Unknown 2004-01-01 $Id: C130.xml,v 1.12 2012/12/22 15:22:18 jberndt Exp $ Models a Lockheed C-130 Hercules. 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. 3070.18 132.5 23.17 491.23 48.88 552.63 0 586.5 0 0 93.8 -24 65 0 0 0 3.66391e+06 2.38552e+06 5.9669e+06 -0 -0 -0 105000 586.5 0 -29.3 152.5 0 -140.8 0.8 0.5 0.02 52500 17500 30 NONE 1 610 -174.9 -140.8 0.8 0.5 0.02 175000 35000 0.0 LEFT 1 610 174.9 -140.8 0.8 0.5 0.02 175000 35000 0.0 RIGHT 1 586.5 -265 -40 0.0 0 0 0 586.5 -265 -40 0.0 0.0 0.0 586.5 -265 -40 0.0 0 0 1 586.5 -265 -40 0.0 0.0 0.0 586.5 265 -40 0.0 0 0 2 586.5 265 -40 0.0 0.0 0.0 586.5 265 -40 0.0 0 0 3 586.5 265 -40 0.0 0.0 0.0 586.5 0 -29.325 1944.4 972.2 586.5 0 -29.325 1944.4 972.2 586.5 0 -29.325 1944.4 972.2 586.5 0 -29.325 1944.4 972.2 586.5 0 -29.325 1944.4 972.2 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 fcs/rudder-command-sum -0.35 0.35 fcs/rudder-pos-rad fcs/flap-cmd-norm 0 15 30 fcs/flap-pos-deg fcs/flap-pos-deg 0 30 0 1 fcs/flap-pos-norm gear/gear-cmd-norm 0 1 gear/gear-pos-norm fcs/speedbrake-cmd-norm 0 1 fcs/speedbrake-pos-norm Drag_at_zero_lift aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -1.5700 1.5000 -0.2600 0.0500 0.0000 0.0250 0.2600 0.0500 1.5700 1.5000
Induced_drag aero/qbar-psf metrics/Sw-sqft aero/cl-squared 0.0390 Drag_due_to_mach aero/qbar-psf metrics/Sw-sqft velocities/mach 0.0000 0.0000 0.7000 0.0000 1.1000 0.0230 1.8000 0.0150
Drag_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.001167 Drag_due_to_gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.0230 Drag_due_to_speedbrakes aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.0250 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 0.0350 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 -0.7400 0.0000 0.2400 0.2400 1.4000 0.6000 0.7040
Delta_Lift_due_to_flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.02 Delta_Lift_due_to_speedbrake aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.0000 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 0.1500 2.0000 0.0500
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 -0.4000 Pitch_moment_due_to_elevator aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-rad velocities/mach 0.0000 -1.0000 2.0000 -0.2500
Pitch_moment_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -22.0000 Pitch_moment_due_to_alpha_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -8.0000 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 -0.0080