Jon Berndt 2001-01-01 $Revision: 1.2 $ Space Shuttle GPL (General Public License) http://www.gnu.org/licenses/gpl.html 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. 2690 78 39.6 0 0 0 0 1074 0 373 498 -22 469 0 0 0 953159 7.46508e+06 7.74758e+06 140307 231300 1080 0 373 375 0 225 0.5 0.02 0.02 150000 10000 15 NONE 0 1172 -136 171 0.5 0.02 0.02 150000 10000 0.0 LEFT 0 1172 136 171 0.5 0.02 0.02 150000 10000 0.0 RIGHT 0 fcs/elevator-cmd-norm fcs/pitch-trim-cmd-norm -1 1 fcs/pitch-trim-sum -50 50 fcs/pitch-command-scale -0.36 fcs/pitch-gain-1 0.017 fcs/elevator-pos-rad -0.68 -26.548 -0.595 -20.513 -0.51 -15.328 -0.425 -10.993 -0.34 -7.508 -0.255 -4.873 -0.17 -3.088 -0.085 -2.153 0 -2.068 0.085 -2.833 0.102 -3.088 0.119 -3.377 0.136 -3.7 0.153 -4.057 0.17 -4.448 0.187 -4.873 0.272 -7.508 0.357 -10.993 0.442 -15.328 0.527 -20.513 0.612 -26.548 0.697 -33.433 velocities/q-rad_sec 0.75 fcs/pitch-scheduled-gain-1 fcs/pitch-sas-feedback -0.26 0.61 fcs/elevator-positioning 600

fcs/elevator-pos-rad

fcs/aileron-cmd-norm -20 20 fcs/roll-command-scale 0.42 fcs/roll-gain-1 0.027 velocities/r-rad_sec -0.9 velocities/p-rad_sec fcs/yaw-roll-crossover-gain fcs/yaw-coupled-aileron-feedback-sum -0.5 fcs/roll-gain-2 fcs/roll-sas-gain -0.35 0.35

fcs/left-aileron-pos-rad

fcs/rudder-cmd-norm -250 250 fcs/yaw-command-scale 0.082 fcs/yaw-gain-1 0.04 velocities/r-rad_sec 0.3 fcs/yaw-gain-2 fcs/yaw-sas-gain -0.52 0.52

fcs/rudder-pos-rad

Drag_minimum aero/qbar-psf metrics/Sw-sqft 0.061 Drag_induced aero/qbar-psf metrics/Sw-sqft aero/cl-squared velocities/mach 0.0000 0.2000 0.5000 0.2000 1.0000 0.2300 1.5000 0.4000 2.0000 0.5000 3.0000 0.8000 4.0000 0.9300 5.0000 1.0500 6.0000 1.1500 9.0000 1.3300 Side_force_due_to_beta aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.4000 Side_force_due_to_aileron aero/qbar-psf metrics/Sw-sqft fcs/left-aileron-pos-rad -0.0500 Side_force_due_to_rudder aero/qbar-psf metrics/Sw-sqft fcs/rudder-pos-rad 0.4500 Lift_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/alpha-rad 6.0000 Lift_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-rad velocities/mach 0.0000 1.0000 0.6000 1.0500 1.0000 1.1500 1.2000 1.0000 1.6000 0.6600 2.0000 0.5000 2.4000 0.4000 3.0000 0.3100 5.6000 0.2100 6.0000 0.2000 9.0000 0.2000 Roll_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad -0.0100 Roll_moment_due_to_roll_rate_(roll_damping) aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-rad_sec -0.3500 Roll_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-rad_sec 0.0400 Roll_moment_due_to_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad velocities/machposition/h-sl-ft 0.0000 80000.0000 0.0000 0.0500 0.0500 0.4000 0.0700 0.0500 0.6000 0.0800 0.0500 1.0000 0.1100 0.0500 1.4000 0.0800 0.0600 1.6000 0.0700 0.0600 2.4000 0.0600 0.0500 6.0000 0.0300 0.0200 Roll_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad 0.0120 Pitch_moment_due_to_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-rad -1.2000 Pitch_moment_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-rad_sec -6.2000 Pitch_moment_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec 0.0000 Pitch_moment_due_to_Mach aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft velocities/mach velocities/machposition/h-sl-ft 0.0000 40000.0000 60000.0000 80000.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.6000 0.0000 -0.0100 -0.0100 0.0000 0.8000 0.0000 -0.1300 -0.1300 0.0000 1.0000 0.0000 -0.1100 -0.1800 0.0000 1.1000 0.0000 -0.1600 -0.1800 0.0000 1.2000 0.0000 -0.2500 -0.1700 0.0000 1.4000 0.0000 -0.0600 -0.1500 0.0000 1.7000 0.0000 -0.0300 -0.0300 0.0000 2.0000 0.0000 -0.0100 -0.0100 0.0000 9.0000 0.0000 0.0000 0.0000 0.0000 Pitch_moment_due_to_elevator_deflection aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-rad velocities/mach 0.0000 -0.5200 0.2500 -0.5200 2.0000 -0.1900 8.0000 -0.0370 Yaw_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad 0.5000 Yaw_moment_due_to_roll_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-rad_sec 0.0000 Yaw_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-rad_sec -1.5000 Yaw_moment_due_to_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/left-aileron-pos-rad 0.0400 Yaw_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.3000