Jon Berndt/Aeromatic 2004-01-01 $Revision: 1.9 $ XB-70 bomber flight model approximation 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.). 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. 6298 105 78.5 415.6 0 468 0 942.8 0 0 160 -32 80 0 0 0 1.34e+06 1.6e+07 1.68e+07 590000 300000 1593 0 -57.9 301.1 0 -277.9 0.8 0.5 0.02 150000 50000 5 NONE 1 1700 -113.4 -277.9 0.8 0.5 0.02 500000 100000 0.0 LEFT 1 1700 113.4 -277.9 0.8 0.5 0.02 500000 100000 0.0 RIGHT 1 1273.8 -210 -40 0.0 0 0 0 1273.8 -210 -40 0.0 0.0 0.0 1273.8 -210 -40 0.0 0 0 1 1273.8 -210 -40 0.0 0.0 0.0 1273.8 -210 -40 0.0 0 0 2 1273.8 -210 -40 0.0 0.0 0.0 1273.8 210 -40 0.0 0 0 3 1273.8 210 -40 0.0 0.0 0.0 1273.8 210 -40 0.0 0 0 4 1273.8 210 -40 0.0 0.0 0.0 1273.8 210 -40 0.0 0 0 5 1273.8 210 -40 0.0 0.0 0.0 1273.8 0 -57.9 4464.3 2232.1 1273.8 0 -57.9 4464.3 2232.1 1273.8 0 -57.9 4464.3 2232.1 1273.8 0 -57.9 4464.3 2232.1 1273.8 0 -57.9 4464.3 2232.1 1273.8 0 -57.9 4464.3 2232.1 1273.8 0 -57.9 4464.3 2232.1 fcs/elevator-cmd-norm fcs/pitch-trim-cmd-norm -1 1 fcs/pitch-trim-sum -0.35 0.3 fcs/elevator-pos-rad 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/rudder-cmd-norm fcs/yaw-trim-cmd-norm -1 1 velocities/r-aero-rad_sec aero/qbar-psf 3.0000 0.0000 11.0000 2.0000
aero/beta-rad aero/qbar-psf 3.0000 0.0000 11.0000 0.0000
fcs/yaw-damper-beta fcs/yaw-damper-rate -0.2000 0.2000 fcs/yaw-damper-sum aero/qbar-psf 2.9900 0.0000 3.0000 1.0000
fcs/rudder-command-sum fcs/yaw-damper-final -1.0000 1.0000 fcs/rudder-sum -0.3500 0.3500 fcs/rudder-pos-rad fcs/flap-cmd-norm 0.0000 15.0000 30.0000 fcs/flap-pos-deg fcs/flap-pos-deg 0 30 0 1 fcs/flap-pos-norm gear/gear-cmd-norm 0.0000 1.0000 gear/gear-pos-norm fcs/speedbrake-cmd-norm 0.0000 1.0000 fcs/speedbrake-pos-norm Drag_at_zero_lift aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -1.5700 1.5000 -0.2600 0.0340 0.0000 0.0170 0.2600 0.0340 1.5700 1.5000
Induced_drag aero/qbar-psf metrics/Sw-sqft aero/cl-squared 0.0420 Drag_due_to_mach aero/qbar-psf metrics/Sw-sqft velocities/mach 0.0000 0.0000 0.7900 0.0000 1.1000 0.0230 1.8000 0.0150
Drag_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-norm 0.0550 Drag_due_to_gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.0110 Drag_due_to_speedbrakes aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.0170 Drag_due_to_sideslip aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.5700 1.2300 -0.2600 0.0500 0.0000 0.0000 0.2600 0.0500 1.5700 1.2300
Drag_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-norm 0.0550 Side_force_due_to_beta aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.0000 Lift_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -0.2000 -0.6800 0.0000 0.2000 0.2300 1.2000 0.6000 0.6000
Delta_Lift_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-norm 1.5000 Delta_Lift_due_to_speedbrake aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm -0.0800 Lift_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-rad 0.2000 Roll_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad -0.1000 Roll_moment_due_to_roll_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-aero-rad_sec -0.4000 Roll_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec 0.1500 Roll_moment_due_to_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad velocities/mach 0.0000 0.1000 2.0000 0.0330
Roll_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad 0.0100 Pitch_moment_due_to_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-rad -0.7000 Pitch_moment_due_to_elevator aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-rad velocities/mach 0.0000 -1.3000 2.0000 -0.3250
Pitch_moment_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -21.0000 Pitch_moment_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -4.0000 Yaw_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad 0.1200 Yaw_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec -0.1500 Yaw_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.1000 Adverse_yaw aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad 0.0000