1<?xml version="1.0"?> 2<?xml-stylesheet href="http://jsbsim.sourceforge.net/JSBSim.xsl" type="text/xsl"?> 3<fdm_config name="Aermacchi MB-339PAN" version="2.0" release="BETA" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd"> 4 <fileheader> 5 <author>HCI Lab - University of Udine</author> 6 <filecreationdate></filecreationdate> 7 <description>MB-339PAN</description> 8 <version>2.1</version> 9 </fileheader> 10 <metrics> 11 <wingarea unit="FT2">207.76</wingarea> 12 <wingspan unit="FT">35.63</wingspan> 13 <chord unit="FT">5.83</chord> 14 <htailarea unit="FT2">35.32</htailarea> 15 <htailarm unit="FT">21.6</htailarm> 16 <vtailarea unit="FT2">20.78</vtailarea> 17 <vtailarm unit="FT">0</vtailarm> 18 <location name="AERORP" unit="IN"> 19 <x>195</x> 20 <y>0</y> 21 <z>22</z> 22 </location> 23 <location name="EYEPOINT" unit="IN"> 24 <x>95</x> 25 <y>0</y> 26 <z>35</z> 27 </location> 28 <location name="VRP" unit="IN"> 29 <x>0</x> 30 <y>0</y> 31 <z>0</z> 32 </location> 33 </metrics> 34 <mass_balance> 35 <ixx unit="SLUG*FT2">10100</ixx> 36 <iyy unit="SLUG*FT2">20323</iyy> 37 <izz unit="SLUG*FT2">23691</izz> 38 <emptywt unit="LBS">6883</emptywt> 39 <location name="CG" unit="IN"> 40 <x>195</x> 41 <y>0</y> 42 <z>22</z> 43 </location> 44 <pointmass name="name"> 45 <weight unit="LBS">180</weight> 46 <location name="POINTMASS" unit="IN"> 47 <x>90</x> 48 <y>0</y> 49 <z>20</z> 50 </location> 51 </pointmass> 52 </mass_balance> 53 <ground_reactions> 54 <contact type="BOGEY" name="NOSE_LG"> 55 <location unit="IN"> 56 <x>47</x> 57 <y>0</y> 58 <z>-25</z> 59 </location> 60 <static_friction>0.8</static_friction> 61 <dynamic_friction>0.5</dynamic_friction> 62 <rolling_friction>0.02</rolling_friction> 63 <spring_coeff unit="LBS/FT">6500</spring_coeff> 64 <damping_coeff unit="LBS/FT/SEC">400</damping_coeff> 65 <max_steer unit="DEG">60</max_steer> 66 <brake_group>NOSE</brake_group> 67 <retractable>1</retractable> 68 </contact> 69 <contact type="BOGEY" name="LEFT_LG"> 70 <location unit="IN"> 71 <x>210</x> 72 <y>-44</y> 73 <z>-25</z> 74 </location> 75 <static_friction>0.8</static_friction> 76 <dynamic_friction>0.5</dynamic_friction> 77 <rolling_friction>0.02</rolling_friction> 78 <spring_coeff unit="LBS/FT">11000</spring_coeff> 79 <damping_coeff unit="LBS/FT/SEC">400</damping_coeff> 80 <max_steer unit="DEG">0.0</max_steer> 81 <brake_group>LEFT</brake_group> 82 <retractable>1</retractable> 83 </contact> 84 <contact type="BOGEY" name="RIGHT_LG"> 85 <location unit="IN"> 86 <x>210</x> 87 <y>44</y> 88 <z>-25</z> 89 </location> 90 <static_friction>0.8</static_friction> 91 <dynamic_friction>0.5</dynamic_friction> 92 <rolling_friction>0.02</rolling_friction> 93 <spring_coeff unit="LBS/FT">11000</spring_coeff> 94 <damping_coeff unit="LBS/FT/SEC">400</damping_coeff> 95 <max_steer unit="DEG">0.0</max_steer> 96 <brake_group>RIGHT</brake_group> 97 <retractable>1</retractable> 98 </contact> 99 <contact type="STRUCTURE" name="NOSE_BOTTOM"> 100 <location unit="IN"> 101 <x>30</x> 102 <y>0</y> 103 <z>-8</z> 104 </location> 105 <static_friction>0.2</static_friction> 106 <dynamic_friction>0.2</dynamic_friction> 107 <rolling_friction>0.2</rolling_friction> 108 <spring_coeff unit="LBS/FT">2000</spring_coeff> 109 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 110 </contact> 111 <contact type="STRUCTURE" name="NOSE_CP"> 112 <location unit="IN"> 113 <x>0</x> 114 <y>0</y> 115 <z>0</z> 116 </location> 117 <static_friction>0.2</static_friction> 118 <dynamic_friction>0.2</dynamic_friction> 119 <rolling_friction>0.2</rolling_friction> 120 <spring_coeff unit="LBS/FT">2000</spring_coeff> 121 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 122 </contact> 123 <contact type="STRUCTURE" name="CANOPY_CP"> 124 <location unit="IN"> 125 <x>85</x> 126 <y>0</y> 127 <z>50</z> 128 </location> 129 <static_friction>0.2</static_friction> 130 <dynamic_friction>0.2</dynamic_friction> 131 <rolling_friction>0.2</rolling_friction> 132 <spring_coeff unit="LBS/FT">2000</spring_coeff> 133 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 134 </contact> 135 <contact type="STRUCTURE" name="RUDDER_CP"> 136 <location unit="IN"> 137 <x>370</x> 138 <y>0</y> 139 <z>122</z> 140 </location> 141 <static_friction>0.2</static_friction> 142 <dynamic_friction>0.2</dynamic_friction> 143 <rolling_friction>0.2</rolling_friction> 144 <spring_coeff unit="LBS/FT">2000</spring_coeff> 145 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 146 </contact> 147 <contact type="STRUCTURE" name="REAR_CP"> 148 <location unit="IN"> 149 <x>419</x> 150 <y>0</y> 151 <z>37</z> 152 </location> 153 <static_friction>0.2</static_friction> 154 <dynamic_friction>0.2</dynamic_friction> 155 <rolling_friction>0.2</rolling_friction> 156 <spring_coeff unit="LBS/FT">2000</spring_coeff> 157 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 158 </contact> 159 <contact type="STRUCTURE" name="LOW_REAR"> 160 <location unit="IN"> 161 <x>400</x> 162 <y>0</y> 163 <z>5</z> 164 </location> 165 <static_friction>0.2</static_friction> 166 <dynamic_friction>0.2</dynamic_friction> 167 <rolling_friction>0.2</rolling_friction> 168 <spring_coeff unit="LBS/FT">2000</spring_coeff> 169 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 170 </contact> 171 <contact type="STRUCTURE" name="REAR_TANK_SX"> 172 <location unit="IN"> 173 <x>245</x> 174 <y>-116</y> 175 <z>-12</z> 176 </location> 177 <static_friction>0.2</static_friction> 178 <dynamic_friction>0.2</dynamic_friction> 179 <rolling_friction>0.2</rolling_friction> 180 <spring_coeff unit="LBS/FT">2000</spring_coeff> 181 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 182 </contact> 183 <contact type="STRUCTURE" name="REAR_TANK_DX"> 184 <location unit="IN"> 185 <x>245</x> 186 <y>116</y> 187 <z>-12</z> 188 </location> 189 <static_friction>0.2</static_friction> 190 <dynamic_friction>0.2</dynamic_friction> 191 <rolling_friction>0.2</rolling_friction> 192 <spring_coeff unit="LBS/FT">2000</spring_coeff> 193 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 194 </contact> 195 <contact type="STRUCTURE" name="AFT_TANK_SX"> 196 <location unit="IN"> 197 <x>155</x> 198 <y>-116</y> 199 <z>-12</z> 200 </location> 201 <static_friction>0.2</static_friction> 202 <dynamic_friction>0.2</dynamic_friction> 203 <rolling_friction>0.2</rolling_friction> 204 <spring_coeff unit="LBS/FT">2000</spring_coeff> 205 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 206 </contact> 207 <contact type="STRUCTURE" name="AFT_TANK_DX"> 208 <location unit="IN"> 209 <x>155</x> 210 <y>116</y> 211 <z>-12</z> 212 </location> 213 <static_friction>0.2</static_friction> 214 <dynamic_friction>0.2</dynamic_friction> 215 <rolling_friction>0.2</rolling_friction> 216 <spring_coeff unit="LBS/FT">2000</spring_coeff> 217 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 218 </contact> 219 <contact type="STRUCTURE" name="SX_WING_TIP"> 220 <location unit="IN"> 221 <x>218</x> 222 <y>-210</y> 223 <z>18</z> 224 </location> 225 <static_friction>0.2</static_friction> 226 <dynamic_friction>0.2</dynamic_friction> 227 <rolling_friction>0.2</rolling_friction> 228 <spring_coeff unit="LBS/FT">2000</spring_coeff> 229 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 230 </contact> 231 <contact type="STRUCTURE" name="DX_WING_TIP"> 232 <location unit="IN"> 233 <x>218</x> 234 <y>210</y> 235 <z>18</z> 236 </location> 237 <static_friction>0.2</static_friction> 238 <dynamic_friction>0.2</dynamic_friction> 239 <rolling_friction>0.2</rolling_friction> 240 <spring_coeff unit="LBS/FT">2000</spring_coeff> 241 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 242 </contact> 243 <contact type="STRUCTURE" name="SX_ELEV_TIP"> 244 <location unit="IN"> 245 <x>410</x> 246 <y>-80</y> 247 <z>34</z> 248 </location> 249 <static_friction>0.2</static_friction> 250 <dynamic_friction>0.2</dynamic_friction> 251 <rolling_friction>0.2</rolling_friction> 252 <spring_coeff unit="LBS/FT">2000</spring_coeff> 253 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 254 </contact> 255 <contact type="STRUCTURE" name="DX_ELEV_TIP"> 256 <location unit="IN"> 257 <x>410</x> 258 <y>80</y> 259 <z>34</z> 260 </location> 261 <static_friction>0.2</static_friction> 262 <dynamic_friction>0.2</dynamic_friction> 263 <rolling_friction>0.2</rolling_friction> 264 <spring_coeff unit="LBS/FT">2000</spring_coeff> 265 <damping_coeff unit="LBS/FT/SEC">100</damping_coeff> 266 </contact> 267 </ground_reactions> 268 <propulsion> 269 <engine file="rollsroyce"> 270 <location unit="IN"> 271 <x>210</x> 272 <y>0</y> 273 <z>22</z> 274 </location> 275 <orient unit="DEG"> 276 <roll>0.0</roll> 277 <pitch>0</pitch> 278 <yaw>0</yaw> 279 </orient> 280 <feed>0</feed> 281 <feed>1</feed> 282 <feed>2</feed> 283 <thruster file="direct"> 284 <location unit="IN"> 285 <x>210</x> 286 <y>0</y> 287 <z>22</z> 288 </location> 289 <orient unit="DEG"> 290 <roll>0.0</roll> 291 <pitch>0.0</pitch> 292 <yaw>0.0</yaw> 293 </orient> 294 </thruster> 295 </engine> 296 <tank type="FUEL"> 297 <!-- Tank number 0 --> 298 <location unit="IN"> 299 <x>145</x> 300 <y>0</y> 301 <z>5</z> 302 </location> 303 <capacity unit="LBS">1135</capacity> 304 <contents unit="LBS">1100</contents> 305 </tank> 306 <tank type="FUEL"> 307 <!-- Tank number 1 --> 308 <location unit="IN"> 309 <x>204</x> 310 <y>-116</y> 311 <z>-5</z> 312 </location> 313 <capacity unit="LBS">442</capacity> 314 <contents unit="LBS">420</contents> 315 </tank> 316 <tank type="FUEL"> 317 <!-- Tank number 2 --> 318 <location unit="IN"> 319 <x>204</x> 320 <y>116</y> 321 <z>-5</z> 322 </location> 323 <capacity unit="LBS">442</capacity> 324 <contents unit="LBS">420</contents> 325 </tank> 326 </propulsion> 327 <flight_control name="Aermacchi MB339 PAN"> 328 <channel name="Pitch"> 329 <pure_gain name="Pitch Damper Gain"> 330 <input>velocities/q-rad_sec</input> 331 <gain>0.6</gain> 332 </pure_gain> 333 <summer name="Pitch Trim Sum"> 334 <input>fcs/elevator-cmd-norm</input> 335 <input>fcs/pitch-trim-cmd-norm</input> 336 <clip> 337 <min>-1</min> 338 <max>1</max> 339 </clip> 340 </summer> 341 <aerosurface_scale name="Elevator Control"> 342 <input>fcs/pitch-trim-sum</input> 343 <gain>0.01745</gain> 344 <range> 345 <min>-20</min> 346 <max>17</max> 347 </range> 348 <output>fcs/elevator-pos-rad</output> 349 </aerosurface_scale> 350 <aerosurface_scale name="Elevator Position Normalized"> 351 <input>fcs/elevator-pos-deg</input> 352 <domain> 353 <min>-20</min> 354 <max>17</max> 355 </domain> 356 <range> 357 <min>-1</min> 358 <max>1</max> 359 </range> 360 <output>fcs/elevator-pos-norm</output> 361 </aerosurface_scale> 362 </channel> 363 <channel name="Roll"> 364 <pure_gain name="Roll Damper Gain Roll"> 365 <input>velocities/p-rad_sec</input> 366 <gain>-0.5</gain> 367 </pure_gain> 368 <pure_gain name="Roll Damper Gain Yaw"> 369 <input>velocities/r-rad_sec</input> 370 <gain>-0.6</gain> 371 </pure_gain> 372 <summer name="Roll Trim Sum"> 373 <input>fcs/aileron-cmd-norm</input> 374 <input>fcs/roll-trim-cmd-norm</input> 375 <clip> 376 <min>-1</min> 377 <max>1</max> 378 </clip> 379 </summer> 380 <aerosurface_scale name="Left Aileron Control"> 381 <input>fcs/roll-trim-sum</input> 382 <gain>0.01745</gain> 383 <range> 384 <min>-15</min> 385 <max>10</max> 386 </range> 387 <output>fcs/left-aileron-pos-rad</output> 388 </aerosurface_scale> 389 <aerosurface_scale name="Left Aileron Position Normalized"> 390 <input>fcs/left-aileron-pos-deg</input> 391 <domain> 392 <min>-15</min> 393 <max>10</max> 394 </domain> 395 <range> 396 <min>-1</min> 397 <max>1</max> 398 </range> 399 <output>fcs/left-aileron-pos-norm</output> 400 </aerosurface_scale> 401 <aerosurface_scale name="Right Aileron Control"> 402 <input>-fcs/roll-trim-sum</input> 403 <gain>0.01745</gain> 404 <range> 405 <min>-15</min> 406 <max>10</max> 407 </range> 408 <output>fcs/right-aileron-pos-rad</output> 409 </aerosurface_scale> 410 <aerosurface_scale name="Right Aileron Position Normalized"> 411 <input>fcs/right-aileron-pos-deg</input> 412 <domain> 413 <min>-15</min> 414 <max>10</max> 415 </domain> 416 <range> 417 <min>-1</min> 418 <max>1</max> 419 </range> 420 <output>fcs/right-aileron-pos-norm</output> 421 </aerosurface_scale> 422 </channel> 423 <channel name="Yaw"> 424 <pure_gain name="Yaw Damper Gain"> 425 <input>velocities/r-rad_sec</input> 426 <gain>0.5</gain> 427 </pure_gain> 428 <summer name="Rudder Command Sum"> 429 <input>fcs/rudder-cmd-norm</input> 430 <input>fcs/yaw-trim-cmd-norm</input> 431 <clip> 432 <min>-1</min> 433 <max>1</max> 434 </clip> 435 </summer> 436 <aerosurface_scale name="Rudder Control"> 437 <input>fcs/rudder-command-sum</input> 438 <gain>0.01745</gain> 439 <range> 440 <min>-20</min> 441 <max>20</max> 442 </range> 443 <output>fcs/rudder-pos-rad</output> 444 </aerosurface_scale> 445 <aerosurface_scale name="Rudder Normalized"> 446 <input>fcs/rudder-pos-rad</input> 447 <domain> 448 <min>-0.35</min> 449 <max>0.35</max> 450 </domain> 451 <range> 452 <min>-1</min> 453 <max>1</max> 454 </range> 455 <output>fcs/rudder-pos-norm</output> 456 </aerosurface_scale> 457 </channel> 458 <channel name="Aeromechanical"> 459 <kinematic name="Flaps Control"> 460 <input>fcs/flap-cmd-norm</input> 461 <traverse> 462 <setting> 463 <position>0</position> 464 <time>0</time> 465 </setting> 466 <setting> 467 <position>.33</position> 468 <time>3</time> 469 </setting> 470 <setting> 471 <position>.66</position> 472 <time>1</time> 473 </setting> 474 <setting> 475 <position>1</position> 476 <time>1</time> 477 </setting> 478 </traverse> 479 <output>fcs/flap-pos-norm</output> 480 </kinematic> 481 <kinematic name="Gear Control"> 482 <input>gear/gear-cmd-norm</input> 483 <traverse> 484 <setting> 485 <position>0</position> 486 <time>0</time> 487 </setting> 488 <setting> 489 <position>1</position> 490 <time>4</time> 491 </setting> 492 </traverse> 493 <output>gear/gear-pos-norm</output> 494 </kinematic> 495 <kinematic name="Speedbrake Control"> 496 <input>fcs/speedbrake-cmd-norm</input> 497 <traverse> 498 <setting> 499 <position>0</position> 500 <time>0</time> 501 </setting> 502 <setting> 503 <position>1</position> 504 <time>3</time> 505 </setting> 506 </traverse> 507 <output>fcs/speedbrake-pos-norm</output> 508 </kinematic> 509 </channel> 510 </flight_control> 511 <aerodynamics> 512 <function name="aero/function/kCLge"> 513 <description>Change_in_lift_due_to_ground_effect</description> 514 <product> 515 <table> 516 <independentVar>aero/h_b-mac-ft</independentVar> 517 <tableData> 518 0.0000 1.4000 519 0.1000 1.3500 520 0.1500 1.2950 521 0.2000 1.2400 522 0.3000 1.1730 523 0.4000 1.1030 524 0.5000 1.0340 525 0.6000 1.0460 526 0.7000 1.0190 527 0.8000 1.0100 528 0.9000 1.0050 529 1.0000 1.0000 530 1.1000 1.0000 531 </tableData> 532 </table> 533 </product> 534 </function> 535 <axis name="DRAG"> 536 <function name="aero/coefficient/CDalpha"> 537 <description>Drag_due_to_alpha</description> 538 <product> 539 <property>aero/qbar-psf</property> 540 <property>metrics/Sw-sqft</property> 541 <table> 542 <independentVar>aero/alpha-rad</independentVar> 543 <tableData> 544 -1.5700 1.5000 545 -0.2600 0.0490 546 0.0000 0.0270 547 0.2600 0.0490 548 1.5700 1.5000 549 </tableData> 550 </table> 551 </product> 552 </function> 553 <function name="aero/coefficient/CDi"> 554 <description>Induced_drag</description> 555 <product> 556 <property>aero/qbar-psf</property> 557 <property>metrics/Sw-sqft</property> 558 <property>aero/cl-squared</property> 559 <value>0.0470</value> 560 </product> 561 </function> 562 <function name="aero/coefficient/CDflap"> 563 <description>Drag_due_to_flaps</description> 564 <product> 565 <property>aero/qbar-psf</property> 566 <property>metrics/Sw-sqft</property> 567 <table> 568 <independentVar>fcs/flap-pos-deg</independentVar> 569 <tableData> 570 0.0000 0.0000 571 30.0000 0.0260 572 60.0000 0.0600 573 </tableData> 574 </table> 575 </product> 576 </function> 577 <function name="aero/coefficient/CDgear"> 578 <description>Drag_due_to_gear</description> 579 <product> 580 <property>aero/qbar-psf</property> 581 <property>metrics/Sw-sqft</property> 582 <table> 583 <independentVar>gear/gear-pos-norm</independentVar> 584 <tableData> 585 0.0000 0.0000 586 1.0000 0.0340 587 </tableData> 588 </table> 589 </product> 590 </function> 591 <function name="aero/coefficient/CDsb"> 592 <description>Drag_due_to_speedbrakes</description> 593 <product> 594 <property>aero/qbar-psf</property> 595 <property>metrics/Sw-sqft</property> 596 <table> 597 <independentVar>fcs/speedbrake-pos-norm</independentVar> 598 <tableData> 599 0.0000 0.0000 600 1.0000 0.1100 601 </tableData> 602 </table> 603 </product> 604 </function> 605 <function name="aero/coefficient/CDbeta"> 606 <description>Drag_due_to_sideslip</description> 607 <product> 608 <property>aero/qbar-psf</property> 609 <property>metrics/Sw-sqft</property> 610 <table> 611 <independentVar>aero/beta-rad</independentVar> 612 <tableData> 613 -1.5700 1.2300 614 -0.2600 0.0470 615 0.0000 0.0000 616 0.2600 0.0470 617 1.5700 1.2300 618 </tableData> 619 </table> 620 </product> 621 </function> 622 <function name="aero/coefficient/CDde"> 623 <description>Drag_due_to_Elevator_Deflection</description> 624 <product> 625 <property>aero/qbar-psf</property> 626 <property>metrics/Sw-sqft</property> 627 <table> 628 <independentVar>fcs/elevator-pos-norm</independentVar> 629 <tableData> 630 -1.0000 0.0380 631 -0.7500 0.0260 632 -0.5000 0.0160 633 -0.2500 0.0080 634 0.0000 0.0040 635 0.2500 0.0120 636 0.5000 0.0190 637 0.7500 0.0280 638 1.0000 0.0400 639 </tableData> 640 </table> 641 </product> 642 </function> 643 </axis> 644 <axis name="SIDE"> 645 <function name="aero/coefficient/CYb"> 646 <description>Side_force_due_to_beta</description> 647 <product> 648 <property>aero/qbar-psf</property> 649 <property>metrics/Sw-sqft</property> 650 <property>aero/beta-rad</property> 651 <value>-0.7000</value> 652 </product> 653 </function> 654 </axis> 655 <axis name="LIFT"> 656 <function name="aero/coefficient/CLalpha"> 657 <description>Lift_due_to_alpha</description> 658 <product> 659 <property>aero/qbar-psf</property> 660 <property>metrics/Sw-sqft</property> 661 <property>aero/function/kCLge</property> 662 <table> 663 <independentVar>aero/alpha-rad</independentVar> 664 <tableData> 665 -1.5700 -1.5000 666 -0.2000 -0.6500 667 0.0000 0.2900 668 0.2300 1.3600 669 0.6000 0.6500 670 1.5700 0.0500 671 </tableData> 672 </table> 673 </product> 674 </function> 675 <function name="aero/coefficient/dCLflap"> 676 <description>Delta_Lift_due_to_flaps</description> 677 <product> 678 <property>aero/qbar-psf</property> 679 <property>metrics/Sw-sqft</property> 680 <property>aero/function/kCLge</property> 681 <table> 682 <independentVar>fcs/flap-pos-deg</independentVar> 683 <tableData> 684 0.0000 0.0000 685 30.0000 0.3600 686 60.0000 0.4100 687 </tableData> 688 </table> 689 </product> 690 </function> 691 <function name="aero/coefficient/CLde"> 692 <description>Lift_due_to_Elevator_Deflection</description> 693 <product> 694 <property>aero/qbar-psf</property> 695 <property>metrics/Sw-sqft</property> 696 <property>aero/function/kCLge</property> 697 <table> 698 <independentVar>fcs/elevator-pos-rad</independentVar> 699 <tableData> 700 -0.3490 -0.0664 701 -0.1750 -0.0338 702 0.0000 0.0000 703 0.1750 0.0327 704 0.2970 0.0614 705 </tableData> 706 </table> 707 </product> 708 </function> 709 </axis> 710 <axis name="ROLL"> 711 <function name="aero/coefficient/Clb"> 712 <description>Roll_moment_due_to_beta</description> 713 <product> 714 <property>aero/qbar-psf</property> 715 <property>metrics/Sw-sqft</property> 716 <property>metrics/bw-ft</property> 717 <property>aero/beta-rad</property> 718 <value>-0.1000</value> 719 </product> 720 </function> 721 <function name="aero/coefficient/Clp"> 722 <description>Roll_moment_due_to_roll_rate_(roll_damping)</description> 723 <product> 724 <property>aero/qbar-psf</property> 725 <property>metrics/Sw-sqft</property> 726 <property>metrics/bw-ft</property> 727 <property>aero/bi2vel</property> 728 <property>velocities/p-aero-rad_sec</property> 729 <table> 730 <independentVar>aero/alpha-rad</independentVar> 731 <tableData> 732 -1.5700 -0.3400 733 -0.2600 -0.3700 734 0.0000 -0.4000 735 0.2600 -0.3700 736 1.5700 -0.3400 737 </tableData> 738 </table> 739 </product> 740 </function> 741 <function name="aero/coefficient/Clr"> 742 <description>Roll_moment_due_to_yaw_rate</description> 743 <product> 744 <property>aero/qbar-psf</property> 745 <property>metrics/Sw-sqft</property> 746 <property>metrics/bw-ft</property> 747 <property>aero/bi2vel</property> 748 <property>velocities/r-aero-rad_sec</property> 749 <value>0.0025</value> 750 </product> 751 </function> 752 <function name="aero/coefficient/Cldal"> 753 <description>Roll_moment_due_to_aileron_left</description> 754 <product> 755 <property>aero/qbar-psf</property> 756 <property>metrics/Sw-sqft</property> 757 <property>metrics/bw-ft</property> 758 <table> 759 <independentVar lookup="row">fcs/left-aileron-pos-rad</independentVar> 760 <independentVar lookup="column">velocities/mach</independentVar> 761 <tableData> 762 0.0000 0.9000 763 -0.2617 -0.0180 -0.0150 764 -0.1745 -0.0120 -0.0105 765 -0.0872 -0.0068 -0.0057 766 0.0000 0.0000 0.0000 767 0.0872 0.0040 0.0026 768 0.1745 0.0087 0.0059 769 </tableData> 770 </table> 771 </product> 772 </function> 773 <function name="aero/coefficient/Cldar"> 774 <description>Roll_moment_due_to_aileron_right</description> 775 <product> 776 <property>aero/qbar-psf</property> 777 <property>metrics/Sw-sqft</property> 778 <property>metrics/bw-ft</property> 779 <table> 780 <independentVar lookup="row">fcs/right-aileron-pos-rad</independentVar> 781 <independentVar lookup="column">velocities/mach</independentVar> 782 <tableData> 783 0.0000 0.9000 784 -0.2617 0.0180 0.0150 785 -0.1745 0.0120 0.0105 786 -0.0872 0.0068 0.0057 787 0.0000 0.0000 0.0000 788 0.0872 -0.0040 -0.0026 789 0.1745 -0.0087 -0.0059 790 </tableData> 791 </table> 792 </product> 793 </function> 794 </axis> 795 <axis name="PITCH"> 796 <function name="aero/coefficient/Cmalpha"> 797 <description>Pitch_moment_due_to_alpha</description> 798 <product> 799 <property>aero/qbar-psf</property> 800 <property>metrics/Sw-sqft</property> 801 <property>metrics/cbarw-ft</property> 802 <property>aero/alpha-rad</property> 803 <value>-0.5000</value> 804 </product> 805 </function> 806 <function name="aero/coefficient/Cmdf"> 807 <description>Pitch_moment_due_to_flaps</description> 808 <product> 809 <property>aero/qbar-psf</property> 810 <property>metrics/Sw-sqft</property> 811 <table> 812 <independentVar>fcs/flap-pos-deg</independentVar> 813 <tableData> 814 0.0000 0.0000 815 30.0000 -0.0200 816 60.0000 -0.0300 817 </tableData> 818 </table> 819 </product> 820 </function> 821 <function name="aero/coefficient/Cmde"> 822 <description>Pitch_moment_due_to_elevator</description> 823 <product> 824 <property>aero/qbar-psf</property> 825 <property>metrics/Sw-sqft</property> 826 <property>metrics/cbarw-ft</property> 827 <table> 828 <independentVar lookup="row">fcs/elevator-pos-rad</independentVar> 829 <independentVar lookup="column">velocities/mach</independentVar> 830 <tableData> 831 0.0000 0.9000 832 -0.3490 0.3400 0.3190 833 -0.1750 0.1810 0.1510 834 0.0000 0.0140 0.0100 835 0.1750 -0.1680 -0.1430 836 0.2970 -0.2770 -0.2530 837 </tableData> 838 </table> 839 </product> 840 </function> 841 <function name="aero/coefficient/Cmq"> 842 <description>Pitch_moment_due_to_pitch_rate_(pitch_damping)</description> 843 <product> 844 <property>aero/qbar-psf</property> 845 <property>metrics/Sw-sqft</property> 846 <property>metrics/cbarw-ft</property> 847 <property>aero/ci2vel</property> 848 <property>velocities/q-aero-rad_sec</property> 849 <value>-15.0000</value> 850 </product> 851 </function> 852 <function name="aero/coefficient/Cmadot"> 853 <description>Pitch_moment_due_to_alpha_rate</description> 854 <product> 855 <property>aero/qbar-psf</property> 856 <property>metrics/Sw-sqft</property> 857 <property>metrics/cbarw-ft</property> 858 <property>aero/ci2vel</property> 859 <property>aero/alphadot-rad_sec</property> 860 <table> 861 <independentVar>velocities/mach</independentVar> 862 <tableData> 863 0.0000 -10.5000 864 0.3000 -9.0000 865 0.6000 -7.9000 866 0.9000 -7.0000 867 </tableData> 868 </table> 869 </product> 870 </function> 871 </axis> 872 <axis name="YAW"> 873 <function name="aero/coefficient/Cnb"> 874 <description>Yaw_moment_due_to_beta</description> 875 <product> 876 <property>aero/qbar-psf</property> 877 <property>metrics/Sw-sqft</property> 878 <property>metrics/bw-ft</property> 879 <property>aero/beta-rad</property> 880 <value>0.1000</value> 881 </product> 882 </function> 883 <function name="aero/coefficient/Cnr"> 884 <description>Yaw_moment_due_to_yaw_rate_(yaw_damping)</description> 885 <product> 886 <property>aero/qbar-psf</property> 887 <property>metrics/Sw-sqft</property> 888 <property>metrics/bw-ft</property> 889 <property>aero/bi2vel</property> 890 <property>velocities/r-aero-rad_sec</property> 891 <value>-0.2400</value> 892 </product> 893 </function> 894 <function name="aero/coefficient/Cnp"> 895 <description>Yaw_moment_due_to_roll_rate</description> 896 <product> 897 <property>aero/qbar-psf</property> 898 <property>metrics/Sw-sqft</property> 899 <property>metrics/bw-ft</property> 900 <property>aero/bi2vel</property> 901 <property>velocities/p-aero-rad_sec</property> 902 <value>-0.0300</value> 903 </product> 904 </function> 905 <function name="aero/coefficient/Cndr"> 906 <description>Yaw_moment_due_to_rudder</description> 907 <product> 908 <property>aero/qbar-psf</property> 909 <property>metrics/Sw-sqft</property> 910 <property>metrics/bw-ft</property> 911 <table> 912 <independentVar>fcs/rudder-pos-rad</independentVar> 913 <tableData> 914 -0.3490 0.0360 915 -0.2620 0.0250 916 -0.1750 0.0160 917 -0.0870 0.0070 918 0.0000 0.0000 919 0.0870 -0.0070 920 0.1750 -0.0160 921 0.2620 -0.0250 922 0.3490 -0.0360 923 </tableData> 924 </table> 925 </product> 926 </function> 927 <function name="aero/coefficient/Cnda_l"> 928 <description>Adverse_yaw_left_aileron</description> 929 <product> 930 <property>aero/qbar-psf</property> 931 <property>metrics/Sw-sqft</property> 932 <property>metrics/bw-ft</property> 933 <table> 934 <independentVar>fcs/left-aileron-pos-rad</independentVar> 935 <tableData> 936 -0.2620 0.0002 937 -0.1750 0.0001 938 -0.0870 0.0000 939 0.0000 0.0000 940 0.0870 -0.0000 941 0.1750 -0.0001 942 </tableData> 943 </table> 944 </product> 945 </function> 946 <function name="aero/coefficient/Cnda_r"> 947 <description>Adverse_yaw_right_aileron</description> 948 <product> 949 <property>aero/qbar-psf</property> 950 <property>metrics/Sw-sqft</property> 951 <property>metrics/bw-ft</property> 952 <table> 953 <independentVar>fcs/right-aileron-pos-rad</independentVar> 954 <tableData> 955 -0.2620 -0.0002 956 -0.1750 -0.0001 957 -0.0870 -0.0000 958 0.0000 0.0000 959 0.0870 0.0000 960 0.1750 0.0001 961 </tableData> 962 </table> 963 </product> 964 </function> 965 </axis> 966 </aerodynamics> 967</fdm_config> 968