.349        -0.85         -0.49
1409                           -0.174        -0.5         -0.4
1410                           0             0             0
1411                           0.174         0.5          0.4
1412                           0.349         0.85          0.49
1413                           0.524         1             0.5
1414                         </tableData>
1415                     </table>
1416                     <value>-0.7</value><!--0.48-->
1417                 </product>
1418             </function>
1419             <function name="aero/coefficient/Cmq">
1420                 <description>Pitch_moment_due_to_pitch_rate</description>
1421                 <product>
1422                     <property>aero/qbar-psf</property>
1423                     <property>metrics/Sw-sqft</property>
1424                     <property>metrics/cbarw-ft</property>
1425                     <property>aero/ci2vel</property>
1426                     <property>velocities/q-aero-rad_sec</property>
1427                     <value>-15</value>
1428                 </product>
1429             </function>
1430             <function name="aero/coefficient/Cmadot">
1431                 <description>Pitch_moment_due_to_alpha_rate</description>
1432                 <product>
1433                     <property>aero/qbar-psf</property>
1434                     <property>metrics/Sw-sqft</property>
1435                     <property>metrics/cbarw-ft</property>
1436                     <property>aero/ci2vel</property>
1437                     <property>aero/alphadot-rad_sec</property>
1438                     <value>-4</value>
1439                 </product>
1440             </function>
1441             <function name="aero/coefficient/Cstab">
1442                 <description>Pitch moment due to stabilizer position</description>
1443                 <product>
1444                     <property>aero/qbar-psf</property>
1445                     <property>metrics/Sw-sqft</property>
1446                     <property>metrics/cbarw-ft</property>
1447                     <table name="mms">
1448                         <independentVar>velocities/mach</independentVar>
1449                         <tableData>
1450                           0.4           1
1451                           0.7           1.083
1452                           0.87          1.2083
1453                           0.9           1.25
1454                           0.95          1.1875
1455                         </tableData>
1456                     </table>
1457                     <table name="cys">
1458                         <independentVar lookup="row">fcs/stabilizer-pos-rad</independentVar>
1459                         <independentVar lookup="column">velocities/mach</independentVar>
1460                         <tableData>
1461                                        0             2
1462                           -0.524        3.2           1.6
1463                           -0.349        3.2           1.6
1464                           -0.174        2.08          1.28
1465                           0             0             0
1466                           0.174         -2.08         -1.28
1467                           0.349         -3.2          -1.6
1468                           0.524         -3.2          -1.6
1469                         </tableData>
1470                     </table>
1471                     <value>-0.47</value>
1472                 </product>
1473             </function>
1474         </axis>
1475         <axis name="YAW" unit="LBS*FT">
1476             <function name="aero/coefficient/Cnb">
1477                 <description>Yaw_moment_due_to_beta</description>
1478                 <product>
1479                     <property>aero/qbar-psf</property>
1480                     <property>metrics/Sw-sqft</property>
1481                     <property>metrics/bw-ft</property>
1482                     <property>aero/beta-rad</property>
1483                     <table name="Yaw moment due flaps and Mach">
1484                         <independentVar lookup="row">fcs/flap-pos-deg</independentVar>
1485                         <independentVar lookup="column">velocities/mach</independentVar>
1486                         <tableData>
1487                                        0.1           0.9
1488                           0             -0.15         -0.218
1489                           28            -0.2          -0.2934
1490                           45            -0.24         -0.3518
1491                         </tableData>
1492                     </table>
1493                     <value>-1</value>
1494                 </product>
1495             </function>
1496             <function name="aero/coefficient/Cnr">
1497                 <description>Yaw_moment_due_to_yaw_rate</description>
1498                 <product>
1499                     <property>aero/qbar-psf</property>
1500                     <property>metrics/Sw-sqft</property>
1501                     <property>metrics/bw-ft</property>
1502                     <property>aero/bi2vel</property>
1503                     <property>velocities/r-aero-rad_sec</property>
1504                     <value>-0.15</value>
1505                 </product>
1506             </function>
1507             <function name="aero/coefficient/Cndr">
1508                 <description>Yaw_moment_due_to_rudder</description>
1509                 <product>
1510                     <property>aero/qbar-psf</property>
1511                     <property>metrics/Sw-sqft</property>
1512                     <property>metrics/bw-ft</property>
1513                     <property>fcs/rudder-pos-rad</property>
1514                     <value>-0.0745</value>
1515                 </product>
1516             </function>
1517         </axis>
1518     </aerodynamics>
1519
1520     <external_reactions>
1521       <force name="pushback" frame="BODY">
1522         <location unit="IN">
1523         <x>  -139 </x>
1524         <y>    0.0 </y>
1525         <z>  -71.0 </z>
1526         </location>
1527         <direction>
1528         <x>1</x>
1529         <y>0</y>
1530         <z>0</z>
1531         </direction>
1532       </force>
1533    </external_reactions>
1534 <!--
1535     <output name="tu-fldata.csv" type="CSV" rate="1">
1536         <simulation> OFF </simulation>
1537         <atmosphere> OFF </atmosphere>
1538         <massprops> OFF </massprops>
1539         <aerosurfaces> ON </aerosurfaces>
1540         <rates> OFF </rates>
1541         <velocities> ON </velocities>
1542         <forces> OFF </forces>
1543         <moments> OFF </moments>
1544         <position> ON </position>
1545         <coefficients> OFF </coefficients>
1546         <ground_reactions> OFF </ground_reactions>
1547         <fcs> OFF </fcs>
1548         <propulsion> ON </propulsion>
1549         <property>velocities/vc-kts</property>
1550         <property>velocities/vc-fps</property>
1551         <property>velocities/mach</property>
1552         <property>ap/pitch/met-input</property>
1553         <property>ap/pitch/met</property>
1554         <property>ap/pitch/gs-k5</property>
1555         <property>ap/pitch/main-stab-summer</property>
1556         <property>ap/pitch/latch-out-rad</property>
1557         <property>debug/gs-epsilon</property>
1558         <property>debug/h-m</property>
1559         <property>debug/wp-hdg-corrected</property>
1560         <property>debug/wp-distance</property>
1561     </output>-->
1562
1563   </fdm_config>