Petar Jedvaj 2016-06-29 $Revision: 1.15 $ General Atomics MQ-9 Reaper. 257.28 65.62 2.00 3.92 32.29 21.65 10.76 21.65 173.24 0.00 0.00 121.27 0.00 40.00 0 0 0 11946 6424 17362 4902 173.24 0.00 -10.83 4314 LBS + full (1280 LBS) fuel should bring model up to entered max weight 2156.8 173.24 0.00 -10.83 100 173 -89 -3 100 173 -74 -3 510 173 -48 -3 510 173 48 -3 100 173 74 -3 100 173 89 -3 56.30 0.00 -51.97 0.80 0.50 0.02 3148.74 5247.90 5.00 NONE 1 180.17 -118.12 -51.97 0.80 0.50 0.02 10495.80 5247.90 0 LEFT 1 180.17 118.12 -51.97 0.80 0.50 0.02 10495.80 5247.90 0 RIGHT 1 173.24 -32.81 -10.83 1.00 1.00 10495.80 10495.80 173.24 32.81 -10.83 1.00 1.00 10495.80 10495.80 373.09 0.00 0.00 0.00 0.00 0.00 0 373.09 0.00 0.00 0.00 0.00 0.00 173.24 0.00 -10.83 2000.00 1000.00 173.24 0.00 -10.83 2000.00 1000.00 fcs/elevator-cmd-norm fcs/pitch-trim-cmd-norm -1 1 fcs/pitch-trim-sum -0.35 0.35

fcs/elevator-pos-rad

fcs/elevator-pos-rad -0.35 0.35 -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 0 15 4 30 3

fcs/flap-pos-deg

fcs/flap-pos-deg 0 30 0 1

fcs/flap-pos-norm

gear/gear-cmd-norm 0 0 1 5

gear/gear-pos-norm

fcs/speedbrake-cmd-norm 0 0 1 1

fcs/speedbrake-pos-norm

Lift due to alpha aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -0.20 -0.730 0.00 0.170 0.23 1.200 0.60 0.582 Delta Lift due to flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.01000 Delta Lift due to speedbrake aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0 Lift due to Elevator Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-rad 0.2 Drag at zero lift aero/qbar-psf metrics/Sw-sqft aero/alpha-rad -1.57 1.500 -0.26 0.026 0.00 0.020 0.26 0.026 1.57 1.500 Induced drag aero/qbar-psf metrics/Sw-sqft aero/cl-squared 0.06 Drag due to mach aero/qbar-psf metrics/Sw-sqft velocities/mach 0.00 0.000 0.75 0.000 1.10 0.023 1.80 0.015 Drag due to flaps aero/qbar-psf metrics/Sw-sqft fcs/flap-pos-deg 0.00133 Drag due to gear aero/qbar-psf metrics/Sw-sqft gear/gear-pos-norm 0.03 Drag due to speedbrakes aero/qbar-psf metrics/Sw-sqft fcs/speedbrake-pos-norm 0.02 Drag due to sideslip aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1.57 1.230 -0.26 0.050 0.00 0.000 0.26 0.050 1.57 1.230 Drag due to Elevator Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-norm 0.04 Side force due to beta aero/qbar-psf metrics/Sw-sqft aero/beta-rad -1 Roll moment due to beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad -0.1 Roll moment due to roll rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-aero-rad_sec -0.4 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 0.18 Roll moment due to rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad 0.01 Pitch moment due to alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-rad -0.5 Pitch moment due to elevator aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-rad velocities/mach 0.0 -1.000 2.0 -0.250 Pitch moment due to pitch rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -15 Pitch moment due to alpha rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -7 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 -0.003