Aircraft/tu154b/tu154b.xml

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