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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"?> <rocket_engine name="Estes E-9"> <!-- --> <isp> 244 </isp> <builduptime> 0.15 </builduptime> <thrust_table name="propulsion/thrust_prop_remain" type="internal"> <tableData> <!-- ========= ========= =========== ========= ===== Prop Burn Thrust Total Impls wdot Time (Wt, lbs) (lbf) (lbf-sec) (lbf/sec) (sec) ========= ========= =========== ========= ===== --> 0.00000, 0.02108 <!-- 0.00000, 0.00009, 0.0000 --> 0.00002, 0.21044 <!-- 0.00469, 0.00086, 0.0406 --> 0.00022, 1.62214 <!-- 0.05456, 0.00665, 0.0950 --> 0.00072, 3.72941 <!-- 0.17671, 0.01529, 0.1406 --> 0.00105, 4.82523 <!-- 0.25520, 0.01978, 0.1590 --> 0.00161, 5.33086 <!-- 0.39301, 0.02185, 0.1861 --> 0.00182, 5.62586 <!-- 0.44281, 0.02306, 0.1952 --> 0.00223, 5.62573 <!-- 0.54402, 0.02306, 0.2132 --> 0.00243, 5.41491 <!-- 0.59332, 0.02220, 0.2221 --> 0.00326, 3.62315 <!-- 0.79401, 0.01485, 0.2665 --> 0.00368, 2.94850 <!-- 0.89672, 0.01209, 0.2978 --> 0.00423, 2.52664 <!-- 1.03182, 0.01036, 0.3471 --> 0.00495, 2.33645 <!-- 1.20665, 0.00958, 0.4190 --> 0.00587, 2.23037 <!-- 1.43252, 0.00914, 0.5180 --> 0.00755, 2.20800 <!-- 1.84174, 0.00905, 0.7024 --> 0.01617, 2.15909 <!-- 3.94340, 0.00885, 1.6649 --> 0.02565, 2.10932 <!-- 6.25675, 0.00865, 2.7488 --> 0.02616, 2.10891 <!-- 6.38007, 0.00865, 2.8073 --> 0.02646, 2.06651 <!-- 6.45517, 0.00847, 2.8432 --> 0.02675, 0.78053 <!-- 6.52501, 0.00320, 2.8923 --> 0.02678, 0.16921 <!-- 6.53346, 0.00069, 2.9101 --> 0.02679, 0.00051 <!-- 6.53460, 0.00000, 2.9235 --> 0.02679, 0.00000 <!-- 6.53460, 0.00000, 2.9300 --> </tableData> </thrust_table> </rocket_engine>