FGR-yasim.xml 11 KB

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  1. <?xml version="1.0" encoding="UTF-8"?>
  2. <!-- FGR2 Phantom II
  3. <airplane mass="31000" version="YASIM_VERSION_CURRENT">-->
  4. <airplane mass="31000" version="YASIM_VERSION_CURRENT">
  5. <!-- Approach configuration -->
  6. <approach speed="130" aoa="8" fuel="0.1">
  7. <control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
  8. <control-setting axis="/controls/engines/engine[1]/throttle" value="0.2"/>
  9. <control-setting axis="/controls/flight/flaps" value="1.0"/>
  10. <control-setting axis="/controls/flight/spoilers" value="0.5"/>
  11. <control-setting axis="/controls/gear/gear-down" value="1"/>
  12. </approach>
  13. <!-- Cruise configuration -->
  14. <!--
  15. <cruise speed="1204" alt="40000" fuel="0.41">
  16. -->
  17. <cruise speed="700" alt="40000" fuel="0.41">
  18. <control-setting axis="/controls/engines/engine[0]/throttle" value="0.84"/>
  19. <control-setting axis="/controls/engines/engine[1]/throttle" value="0.84"/>
  20. <control-setting axis="/controls/flight/flaps" value="0.0"/>
  21. <control-setting axis="/controls/gear/gear-down" value="0"/>
  22. </cruise>
  23. <!-- pilot eyepoint -->
  24. <cockpit x="5.5" y="0.0" z="1.0"/>
  25. <fuselage ax="9.3" ay="0" az="0" bx="4" by="0" bz="0.78" width="1.8" taper="0.2" midpoint="1" idrag="0.3"/>
  26. <fuselage ax="4" ay="0" az="0.78" bx="-4" by="0" bz="0.7" width="1.8" taper="1" midpoint="0" idrag="0.3"/>
  27. <fuselage ax="-4" ay="0" az="0.78" bx="-8.6" by="0" bz="1.3" width="1.8" taper="0.2" midpoint="0" idrag="0.2"/>
  28. <!-- Engines -->
  29. <fuselage ax="4.5" ay="0.9" az="0.7" bx="-4.7" by="0.6" bz="0.3" width="1.0" taper= "1" midpoint= "0.8" idrag="0.3" />
  30. <fuselage ax="4.5" ay="-0.9" az="0.7" bx="-4.7" by="-0.6" bz="0.3" width="1.0" taper= "1" midpoint= "0.8" idrag="0.3" />
  31. <wing x="0.3" y="1.2" z="-0.1"
  32. chord="6.3"
  33. length="3.85"
  34. taper="0.54"
  35. incidence="1.4"
  36. twist="-2.0"
  37. idrag="0.5"
  38. sweep="37"
  39. dihedral="0">
  40. <stall aoa="21" width="8" peak="1.3"/>
  41. <flap0 start="0.01" end="0.47" lift="1.9" drag="1.4"/>
  42. <flap1 start="0.47" end="0.813" lift="1.2" drag="1.2"/>
  43. <slat aoa="4" start="0.04" end="0.813" lift="1.4" drag="1.3"/>
  44. <control-input axis="/controls/flight/flaps" control="FLAP0"/>
  45. <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
  46. <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
  47. <control-input axis="/controls/flight/flaps" control="SLAT"/>
  48. <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
  49. <control-output control="FLAP1" prop="/surface-positions/aileron-pos-norm"/>
  50. <control-output control="SLAT" prop="surface-positions/slat-pos-norm"/>
  51. <control-speed control="SLAT" transition-time="1.9"/>
  52. <control-speed control="FLAP0" transition-time="15"/>
  53. <control-speed control="FLAP1" transition-time="0.25"/>
  54. </wing>
  55. <!-- Wing end -->
  56. <mstab x="-2" y="4.3" z="-0.1" chord="3.4"
  57. length="2.6"
  58. taper="0.4"
  59. incidence="1.4"
  60. sweep="37"
  61. dihedral="14"
  62. camber="-0.05">
  63. <stall aoa="18" width="2" peak="1.3"/>
  64. </mstab>
  65. <!-- body -->
  66. <mstab x="0" y="0" z="0.173" chord="7"
  67. length="1.025"
  68. taper="1"
  69. incidence="0"
  70. sweep="0"
  71. dihedral="0"
  72. camber="-0.05">
  73. <stall aoa="18" width="2" peak="1.3"/>
  74. <flap0 start="0.01" end="0.47" lift="1.1" drag="29.9"/>
  75. <control-input axis="/controls/flight/speedbrake" control="FLAP0"/>
  76. <control-output control="FLAP0" prop="/surface-positions/speedbrake-pos-norm"/>
  77. <control-speed control="FLAP0" transition-time="4"/>
  78. </mstab>
  79. <hstab x="-6.976" y="0.220" z="1.05"
  80. taper="0.38"
  81. length="3"
  82. chord="2.8"
  83. incidence="-1.7"
  84. sweep="30"
  85. dihedral="-25">
  86. <stall aoa="35" width="33" peak="2"/>
  87. <flap0 start="0.01" end="1.7" lift="1.65" drag="1.4"/>
  88. <control-input axis="/controls/flight/elevator" control="FLAP0"/>
  89. <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
  90. <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
  91. <control-speed control="FLAP0" transition-time="0.4"/>
  92. </hstab>
  93. <vstab x="-5.7" y="0" z="1.3"
  94. chord="6.1"
  95. length="3"
  96. taper="0.20"
  97. incidence="0"
  98. sweep="50">
  99. <stall aoa="27" width="10" peak="1.5"/>
  100. <flap0 start="0.1" end=".8" lift="1.3" drag="1.3"/>
  101. <control-input axis="/controls/flight/rudder" control="FLAP0" invert="true"/>
  102. <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>
  103. <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>
  104. <control-speed control="FLAP0" transition-time="1"/>
  105. </vstab>
  106. <!-- Engines source : http://en.wikipedia.org/wiki/Rolls-Royce_Spey
  107. name : Rolls-Royce Spey
  108. type : Turbofan
  109. power cruise : 12150 lbf
  110. adterburner : 20515 lbf
  111. weight : 4093 lb
  112. -->
  113. <jet x="0" y="0.555" z="-0.334"
  114. mass="4093"
  115. thrust="12140"
  116. afterburner="20515"
  117. n1-idle="1"
  118. n1-max="125" >
  119. <actionpt x="-2.561" y="0.483" z="-0.572"/>
  120. <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
  121. <control-input axis="/controls/engines/engine[0]/throttle" src0="0.85" dst0="0.0" src1="1.0" dst1="1.0" control="REHEAT"/>
  122. <control-output control="REHEAT" prop="engines/engine[0]/afterburner" />
  123. </jet>
  124. <jet x="0" y="-0.555" z="-0.334"
  125. mass="4093"
  126. thrust="12140"
  127. afterburner="20515"
  128. n1-idle="1"
  129. n1-max="125" >
  130. <actionpt x="-2.561" y="-0.483" z="-0.572"/>
  131. <control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
  132. <control-input axis="/controls/engines/engine[1]/throttle" src0="0.85" dst0="0.0" src1="1.0" dst1="1.0" control="REHEAT"/>
  133. <control-output control="REHEAT" prop="engines/engine[1]/afterburner" />
  134. </jet>
  135. <!-- nose -->
  136. <gear x="6.423" y="0" z="-1.970"
  137. retract-time="8"
  138. compression="0.7"
  139. spring="1.1"
  140. damp="1.4">
  141. <control-input axis="/controls/flight/rudder" control="STEER" square="false"/>
  142. <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
  143. <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
  144. <control-speed control="EXTEND" transition-time="7"/>
  145. </gear>
  146. <!-- left main -->
  147. <gear x="-0.664" y="2.695" z="-2.060"
  148. retract-time="8"
  149. compression="0.8"
  150. spring="0.85"
  151. damp="2">
  152. <control-input axis="/controls/gear/brake-left" control="BRAKE"/><control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
  153. <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
  154. <control-output control="EXTEND" prop="gear/gear[1]/position-norm"/>
  155. <control-speed control="EXTEND" transition-time="7"/>
  156. </gear>
  157. <!-- right main -->
  158. <gear x="-0.664" y="-2.695" z="-2.060"
  159. retract-time="8"
  160. compression="0.8"
  161. spring="0.85"
  162. damp="2">
  163. <control-input axis="/controls/gear/brake-right" control="BRAKE"/>
  164. <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
  165. <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
  166. <control-output control="EXTEND" prop="gear/gear[2]/position-norm"/>
  167. <control-speed control="EXTEND" transition-time="7"/>
  168. </gear>
  169. <!-- FUEL tank1 -->
  170. <tank x="0.6" y=" 0.0" z="1.0" jet="true" capacity="6000"/>
  171. <!-- FUEL feed -->
  172. <tank x="1.5" y=" 0.0" z="1.0" jet="true" capacity="1400"/>
  173. <tank x="2.5" y=" 0.0" z="1.0" jet="true" capacity="2100"/>
  174. <!-- FUEL Wing -->
  175. <tank x="0.3" y= "3.0" z="-0.1" jet="true" capacity="2100"/>
  176. <tank x="0.3" y="-3.0" z="-0.1" jet="true" capacity="2100"/>
  177. <!-- EXT TANK -->
  178. <tank x="0.0" y= " 0.0" z="-0.8" jet="true" capacity="3950"/>
  179. <tank x="0.0" y= " 3.3" z="-0.8" jet="true" capacity="2500"/>
  180. <tank x="0.0" y= "-3.3" z="-0.8" jet="true" capacity="2500"/>
  181. <!-- Internal tanks
  182. <tank x="3.5" y="0" z="0.6" jet="true" capacity="1004"/>
  183. <tank x="2.75" y="0" z="0.6" jet="true" capacity="1004"/>
  184. <tank x="1.1" y="0.0" z="0.6" jet="true" capacity="1004"/>
  185. <tank x="0" y="0.0" z="0.6" jet="true" capacity="1004"/>
  186. <tank x="-1.1" y="0.0" z="0.6" jet="true" capacity="1004"/>
  187. <tank x="-2.0" y="0" z="0.6" jet="true" capacity="1004"/>
  188. <tank x="-3.1" y="0" z="0.6" jet="true" capacity="1004"/>-->
  189. <!-- left wing internal tank
  190. <tank x="0" y="1.4" z="0" jet="true" capacity="1004"/>-->
  191. <!-- right wing internal tank
  192. <tank x="0" y="-1.4" z="0" jet="true" capacity="1004"/>-->
  193. <!-- left wing drop tank
  194. <tank x="0" y="3.65" z="0" jet="true" capacity="4080"/>-->
  195. <!-- centre drop tank
  196. <tank x="0.5" y="0" z="-0.6" jet="true" capacity="4080"/>-->
  197. <!-- right wing drop tanks
  198. <tank x="0" y="-3.65" z="0" jet="true" capacity="4080"/>-->
  199. <!-- ballast -->
  200. <ballast x="6.7" y="0" z="-1.59" mass="3000"/>
  201. <ballast x="5.74" y="0" z="-0.35" mass="1200"/>
  202. <ballast x="4" y="0" z="0.2" mass="4900"/>
  203. <!-- ballast -->
  204. <ballast x="5.05" y="0" z="-0.1" mass="200"/>
  205. <ballast x="-0.8" y="3" z="-1.59" mass="200"/>
  206. <ballast x="-0.8" y="-3" z="-1.59" mass="200"/>
  207. <!-- Parachute -->
  208. <!-- X axis - force forward -->
  209. <thruster x="-7.015" y="-0.108" z="0.720" vx="1" vy="0" vz="0"
  210. thrust="10000">
  211. <control-input axis="/controls/engines/thruster[1]/throttle" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
  212. </thruster>
  213. <!-- Y axis - force left -->
  214. <thruster x="-7.015" y="-0.108" z="0.720" vx="0" vy="1" vz="0"
  215. thrust="10000">
  216. <control-input axis="/controls/engines/thruster[2]/throttle" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
  217. </thruster>
  218. <!-- Z axis - force up -->
  219. <thruster x="-7.015" y="-0.108" z="0.720" vx="0" vy="0" vz="1"
  220. thrust="10000">
  221. <control-input axis="/controls/engines/thruster[3]/throttle" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
  222. </thruster>
  223. <!-- Hook -->
  224. <hook x="-4.8" y="0" z="-0.282"
  225. length="2.571"
  226. down-angle="60"
  227. up-angle="-18.6">
  228. <control-input axis="/controls/gear/tailhook" control="HEXTEND"/>
  229. <control-speed control="HEXTEND" transition-time="1.35"/>
  230. </hook>
  231. <!-- Launch-bar -0.780453-->
  232. <launchbar x="6.8"
  233. y="0.0"
  234. z="-1.0"
  235. length="3.5052">
  236. <!--down-angle="90"
  237. up-angle="0"
  238. holdback-x="-16.3"
  239. holdback-y="0.0"
  240. holdback-z="0.1175"
  241. holdback-length="2.0"-->
  242. <control-input axis="/controls/gear/launchbar"
  243. control="LEXTEND"/>
  244. <control-speed control="LEXTEND"
  245. transition-time="1"/>
  246. <control-input axis="/controls/gear/launchbar/acceleration-norm"
  247. control="LACCEL"/>
  248. </launchbar>
  249. <!-- Stores -->
  250. <weight x="0"
  251. y="3.65"
  252. z="0"
  253. size="0.9"
  254. mass-prop="sim/weight[0]/weight-lb"/>
  255. <weight x="1.5"
  256. y="2.17"
  257. z="-0.55"
  258. size="0.6"
  259. mass-prop="sim/weight[1]/weight-lb"/>
  260. <weight x="3.5"
  261. y="0.45"
  262. z="-0.25"
  263. size="0.3"
  264. mass-prop="sim/weight[2]/weight-lb"/>
  265. <weight x="-1.8"
  266. y="1.1"
  267. z="-0.36"
  268. size="0.3"
  269. mass-prop="sim/weight[3]/weight-lb"/>
  270. <weight x="0"
  271. y="0"
  272. z="-0.8"
  273. size="0.95"
  274. mass-prop="sim/weight[4]/weight-lb"/>
  275. <weight x="-1.8"
  276. y="-1.1"
  277. z="-0.36"
  278. size="0.3"
  279. mass-prop="sim/weight[5]/weight-lb"/>
  280. <weight x="3.5"
  281. y="0.45"
  282. z="-0.25"
  283. size="0.3"
  284. mass-prop="sim/weight[6]/weight-lb"/>
  285. <weight x="1.5"
  286. y="-2.17"
  287. z="-0.55"
  288. size="0.6"
  289. mass-prop="sim/weight[7]/weight-lb"/>
  290. <weight x="0"
  291. y="-3.65"
  292. z="0"
  293. size="0.9"
  294. mass-prop="sim/weight[8]/weight-lb"/>
  295. </airplane>