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Path: blob/master/Tools/autotest/aircraft/Rascal/Rascal.xml
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<?xml version="1.0"?>1<?xml-stylesheet href="http://jsbsim.sourceforge.net/JSBSim.xsl" type="text/xsl"?>2<fdm_config name="rascal" version="2.0" release="BETA"3xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"4xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">56<fileheader>7<author> Author Name </author>8<filecreationdate> Creation Date </filecreationdate>9<version> Version </version>10<description> Models a rascal </description>11</fileheader>1213<metrics>14<wingarea unit="FT2"> 10.57 </wingarea>15<wingspan unit="FT"> 9.17 </wingspan>16<chord unit="FT"> 1.15 </chord>17<htailarea unit="FT2"> 1.69 </htailarea>18<htailarm unit="FT"> 3.28 </htailarm>19<vtailarea unit="FT2"> 1.06 </vtailarea>20<vtailarm unit="FT"> 0 </vtailarm>21<location name="AERORP" unit="IN">22<x> 37.4 </x>23<y> 0 </y>24<z> 0 </z>25</location>26<location name="EYEPOINT" unit="IN">27<x> 20 </x>28<y> 0 </y>29<z> 5 </z>30</location>31<location name="VRP" unit="IN">32<x> 0 </x>33<y> 0 </y>34<z> 0 </z>35</location>36</metrics>3738<mass_balance>39<ixx unit="SLUG*FT2"> 1.95 </ixx>40<iyy unit="SLUG*FT2"> 1.55 </iyy>41<izz unit="SLUG*FT2"> 1.91 </izz>42<ixy unit="SLUG*FT2"> 0 </ixy>43<ixz unit="SLUG*FT2"> 0 </ixz>44<iyz unit="SLUG*FT2"> 0 </iyz>45<emptywt unit="LBS"> 13 </emptywt>46<location name="CG" unit="IN">47<x> 36.4 </x>48<y> 0 </y>49<z> 4 </z>50</location>51</mass_balance>5253<ground_reactions>54<contact type="BOGEY" name="LEFT_MLG">55<location unit="IN">56<x> 33.1 </x>57<y> -12.9 </y>58<z> -13.1 </z>59</location>60<static_friction> 0.8 </static_friction>61<dynamic_friction> 0.5 </dynamic_friction>62<rolling_friction> 0.1 </rolling_friction>63<spring_coeff unit="LBS/FT"> 480 </spring_coeff>64<damping_coeff unit="LBS/FT/SEC"> 100 </damping_coeff>65<max_steer unit="DEG"> 0.0 </max_steer>66<brake_group> NONE </brake_group>67<retractable>0</retractable>68</contact>69<contact type="BOGEY" name="RIGHT_MLG">70<location unit="IN">71<x> 33.1 </x>72<y> 12.9 </y>73<z> -13.1 </z>74</location>75<static_friction> 0.8 </static_friction>76<dynamic_friction> 0.5 </dynamic_friction>77<rolling_friction> 0.1 </rolling_friction>78<spring_coeff unit="LBS/FT"> 480 </spring_coeff>79<damping_coeff unit="LBS/FT/SEC"> 100 </damping_coeff>80<max_steer unit="DEG"> 0.0 </max_steer>81<brake_group> NONE </brake_group>82<retractable>0</retractable>83</contact>84<contact type="BOGEY" name="TAIL_LG">85<location unit="IN">86<x> 68.9 </x>87<y> 0 </y>88<z> -4 </z>89</location>90<static_friction> 0.8 </static_friction>91<dynamic_friction> 0.5 </dynamic_friction>92<rolling_friction> 0.1 </rolling_friction>93<spring_coeff unit="LBS/FT"> 480 </spring_coeff>94<damping_coeff unit="LBS/FT/SEC"> 100 </damping_coeff>95<max_steer unit="DEG"> 360.0 </max_steer>96<brake_group> NONE </brake_group>97<retractable>0</retractable>98</contact>99</ground_reactions>100101<propulsion>102<engine file="Zenoah_G-26A">103<location unit="IN">104<x> 36 </x>105<y> 0 </y>106<z> 0 </z>107</location>108<orient unit="DEG">109<roll> 0.0 </roll>110<pitch> 0 </pitch>111<yaw> 0 </yaw>112</orient>113<feed>0</feed>114<thruster file="18x8">115<location unit="IN">116<x> 1 </x>117<y> 0 </y>118<z> 0 </z>119</location>120<orient unit="DEG">121<roll> 0.0 </roll>122<pitch> 0.0 </pitch>123<yaw> 0.0 </yaw>124</orient>125<p_factor>1.0</p_factor>126</thruster>127</engine>128<tank type="FUEL"> <!-- Tank number 0 -->129<location unit="IN">130<x> 36.36 </x>131<y> 0 </y>132<z> -1.89375 </z>133</location>134<capacity unit="LBS"> 1.5 </capacity>135<contents unit="LBS"> 1.5 </contents>136</tank>137</propulsion>138139<flight_control name="FCS: rascal">140<channel name="All">141142<summer name="Pitch Trim Sum">143<input>fcs/elevator-cmd-norm</input>144<input>fcs/pitch-trim-cmd-norm</input>145<clipto>146<min>-1</min>147<max>1</max>148</clipto>149</summer>150151<aerosurface_scale name="Elevator Control">152<input>fcs/pitch-trim-sum</input>153<range>154<min>-0.35</min>155<max>0.3</max>156</range>157<output>fcs/elevator-pos-rad</output>158</aerosurface_scale>159160<aerosurface_scale name="Elevator Normalized">161<input>fcs/elevator-pos-rad</input>162<domain>163<min>-0.3</min>164<max> 0.3</max>165</domain>166<range>167<min>-1</min>168<max> 1</max>169</range>170<output>fcs/elevator-pos-norm</output>171</aerosurface_scale>172173<summer name="Roll Trim Sum">174<input>fcs/aileron-cmd-norm</input>175<input>fcs/roll-trim-cmd-norm</input>176<clipto>177<min>-1</min>178<max>1</max>179</clipto>180</summer>181182<aerosurface_scale name="Left Aileron Control">183<input>fcs/roll-trim-sum</input>184<range>185<min>-0.35</min>186<max>0.35</max>187</range>188<output>fcs/left-aileron-pos-rad</output>189</aerosurface_scale>190191<aerosurface_scale name="Right Aileron Control">192<input>-fcs/roll-trim-sum</input>193<range>194<min>-0.35</min>195<max>0.35</max>196</range>197<output>fcs/right-aileron-pos-rad</output>198</aerosurface_scale>199200<aerosurface_scale name="Left aileron Normalized">201<input>fcs/left-aileron-pos-rad</input>202<domain>203<min>-0.35</min>204<max> 0.35</max>205</domain>206<range>207<min>-1</min>208<max> 1</max>209</range>210<output>fcs/left-aileron-pos-norm</output>211</aerosurface_scale>212213<aerosurface_scale name="Right aileron Normalized">214<input>fcs/right-aileron-pos-rad</input>215<domain>216<min>-0.35</min>217<max> 0.35</max>218</domain>219<range>220<min>-1</min>221<max> 1</max>222</range>223<output>fcs/right-aileron-pos-norm</output>224</aerosurface_scale>225226<summer name="Rudder Command Sum">227<input>fcs/rudder-cmd-norm</input>228<input>fcs/yaw-trim-cmd-norm</input>229<clipto>230<min>-1</min>231<max>1</max>232</clipto>233</summer>234235<aerosurface_scale name="Rudder Control">236<input>fcs/rudder-command-sum</input>237<range>238<min>-0.35</min>239<max>0.35</max>240</range>241<output>fcs/rudder-pos-rad</output>242</aerosurface_scale>243244<aerosurface_scale name="Rudder Normalized">245<input>fcs/rudder-pos-rad</input>246<domain>247<min>-0.35</min>248<max> 0.35</max>249</domain>250<range>251<min>-1</min>252<max> 1</max>253</range>254<output>fcs/rudder-pos-norm</output>255</aerosurface_scale>256</channel>257</flight_control>258259<aerodynamics>260<axis name="DRAG">261<function name="aero/coefficient/CD0">262<description>Drag_at_zero_lift</description>263<product>264<property>aero/qbar-psf</property>265<property>metrics/Sw-sqft</property>266<table>267<independentVar>aero/alpha-rad</independentVar>268<tableData>269-1.5700 1.5000270-0.2600 0.05602710.0000 0.02802720.2600 0.05602731.5700 1.5000274</tableData>275</table>276</product>277</function>278<function name="aero/coefficient/CDi">279<description>Induced_drag</description>280<product>281<property>aero/qbar-psf</property>282<property>metrics/Sw-sqft</property>283<property>aero/cl-squared</property>284<value>0.0400</value>285</product>286</function>287<function name="aero/coefficient/CDbeta">288<description>Drag_due_to_sideslip</description>289<product>290<property>aero/qbar-psf</property>291<property>metrics/Sw-sqft</property>292<table>293<independentVar>aero/beta-rad</independentVar>294<tableData>295-1.5700 1.2300296-0.2600 0.05002970.0000 0.00002980.2600 0.05002991.5700 1.2300300</tableData>301</table>302</product>303</function>304<function name="aero/coefficient/CDde">305<description>Drag_due_to_Elevator_Deflection</description>306<product>307<property>aero/qbar-psf</property>308<property>metrics/Sw-sqft</property>309<property>fcs/elevator-pos-norm</property>310<value>0.0300</value>311</product>312</function>313</axis>314315<axis name="SIDE">316<function name="aero/coefficient/CYb">317<description>Side_force_due_to_beta</description>318<product>319<property>aero/qbar-psf</property>320<property>metrics/Sw-sqft</property>321<property>aero/beta-rad</property>322<value>-1.0000</value>323</product>324</function>325</axis>326327<axis name="LIFT">328<function name="aero/coefficient/CLalpha">329<description>Lift_due_to_alpha</description>330<product>331<property>aero/qbar-psf</property>332<property>metrics/Sw-sqft</property>333<table>334<independentVar>aero/alpha-rad</independentVar>335<tableData>336-0.2000 -0.75003370.0000 0.25003380.2300 1.40003390.6000 0.7100340</tableData>341</table>342</product>343</function>344<function name="aero/coefficient/CLde">345<description>Lift_due_to_Elevator_Deflection</description>346<product>347<property>aero/qbar-psf</property>348<property>metrics/Sw-sqft</property>349<property>fcs/elevator-pos-rad</property>350<value>0.2000</value>351</product>352</function>353</axis>354355<axis name="ROLL">356<function name="aero/coefficient/Clb">357<description>Roll_moment_due_to_beta</description>358<!-- aka dihedral effect -->359<product>360<property>aero/qbar-psf</property>361<property>metrics/Sw-sqft</property>362<property>metrics/bw-ft</property>363<property>aero/beta-rad</property>364<value>-0.1000</value>365</product>366</function>367<function name="aero/coefficient/Clp">368<description>Roll_moment_due_to_roll_rate</description>369<product>370<property>aero/qbar-psf</property>371<property>metrics/Sw-sqft</property>372<property>metrics/bw-ft</property>373<property>aero/bi2vel</property>374<property>velocities/p-aero-rad_sec</property>375<value>-0.4000</value>376</product>377</function>378<function name="aero/coefficient/Clr">379<description>Roll_moment_due_to_yaw_rate</description>380<product>381<property>aero/qbar-psf</property>382<property>metrics/Sw-sqft</property>383<property>metrics/bw-ft</property>384<property>aero/bi2vel</property>385<property>velocities/r-aero-rad_sec</property>386<value>0.1500</value>387</product>388</function>389<function name="aero/coefficient/Clda">390<description>Roll_moment_due_to_aileron</description>391<product>392<property>aero/qbar-psf</property>393<property>metrics/Sw-sqft</property>394<property>metrics/bw-ft</property>395<property>fcs/left-aileron-pos-rad</property>396<table>397<independentVar>velocities/mach</independentVar>398<tableData>3990.0000 0.13004002.0000 0.0570401</tableData>402</table>403</product>404</function>405<function name="aero/coefficient/Cldr">406<description>Roll_moment_due_to_rudder</description>407<product>408<property>aero/qbar-psf</property>409<property>metrics/Sw-sqft</property>410<property>metrics/bw-ft</property>411<property>fcs/rudder-pos-rad</property>412<value>0.0100</value>413</product>414</function>415</axis>416417<axis name="PITCH">418<function name="aero/coefficient/Cmalpha">419<description>Pitch_moment_due_to_alpha</description>420<product>421<property>aero/qbar-psf</property>422<property>metrics/Sw-sqft</property>423<property>metrics/cbarw-ft</property>424<property>aero/alpha-rad</property>425<value>-0.5000</value>426</product>427</function>428<function name="aero/coefficient/Cmde">429<description>Pitch_moment_due_to_elevator</description>430<product>431<property>aero/qbar-psf</property>432<property>metrics/Sw-sqft</property>433<property>metrics/cbarw-ft</property>434<property>fcs/elevator-pos-rad</property>435<table>436<independentVar>velocities/mach</independentVar>437<tableData>4380.0000 -0.5000 <!-- was -1.1 -->4392.0000 -0.2750440</tableData>441</table>442</product>443</function>444<function name="aero/coefficient/Cmq">445<description>Pitch_moment_due_to_pitch_rate</description>446<product>447<property>aero/qbar-psf</property>448<property>metrics/Sw-sqft</property>449<property>metrics/cbarw-ft</property>450<property>aero/ci2vel</property>451<property>velocities/q-aero-rad_sec</property>452<value>-12.0000</value>453</product>454</function>455<function name="aero/coefficient/Cmadot">456<description>Pitch_moment_due_to_alpha_rate</description>457<product>458<property>aero/qbar-psf</property>459<property>metrics/Sw-sqft</property>460<property>metrics/cbarw-ft</property>461<property>aero/ci2vel</property>462<property>aero/alphadot-rad_sec</property>463<value>-7.0000</value>464</product>465</function>466</axis>467468<axis name="YAW">469<function name="aero/coefficient/Cnb">470<description>Yaw_moment_due_to_beta</description>471<product>472<property>aero/qbar-psf</property>473<property>metrics/Sw-sqft</property>474<property>metrics/bw-ft</property>475<property>aero/beta-rad</property>476<value>0.1200</value>477</product>478</function>479<function name="aero/coefficient/Cnr">480<description>Yaw_moment_due_to_yaw_rate</description>481<product>482<property>aero/qbar-psf</property>483<property>metrics/Sw-sqft</property>484<property>metrics/bw-ft</property>485<property>aero/bi2vel</property>486<property>velocities/r-aero-rad_sec</property>487<value>-0.1500</value>488</product>489</function>490<function name="aero/coefficient/Cndr">491<description>Yaw_moment_due_to_rudder</description>492<product>493<property>aero/qbar-psf</property>494<property>metrics/Sw-sqft</property>495<property>metrics/bw-ft</property>496<property>fcs/rudder-pos-rad</property>497<value>-0.0500</value>498</product>499</function>500<function name="aero/coefficient/Cnda">501<description>Adverse_yaw</description>502<product>503<property>aero/qbar-psf</property>504<property>metrics/Sw-sqft</property>505<property>metrics/bw-ft</property>506<property>fcs/left-aileron-pos-rad</property>507<value>-0.0300</value>508</product>509</function>510<function name="aero/coefficient/Cndi">511<description>Yaw_moment_due_to_tail_incidence</description>512<product>513<property>aero/qbar-psf</property>514<property>metrics/Sw-sqft</property>515<property>metrics/bw-ft</property>516<value>0.0007</value>517</product>518</function>519</axis>520</aerodynamics>521522<!-- <output name="RascalOutputFile.csv" type="CSV" rate="10">523<rates> ON </rates>524<velocities> ON </velocities>525<position> ON </position>526<fcs> ON </fcs>527<propulsion> ON </propulsion>528</output> -->529530<input port="5505"/>531532</fdm_config>533534535