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jsbsim.js

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JSBSim flight dynamics model ported to JavaScript

github.com/csbrandt/JSBSim.js

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<?xml version="1.0"?> <!-- File: F119-PW-100.xml Author: Aero-Matic v 0.8 Inputs: name: F119-PW-100 type: turbine thrust: 37000.8 lb augmented? yes injected? no --> <turbine_engine name="F119-PW-100"> <milthrust> 26950.0 </milthrust> <maxthrust> 37000.0 </maxthrust> <bypassratio> 0.2 </bypassratio> <tsfc> 0.8 </tsfc> <atsfc> 1.95 </atsfc> <idlen1> 40.0 </idlen1> <idlen2> 53.0 </idlen2> <maxn1> 100.0 </maxn1> <maxn2> 100.0 </maxn2> <augmented> 1 </augmented> <augmethod> 1 </augmethod> <injected> 0 </injected> <function name="IdleThrust"> <table> <independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="column">atmosphere/density-altitude</independentVar> <tableData> -10000 0 10000 20000 30000 40000 50000 60000 0.0 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467 0.0 0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342 0.0 0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203 0.0 0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073 0.0 0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900 0.0 1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800 0.0 </tableData> </table> </function> <function name="MilThrust"> <table> <independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="column">atmosphere/density-altitude</independentVar> <tableData> -10000 0 10000 20000 30000 40000 50000 60000 70000 80000 0.0 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490 0.0800 0.040 0.0 0.2 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430 0.0780 0.040 0.0 0.4 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450 0.0790 0.040 0.0 0.6 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540 0.0850 0.045 0.0 0.8 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700 0.0935 0.045 0.0 1.0 1.3690 1.1760 0.9135 0.6836 0.4988 0.3308 0.2048 0.1127 0.052 0.0 1.2 1.4850 1.2915 1.0238 0.7812 0.5723 0.3780 0.2363 0.1300 0.065 0.0 1.4 1.5941 1.4070 1.1403 0.8873 0.6595 0.4452 0.2762 0.1520 0.076 0.0 1.6 1.6211 1.5250 1.2450 0.9890 0.7774 0.5260 0.3211 0.1767 0.087 0.0 1.8 1.6211 1.6290 1.3474 1.0950 0.8774 0.6160 0.3811 0.2096 0.104 0.0 2.0 1.6211 1.6000 1.4300 1.1850 0.9500 0.7050 0.4435 0.2420 0.121 0.0 2.2 1.6211 1.6000 1.3600 1.1000 0.8600 0.6167 0.4000 0.2050 0.100 0.0 </tableData> </table> </function> <function name="AugThrust"> <table> <independentVar lookup="row">velocities/mach</independentVar> <independentVar lookup="column">atmosphere/density-altitude</independentVar> <tableData> -10000 0 10000 20000 30000 40000 50000 60000 70000 80000 0.0 1.1816 1.0000 0.8184 0.6627 0.5280 0.3756 0.2327 0.1279 0.063 0.0 0.2 1.1308 0.9599 0.7890 0.6406 0.5116 0.3645 0.2258 0.1242 0.062 0.0 0.4 1.1150 0.9474 0.7798 0.6340 0.5070 0.3615 0.2240 0.1232 0.061 0.0 0.6 1.1284 0.9589 0.7894 0.6420 0.5134 0.3661 0.2268 0.1240 0.062 0.0 0.8 1.1707 0.9990 0.8177 0.6647 0.5309 0.3784 0.2345 0.1290 0.065 0.0 1.0 1.2411 1.1056 0.9080 0.7367 0.5876 0.4182 0.2590 0.1425 0.071 0.0 1.2 1.3287 1.1817 0.9682 0.7835 0.6233 0.4430 0.2745 0.1513 0.075 0.0 1.4 1.4365 1.2756 1.0430 0.8422 0.6678 0.4735 0.2933 0.1613 0.081 0.0 1.6 1.5711 1.3923 1.1349 0.9135 0.7218 0.5103 0.3162 0.1739 0.085 0.0 1.8 1.7301 1.5307 1.2449 0.9987 0.7870 0.5553 0.3441 0.1893 0.095 0.0 2.0 1.8314 1.6485 1.3740 1.1000 0.8627 0.6708 0.3764 0.2070 0.103 0.0 2.2 1.9700 1.7745 1.4805 1.3020 0.9555 0.6676 0.4137 0.2275 0.115 0.0 2.4 2.0700 1.8900 1.6065 1.4070 1.0500 0.7560 0.4830 0.2657 0.138 0.0 2.6 2.2000 2.0160 1.7220 1.5120 1.1550 0.8400 0.5460 0.3003 0.150 0.0 </tableData> </table> </function> </turbine_engine>