xcvb specter (some table data from first non working version) yurik_nsk (many ideas from Tu-154) 2015-06-22 1.0 Tu-134a airliner 127.3 29 4.319 0.01745 30.68 14.90 21.25 13.20 20 0 0 3 -1 0 18.5 0.0 2.0 574000 3500000 3840000 0 200000 0 28000 20 0 0.5 I need some ballast in the front 2000 3 0 0 9000 14 0 0 4.0 0.0 -2.45 0.6 0.8 0.02 800000 150000 15 NONE 1 19.5 -4.8 -2.4 0.6 0.5 0.02 1.7e+06 100000 0 LEFT 1 19.5 4.8 -2.4 0.6 0.5 0.02 1.7e+06 100000 0 RIGHT 1 2.0 0.0 -0.9 0.8 0.5 0 3e+06 630720 0 NONE 0 25.7 -14.5 -0.9 0.8 0.5 0 5896.17 1179.23 0 NONE 0 25.7 14.5 -0.9 0.8 0.5 0 5896.17 1179.23 0 NONE 0 32.0 0.0 -1.5 0.8 0.5 0 3e+06 630720 0 NONE 0 26.0 2.2 1.2 0.0 0.0 0.0 0 1 2 3 4 5 6 29.25 2.1 1.25 0.0 2.0 4.0 26.0 -2.2 1.2 0.0 0.0 0.0 0 1 2 3 4 5 6 29.25 -2.1 1.25 0.0 2.0 -4.0 23.5 -11.5 -0.3 1 1644 0 21.4 -8.0 -0.3 1 7000 3500 18.5 -3.0 -0.4 1 3130 3130 18.5 0.0 -0.5 1 2142 2142 18.5 3.0 -0.4 1 3130 3130 21.4 8.0 -0.3 1 7000 3500 23.5 11.5 -0.3 1 1644 0 fcs/elevator-cmd-norm fcs/pitch-trim-cmd-norm -1 1 fcs/pitch-trim-sum -0.506 0.28 fcs/elevator-pos-rad fcs/elevator-pos-rad -1 1 -1 1 fcs/elevator-pos-norm fcs/aileron-cmd-norm fcs/roll-trim-cmd-norm -1 1 fcs/roll-trim-sum -0.35 0.35 fcs/left-aileron-pos-rad fcs/roll-trim-sum -0.35 0.35 fcs/right-aileron-pos-rad fcs/left-aileron-pos-rad -0.35 0.35 -1 1 fcs/left-aileron-pos-norm fcs/right-aileron-pos-rad -0.35 0.35 -1 1 fcs/right-aileron-pos-norm fcs/yaw-damper-enable fcs/rudder-cmd-norm fcs/yaw-trim-cmd-norm -1 1 velocities/r-aero-rad_sec velocities/ve-kts 30 0.00 60 2.00
fcs/yaw-damper-enable fcs/rudder-command-sum fcs/yaw-damper-rate -1.1 1.1 fcs/rudder-sum -1.1 1.1 -0.35 0.35 fcs/rudder-pos-rad fcs/rudder-pos-rad -0.35 0.35 -1 1 fcs/rudder-pos-norm fcs/flap-cmd-norm 0 10 15 20 25 30 38 fcs/flap-pos-deg fcs/flap-pos-deg 0 38 0 1 fcs/flap-pos-norm gear/gear-cmd-norm 0 1 gear/gear-pos-norm fcs/spoiler-cmd-norm 0 1 fcs/speedbrake-pos-norm Mach and flaps parameter fcs/flap-pos-deg velocities/mach -1 Lift due to alpha aero/alpha-wing-radaero/function/cmf -0.82 -0.80 -0.75 -0.70 -0.60 0 20 30 38 -0.070 -0.50 -0.55 -0.60 -0.70 -0.80 -0.40 0.00 0.10 0.20 0.000 -0.05 -0.05 -0.05 -0.10 -0.15 -0.07 0.37 0.55 0.67 0.087 0.46 0.47 0.48 0.46 0.45 0.39 0.81 1.01 1.13 0.175 0.75 0.76 0.82 0.89 0.93 0.84 1.24 1.43 1.55 0.209 0.79 0.82 0.87 0.96 1.05 1.00 1.35 1.55 1.70 0.262 0.81 0.88 0.94 1.03 1.13 1.23 1.62 1.81 1.93 0.279 0.82 0.90 0.96 1.05 1.15 1.30 1.70 1.88 2.00 0.297 0.83 0.92 0.99 1.08 1.16 1.35 1.73 1.90 2.05
Lift_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/function/cy 1.1 Delta_Lift_due_to_speedbrake aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm -0.65 Lift_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-rad 0.2 Delta_Lift_due_to_gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm -0.06 Lift near ground position/h-agl-ft 0 0.3 10 0.25 27 0
aero/qbar-psf metrics/Sw-sqft Drag_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/alpha-wing-radaero/function/cmf -0.82 -0.6 -0.2 20 38 -0.0698 0.023 0.035 0.03 0.05 0.13 0.0 0.023 0.025 0.02 0.05 0.14 0.0349 0.023 0.025 0.02 0.05 0.15 0.0698 0.03 0.025 0.02 0.06 0.17 0.1047 0.035 0.035 0.03 0.08 0.19 0.1396 0.053 0.045 0.04 0.1 0.22 0.1745 0.07 0.055 0.05 0.13 0.25 0.2094 0.09 0.065 0.06 0.16 0.28 0.2443 0.12 0.098 0.09 0.19 0.31 0.2793 0.16 0.13 0.12 0.23 0.34 0.3142 0.22 0.19 0.18 0.29 0.38 0.3491 0.3 0.25 0.24 0.35 0.45
1.0 Drag_due_to_gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm velocities/mach 0.0 0.012 0.1 0.012 0.2 0.012 0.3 0.012 0.4 0.013 0.5 0.015 0.6 0.017 0.7 0.022 0.8 0.031 0.9 0.065
Drag_due_to_speedbrakes aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.019 Drag_due_to_sideslip aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.57 1.23 -0.26 0.05 0 0 0.26 0.05 1.57 1.23
Drag_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-norm 0.01 Drag near ground position/h-agl-ft 0 -0.01 10 -0.008 27 0
aero/qbar-psf metrics/Sw-sqft Side_force_due_to_beta aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.0000 Roll_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad aero/alpha-wing-radfcs/flap-pos-deg 0 20 38 0 -0.00135 -0.004 -0.0034 0.08727 -0.0017 -0.0043 -0.00375 0.17453 -0.0019 -0.0046 -0.004 0.2678 -0.0025 -0.0047 -0.0048 0.3678 -0.0048 -0.0048 -0.0048
Roll_moment_due_to_roll_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-aero-rad_sec -0.5 Roll_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec 0.15 Roll_moment_due_to_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad velocities/mach 0.15 0.0659 0.5 0.0595 1 0.03438
1.4 Roll_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad -0.0156 Pitch moment due to alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-wing-radfcs/flap-pos-deg 0 20 38 -0.07 0.6 0.55 0.5 0 0.3 0.25 0.19 0.09 0 0 -0.2 0.21 -0.4 -0.3 -0.42 0.26 -0.51 -0.4 -0.39 0.31 -0.51 -0.44 -0.4 0.35 -0.5 -0.38 -0.41 0.38 -0.08 -0.08 -0.18
Pitch moment due to elevator aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-rad velocities/mach 0.3000 -1.5000 1.0000 -0.5000
Pitch moment due to pitch rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -17 Pitch moment due to alpha rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -4 Yaw moment due to beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad 0.12 Yaw moment due to yaw rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec -0.15 Yaw moment due to rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.1 Adverse yaw aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad 0 -160 0 -96 1 0 0