jsbsim.js
Version:
JSBSim flight dynamics model ported to JavaScript
332 lines (320 loc) • 19.8 kB
text/xml
<fdm_config name="MK-82" version="2.0" release="BETA"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sourceforge.net/JSBSim.xsd">
<fileheader>
<author> Unknown </author>
<filecreationdate> 2001-01-01 </filecreationdate>
<version> $Revision: 1.12 $ </version>
<description> Mk-82 </description>
<note>
This model was created using publicly available data, publicly available
technical reports, textbooks, and guesses. It contains no proprietary or
restricted data. If this model has been validated at all, it would be
only to the extent that it seems to "fly right", and that it possibly
complies with published, publicly known, performance data (maximum speed,
endurance, etc.). Or, it could be a gross approximation, with the only
similarity to an actual object being the name. Thus, this model is meant
for educational and entertainment purposes only.
This simulation model is not endorsed by the manufacturer. This model is not
to be sold.
</note>
</fileheader>
<metrics>
<wingarea unit="FT2"> 2.54 </wingarea>
<wingspan unit="FT"> 0.9 </wingspan>
<chord unit="FT"> 0.9 </chord>
<htailarea unit="FT2"> 0 </htailarea>
<htailarm unit="FT"> 0 </htailarm>
<vtailarea unit="FT2"> 0 </vtailarea>
<vtailarm unit="FT"> 0 </vtailarm>
<location name="AERORP" unit="IN">
<x> 33.08 </x>
<y> 0 </y>
<z> 0 </z>
</location>
<location name="EYEPOINT" unit="IN">
<x> 0 </x>
<y> 0 </y>
<z> 0 </z>
</location>
<location name="VRP" unit="IN">
<x> 31 </x>
<y> 0 </y>
<z> 0 </z>
</location>
</metrics>
<mass_balance>
<ixx unit="SLUG*FT2"> 0.66 </ixx>
<iyy unit="SLUG*FT2"> 633 </iyy>
<izz unit="SLUG*FT2"> 633 </izz>
<emptywt unit="LBS"> 500 </emptywt>
<location name="CG" unit="IN">
<x> 31 </x>
<y> 0 </y>
<z> 0 </z>
</location>
</mass_balance>
<ground_reactions>
<contact type="BOGEY" name="NOSE_CONTACT">
<location unit="IN">
<x> 0 </x>
<y> 0 </y>
<z> 0 </z>
</location>
<static_friction> 0 </static_friction>
<dynamic_friction> 0 </dynamic_friction>
<rolling_friction> 0 </rolling_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 200000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
<contact type="BOGEY" name="TAIL_CONTACT">
<location unit="IN">
<x> 66 </x>
<y> 0 </y>
<z> 0 </z>
</location>
<static_friction> 0 </static_friction>
<dynamic_friction> 0 </dynamic_friction>
<rolling_friction> 0 </rolling_friction>
<spring_coeff unit="LBS/FT"> 10000 </spring_coeff>
<damping_coeff unit="LBS/FT/SEC"> 200000 </damping_coeff>
<max_steer unit="DEG"> 0.0 </max_steer>
<brake_group> NONE </brake_group>
<retractable>0</retractable>
</contact>
</ground_reactions>
<propulsion>
</propulsion>
<flight_control name="FCS: MK-82 FCS">
</flight_control>
<aerodynamics>
<axis name="DRAG">
<function name="aero/coefficient/CDmin">
<description>Drag_minimum</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<table>
<independentVar>velocities/mach</independentVar>
<tableData>
0.2000 0.1400
0.4000 0.1390
0.8000 0.1440
0.9000 0.1490
0.9500 0.2110
0.9800 0.2520
1.0000 0.2810
1.0200 0.3050
1.0500 0.3270
1.1000 0.3590
1.2000 0.3730
1.4000 0.4180
1.6000 0.2750
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/CDi">
<description>Drag_induced</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/cl-squared</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">velocities/mach</independentVar>
<tableData>
0.2000 0.4000 0.8000 0.9000 0.9500 0.9800 1.0000 1.0200 1.0500 1.1000 1.2000 1.4000 1.6000
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
0.1750 0.1560 0.1500 0.1070 0.1050 0.1030 0.1020 0.1020 0.1010 0.0990 0.0980 0.1110 0.1600 0.1190
0.3490 0.6730 0.5730 0.4500 0.4510 0.4440 0.4430 0.4450 0.4430 0.4450 0.4470 0.6230 0.8560 0.7290
0.5240 1.4760 1.3320 1.1990 1.4870 1.5370 1.6100 1.6740 1.7090 1.7460 1.7740 1.9140 2.3430 1.9960
0.6980 2.1210 2.0970 2.8570 2.9140 2.9880 3.1060 3.2080 3.2780 3.3460 3.3770 3.5290 4.2260 3.5760
0.8730 2.5020 2.7550 4.5630 4.5610 4.6780 4.9210 5.1210 5.2740 5.4180 5.4270 5.5120 6.2080 5.3600
1.0470 2.9490 3.3400 6.2000 6.2250 6.3620 6.6550 6.8950 7.0660 7.2180 7.2770 7.4390 8.0250 7.1240
1.2220 3.2720 4.0200 7.6130 7.5170 7.6200 8.0050 8.3230 8.5590 8.7720 8.8950 9.0890 9.4860 8.6470
1.3960 3.4140 4.4490 8.5890 8.3450 8.5060 8.9530 9.3140 9.5900 9.8810 10.0510 10.1820 10.4330 9.7400
1.5530 3.3830 4.5250 8.9570 8.6620 8.8520 9.3210 9.6990 10.0120 10.3210 10.5040 10.5930 10.7020 10.1650
</tableData>
</table>
</product>
</function>
</axis>
<axis name="SIDE">
<function name="aero/coefficient/CYb">
<description>Side_force_due_to_beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/beta-rad</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">velocities/mach</independentVar>
<tableData>
0.2000 0.4000 0.8000 0.9000 0.9500 0.9800 1.0000 1.0200 1.0500 1.1000 1.2000 1.4000 1.6000
0.0000 -4.5720 -4.7780 -2.8390 -2.7830 -2.7820 -2.7820 -2.8020 -2.7880 -2.7260 -2.6240 -2.1270 -3.7510 -1.8680
0.1750 -3.4650 -3.4620 -2.5390 -2.5700 -2.5920 -2.6220 -2.6620 -2.6740 -2.6870 -2.6990 -3.2400 -5.0870 -3.5300
0.3490 -4.0330 -3.1760 -2.3060 -2.4370 -2.4890 -2.5570 -2.6210 -2.6490 -2.7270 -2.8330 -4.4100 -6.4600 -5.2600
0.5240 -3.7880 -3.2320 -2.9470 -4.1930 -4.5100 -4.8660 -5.1520 -5.3400 -5.5510 -5.7630 -6.4010 -7.7820 -6.4780
0.6980 -3.1380 -3.0860 -4.9400 -5.1690 -5.4310 -5.7500 -6.0080 -6.2040 -6.4040 -6.5570 -6.9630 -7.8090 -6.5080
0.8730 -2.9750 -3.2000 -5.2580 -5.3000 -5.5000 -5.8190 -6.0770 -6.2740 -6.4640 -6.5150 -6.6640 -7.2910 -6.2470
1.0470 -2.7910 -3.0190 -4.9470 -4.9880 -5.1250 -5.3530 -5.5420 -5.6700 -5.7860 -5.8440 -6.0050 -6.4240 -5.6280
1.2220 -2.5860 -2.8680 -4.3030 -4.2850 -4.3540 -4.5250 -4.6730 -4.7700 -4.8570 -4.9100 -5.0550 -5.3130 -4.7050
1.3960 -2.3880 -2.5850 -3.4120 -3.3890 -3.4360 -3.5320 -3.6200 -3.6690 -3.7200 -3.7470 -3.8640 -4.0610 -3.5780
1.5530 -2.2370 -2.2840 -2.4930 -2.5160 -2.5300 -2.5510 -2.5830 -2.5840 -2.5840 -2.5790 -2.7030 -2.9020 -2.4700
</tableData>
</table>
</product>
</function>
</axis>
<axis name="LIFT">
<function name="aero/coefficient/CLwbh">
<description>Lift_due_to_alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>aero/alpha-rad</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">velocities/mach</independentVar>
<tableData>
0.2000 0.4000 0.8000 0.9000 0.9500 0.9800 1.0000 1.0200 1.0500 1.1000 1.2000 1.4000 1.6000
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
0.1750 0.8920 0.8530 0.6050 0.5960 0.5830 0.5770 0.5780 0.5720 0.5640 0.5510 0.6290 0.0000 0.0000
0.3490 1.8910 1.5980 1.2390 1.2460 1.2240 1.2220 1.2310 1.2240 1.2300 1.2340 1.7500 0.9180 0.6530
0.5240 2.6800 2.3890 2.1310 2.7150 2.8200 2.9670 3.0950 3.1670 3.2450 3.3060 3.5860 2.3710 1.9530
0.6980 2.7130 2.6710 3.8650 3.9660 4.0880 4.2740 4.4320 4.5460 4.6580 4.7190 4.9500 4.0820 3.3810
0.8730 2.2200 2.4250 4.1130 4.1320 4.2580 4.4950 4.6880 4.8340 4.9760 5.0020 5.1060 5.0580 4.1590
1.0470 1.7770 1.9990 3.7420 3.7690 3.8700 4.0620 4.2180 4.3260 4.4280 4.4760 4.5890 5.2690 4.4650
1.2220 1.2300 1.5000 2.8490 2.8190 2.8740 3.0280 3.1540 3.2430 3.3290 3.3840 3.4650 4.7080 4.1210
1.3960 0.6120 0.7940 1.5350 1.4940 1.5310 1.6170 1.6850 1.7320 1.7870 1.8230 1.8500 3.5210 3.1700
1.5530 0.0470 0.0670 0.1450 0.1400 0.1440 0.1520 0.1590 0.1600 0.1650 0.1690 0.1720 1.8770 1.7320
</tableData>
</table>
</product>
</function>
</axis>
<axis name="ROLL">
<function name="aero/coefficient/Clbeta">
<description>Roll_moment_due_to_beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/beta-rad</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">velocities/mach</independentVar>
<tableData>
0.2000 0.4000 0.8000 0.9000 0.9500 0.9800 1.0000 1.0200 1.0500 1.1000 1.2000 1.4000 1.6000
0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
0.1750 0.1500 0.0890 0.0050 0.0110 0.0140 0.0160 0.0170 0.0170 0.0180 0.0190 0.0210 0.0370 0.0400
0.3490 -0.0550 -0.0550 -0.0370 -0.0290 -0.0270 -0.0240 -0.0220 -0.0200 -0.0160 -0.0100 0.0020 0.0350 0.0420
0.5240 -0.0280 -0.0200 0.0110 0.0160 0.0180 0.0190 0.0200 0.0210 0.0220 0.0180 0.0260 0.0500 0.0740
0.6980 0.2960 0.2760 0.2300 0.2210 0.2130 0.2090 0.2080 0.2040 0.1980 0.1880 0.1790 0.1560 0.1660
0.8730 0.3000 0.2920 0.2750 0.2730 0.2700 0.2690 0.2700 0.2680 0.2660 0.2610 0.2660 0.2690 0.2570
1.0470 0.2960 0.2980 0.3070 0.3110 0.3100 0.3110 0.3130 0.3120 0.3110 0.3080 0.3210 0.3390 0.3230
1.2220 0.3100 0.3120 0.3240 0.3290 0.3290 0.3300 0.3330 0.3320 0.3300 0.3280 0.3430 0.3650 0.3520
1.3960 0.3160 0.3170 0.3300 0.3360 0.3370 0.3380 0.3410 0.3400 0.3390 0.3380 0.3540 0.3780 0.3660
1.5530 0.3120 0.3130 0.3270 0.3320 0.3330 0.3340 0.3380 0.3370 0.3360 0.3340 0.3500 0.3740 0.3630
</tableData>
</table>
</product>
</function>
</axis>
<axis name="PITCH">
<function name="aero/coefficient/Cmalpha">
<description>Pitch_moment_due_to_alpha</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/alpha-rad</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">velocities/mach</independentVar>
<tableData>
0.2000 0.4000 0.8000 0.9000 0.9500 0.9800 1.0000 1.0200 1.0500 1.1000 1.2000 1.4000 1.6000
0.0000 -1.3720 -1.7830 -1.3250 -0.2610 -0.2670 -0.0530 -0.2280 -0.1110 0.3980 -0.0010 -1.6930 -3.6220 9.0240
0.1750 -3.6990 -3.7670 -2.3840 -1.2630 -1.1680 -0.9210 -1.0390 -0.8730 -0.3300 -0.5070 -1.5380 -2.5500 8.7340
0.3490 -6.2840 -6.2120 -4.5940 -3.4430 -3.2580 -2.9880 -3.0420 -2.8720 -2.3760 -2.4010 -3.1630 -3.7190 5.6670
0.5240 -6.6830 -6.6450 -5.4900 -4.8850 -4.7620 -4.5880 -4.6300 -4.5470 -4.2660 -4.3030 -5.0530 -5.7670 0.4580
0.6980 -1.3220 -1.7460 -2.7300 -3.1210 -3.2820 -3.3450 -3.4360 -3.5030 -3.5630 -3.7900 -4.5880 -6.0190 -3.9490
0.8730 0.4270 -0.0950 -2.1340 -2.9000 -3.1370 -3.3200 -3.3910 -3.5370 -3.8170 -3.9870 -4.4190 -5.6210 -7.8500
1.0470 -3.0160 -3.0290 -4.1670 -4.9730 -5.0950 -5.2690 -5.2630 -5.4040 -5.7450 -5.6550 -5.4110 -5.5440 -11.3800
1.2220 -4.2180 -4.1060 -5.2920 -6.2680 -6.3560 -6.5490 -6.5100 -6.6640 -7.0630 -6.8850 -6.3960 -6.1490 -14.1200
1.3960 -4.5480 -4.4880 -5.7950 -6.8090 -6.8780 -7.0910 -7.0530 -7.2180 -7.6500 -7.4550 -6.9020 -6.5500 -15.1500
1.5530 -4.5480 -4.5460 -5.8850 -6.8540 -6.9290 -7.1500 -7.1170 -7.2760 -7.7250 -7.5390 -6.9700 -6.6060 -15.1600
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/Cmq">
<description>Pitch_moment_due_to_pitch_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>velocities/q-aero-rad_sec</property>
<value>-50.0000</value>
</product>
</function>
<function name="aero/coefficient/Cmadot">
<description>Pitch_moment_due_to_alpha_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/ci2vel</property>
<property>aero/alphadot-rad_sec</property>
<value>-3.4600</value>
</product>
</function>
</axis>
<axis name="YAW">
<function name="aero/coefficient/Cnbeta">
<description>Yaw_moment_due_to_beta</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/cbarw-ft</property>
<property>aero/beta-rad</property>
<table>
<independentVar lookup="row">aero/alpha-rad</independentVar>
<independentVar lookup="column">velocities/mach</independentVar>
<tableData>
0.2000 0.4000 0.8000 0.9000 0.9500 0.9800 1.0000 1.0200 1.0500 1.1000 1.2000 1.4000 1.6000
0.0000 1.3720 1.7830 1.3250 0.2610 0.2670 0.0530 0.2280 0.1110 -0.3980 0.0010 1.6930 3.6220 -9.0240
0.1750 3.6990 3.7670 2.3840 1.2630 1.1680 0.9210 1.0390 0.8730 0.3300 0.5070 1.5380 2.5500 -8.7340
0.3490 6.2840 6.2120 4.5940 3.4430 3.2580 2.9880 3.0420 2.8720 2.3760 2.4010 3.1630 3.7190 -5.6670
0.5240 6.6830 6.6450 5.4900 4.8850 4.7620 4.5880 4.6300 4.5470 4.2660 4.3030 5.0530 5.7670 -0.4580
0.6980 1.3220 1.7460 2.7300 3.1210 3.2820 3.3450 3.4360 3.5030 3.5630 3.7900 4.5880 6.0190 3.9490
0.8730 -0.4270 0.0950 2.1340 2.9000 3.1370 3.3200 3.3910 3.5370 3.8170 3.9870 4.4190 5.6210 7.8500
1.0470 3.0160 3.0290 4.1670 4.9730 5.0950 5.2690 5.2630 5.4040 5.7450 5.6550 5.4110 5.5440 11.3800
1.2220 4.2180 4.1060 5.2920 6.2680 6.3560 6.5490 6.5100 6.6640 7.0630 6.8850 6.3960 6.1490 14.1200
1.3960 4.5480 4.4880 5.7950 6.8090 6.8780 7.0910 7.0530 7.2180 7.6500 7.4550 6.9020 6.5500 15.1500
1.5530 4.5480 4.5460 5.8850 6.8540 6.9290 7.1500 7.1170 7.2760 7.7250 7.5390 6.9700 6.6060 15.1600
</tableData>
</table>
</product>
</function>
<function name="aero/coefficient/Cnr">
<description>Yaw_moment_due_to_yaw_rate</description>
<product>
<property>aero/qbar-psf</property>
<property>metrics/Sw-sqft</property>
<property>metrics/bw-ft</property>
<property>aero/bi2vel</property>
<property>velocities/r-aero-rad_sec</property>
<value>-60.0000</value>
</product>
</function>
</axis>
</aerodynamics>
</fdm_config>