66 lines
1.8 KiB
Text
66 lines
1.8 KiB
Text
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# Jeff Scott
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# North American X-15
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# rocket-powered high-speed research aircraft, data from:
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# Flight Gear JSBsim X15.cfg file
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# Jon Brendt's X-15 web site
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# http://www.hal-pc.org/~jsb/X-15.html
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# 03-28-2000 file creation
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init Dz_cg 5.0 # [ft]
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geometry bw 22.36 # [ft]
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geometry cbar 10.27 # [ft]
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geometry Sw 200.0 # [ft^2]
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controlSurface de 35 15 # [deg]
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controlSurface da 15 15 # [deg]
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controlSurface dr 20 20 # [deg] guess for now
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mass Weight 31240 # [lb]
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mass I_xx 3650 # [slug-ft^2]
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mass I_yy 80000 # [slug-ft^2]
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mass I_zz 82000 # [slug-ft^2]
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mass I_xz 590 # [slug-ft^2]
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# aircraft specs: 51090 lb at sea level
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# 57000 lb at 45,000 ft
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# 70000 lb at peak altitude
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engine simpleSingle 51090 # [lb]
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#CL CLo <CLo> # []
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CL CL_a 3.5 # [/rad]
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#CL CL_adot <CL_adot> # [/rad]
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#CL CL_q <CL_q> # [/rad]
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CL CL_de 0.54 # [/rad]
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CD CDo 0.095 # []
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#CD CDK # []
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CD CD_a 0.6 # [/rad]
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#CD CD_de <CD_de> # [/rad]
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#Cm Cmo <Cmo> # []
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Cm Cm_a -1.2 # [/rad]
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Cm Cm_adot 0.0 # [/rad]
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Cm Cm_q -6.2 # [/rad]
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Cm Cm_de -0.9 # [/rad]
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CY CY_beta -1.4 # [/rad]
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#CY CY_p <CY_p> # [/rad]
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#CY CY_r <CY_r> # [/rad]
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CY CY_da 0.05 # [/rad] sign reversed
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CY CY_dr 0.45 # [/rad]
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Cl Cl_beta -0.01 # [/rad]
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Cl Cl_p -0.35 # [/rad]
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Cl Cl_r 0.04 # [/rad]
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Cl Cl_da -0.06 # [/rad] sign reversed
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Cl Cl_dr 0.012 # [/rad]
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Cn Cn_beta 0.5 # [/rad]
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Cn Cn_p 0.0 # [/rad]
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Cn Cn_r -1.5 # [/rad]
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Cn Cn_da -0.04 # [/rad] sign reversed
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Cn Cn_dr -0.3 # [/rad]
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