Unknown 2002-01-01 $Id: c172p.xml,v 1.41 Jan 2018 $ Cessna 172P Skyhawk 174 35.8 4.9 21.9 15.7 16.5 0 40.6 0 59.4 37 0 48 42.6 0 38.5 948 1285 1906 -0 -0 -0 1467 39.06 0 34 180 36 -14 24 0 36 14 24 0 70 -14 24 0 70 14 24 0 95 0 24 0 58.2 -43 -15.5 0 58.2 43 -15.5 0 58.2 -43 -15.5 0 58.2 43 -15.5 0 41 -43 -25 0 41 43 -25 0 41 -43 -25 0 41 43 -25 0 58.2 -43 -15.5 0 58.2 43 -15.5 0 30.29 0 26.6 0 -19.7 0 26.6 The hydrodynamic interactions of the floats are modelled by external forces. -6.8 0 -20.3 0.8 0.5 0.02 3600 1200 30 NONE 0 58.2 -43 -15.3 0.8 0.5 0.02 5400 1800 0.0 LEFT 0 58.2 43 -15.1 0.8 0.5 0.02 5400 1800 0.0 RIGHT 0 226.7 0 17 0.5 0.25 2000 1000 20 -232 50 0.75 0.5 1830.15 366.03 20 232 50 0.75 0.5 1830.15 366.03 -6.8 0 0 0.9 0.5 1830.15 366.03 58.2 -48 0 0.8 0.4 1830.15 366.03 58.2 48 0 0.8 0.4 1830.15 366.03 -119 0 35 .75 .5 1830.15 366.03 -119 0 8 3.0 2.0 1830.15 366.03 -4.7 0 60 3.0 2.0 1830.15 366.03 253.5 0 90 3.0 2.0 1830.15 366.03 3.230 -56.889 38.5 0.5 0.2 1830.15 366.03 3.230 56.889 38.5 0.5 0.2 1830.15 366.03 70.16 -56.889 38.5 0.5 0.2 1830.15 366.03 70.16 56.889 38.5 0.5 0.2 1830.15 366.03 160.71 -56.889 38.5 0.5 0.2 1830.15 366.03 160.71 56.889 38.5 0.5 0.2 1830.15 366.03 -78 -56.889 0 0.05 0.05 0.02 1000 600 360 NONE 1 -78 56.889 0 0.05 0.05 0.02 1000 600 360 NONE 1 76 -56.889 0 0.80 0.50 0.02 5400 1600 0 LEFT 1 76 56.889 0 0.80 0.50 0.02 5400 1600 0 RIGHT 1 18.44 0 -10 0.8 0.5 0.02 1800 600 10 NONE 0 93 -51 -10 0.8 0.5 0.02 5400 400 0.0 NONE 0 93 52 -10 0.8 0.5 0.02 5400 400 0.0 NONE 0 -19.7 0 26.6 0.0 0 0 4 -37.7 0 26.6 0.0 0.0 0.0 1 15 -19.7 0 26.6 0.0 0 0 4 -37.7 0 26.6 0.0 0.0 0.0 1 15 48 -44 55 129.43 0.0 AVGAS 48 44 55 129.43 0.0 AVGAS 48 -44 55 204 0.0 AVGAS 48 44 55 204 0.0 AVGAS -10 0 26 0.1 0.0 1 AVGAS fcs/elevator-cmd-norm -1 1 /sim/model/c172p/cockpit/yoke-elevator fcs/elevator-cmd-norm-filtered fcs/pitch-trim-cmd-norm -1 1 fcs/pitch-trim-sum 0.01745 -28 23 fcs/elevator-pos-rad fcs/elevator-pos-deg -28 23 -1 1 fcs/elevator-pos-norm fcs/aileron-cmd-norm -1 1 /sim/model/c172p/cockpit/yoke-aileron fcs/aileron-cmd-norm-filtered fcs/roll-trim-cmd-norm -1 1 fcs/roll-trim-sum 0.01745 -20 15 fcs/left-aileron-pos-rad fcs/left-aileron-pos-deg -20 15 -1 1 fcs/left-aileron-pos-norm -fcs/roll-trim-sum 0.01745 -20 15 fcs/right-aileron-pos-rad fcs/right-aileron-pos-deg -20 15 1 -1 fcs/right-aileron-pos-norm fcs/rudder-cmd-norm -1 1 /sim/model/c172p/cockpit/pedals-rudder fcs/rudder-cmd-norm-filtered fcs/yaw-trim-cmd-norm fcs/yaw-trim-cockpit -1 1 fcs/yaw-trim-sum 0.01745 -16 16 fcs/rudder-pos-rad fcs/rudder-pos-deg -16 16 -1 1 fcs/rudder-pos-norm /sim/model/c172p/securing/chock-visible /fdm/jsbsim/damage/repairing /controls/gear/brake-parking fcs/parking-brake-sum /controls/gear/brake-left fcs/left-brake-cmd-norm fcs/parking-brake-sum /controls/gear/brake-right fcs/right-brake-cmd-norm /gear/gear[0]/compression-norm gt 0.001 fcs/left-brake-cmd-norm -1 fcs/right-brake-cmd-norm 1 fcs/nose-gear-right-brake-steer-factor fcs/nose-gear-left-brake-steer-factor /gear/gear[0]/rollspeed-ms gt 0.25 fcs/brake-influence-enabled fcs/brake-sum fcs/brake-sum-adjusted/controls/flight/rudder -1 0 1 -1 -30 0 10 0 -10 0 10 1 -10 0 30
fcs/nws-cmd-deg fcs/nws-enabled fcs/nws-cmd-deg-adjusted 80 fcs/steer-pos-deg fcs/flap-input-norm /systems/electrical/outputs/flaps le 16 fcs/flap-input-norm 0 10 20 30 fcs/flap-pos-deg fcs/flap-pos-deg 0 30 0 1 fcs/flap-pos-norm /controls/flight/flaps 0 1 /sim/model/c172p/cockpit/flaps-lever /controls/engines/engine/primer/controls/engines/current-engine/throttle 0.09 0.1 0.5 0.51 2 0 0 0 0 3 0 1 1 0 4 0 1 1 0 5 0 1 1 0 6 0 1 1 0 7 0 0 0 0
fcs/mixture-cmd-norm[0] fcs/mixture-primer-cmd fcs/mixture-cmd-norm[1] fcs/mixture-primer-cmd fcs/mixture-pos-norm[0] /controls/engines/engine/use-primer eq 1 /engines/engine[0]/oil-temperature-degf le 75 fcs/mixture-pos-norm[1] /controls/engines/engine/use-primer eq 1 /engines/engine[1]/oil-temperature-degf le 75 gear/gear-input-norm /sim/model/c172p/hydraulics/hydraulic-pump eq 0 gear/gear-input-norm 0 1 gear/gear-pos-norm /controls/gear/water-rudder 0 1 -0.087 0.28 0.15 0.297 Change_in_drag_due_to_ground_effect aero/h_b-mac-ft 0.0000 0.4800 0.1000 0.5150 0.1500 0.6290 0.2000 0.7090 0.3000 0.8150 0.4000 0.8820 0.5000 0.9280 0.6000 0.9620 0.7000 0.9880 0.8000 1.0000 0.9000 1.0000 1.0000 1.0000 1.1000 1.0000
Change_in_lift_due_to_ground_effect aero/h_b-mac-ft 0.0000 1.2030 0.1000 1.1270 0.1500 1.0900 0.2000 1.0730 0.3000 1.0460 0.4000 1.0280 0.5000 1.0190 0.6000 1.0130 0.7000 1.0080 0.8000 1.0060 0.9000 1.0030 1.0000 1.0020 1.1000 1.0000
propeller induced velocity propulsion/engine/prop-induced-velocity_fps propulsion/engine[1]/prop-induced-velocity_fps q bar due to the propeller induced velocity aero/function/vel-propwash-fps aero/function/vel-propwash-fps atmosphere/rho-slugs_ft3 0.5 velocity including the propulsion induced velocity. velocities/u-aero-fps propulsion/engine/prop-induced-velocity_fps propulsion/engine[1]/prop-induced-velocity_fps q bar including the propulsion induced velocity. aero/function/velocity-induced-fps aero/function/velocity-induced-fps atmosphere/rho-slugs_ft3 0.5 Total damage on wings wing-damage/left-wing wing-damage/right-wing 0.5 Averaged aileron position fcs/left-aileron-pos-rad fcs/right-aileron-pos-rad -1 Drag_at_zero_lift aero/qbar-psf metrics/Sw-sqft 0.027 gear/drag-coef[1] gear/drag-coef[2] gear/drag-coef[3] gear/drag-coef[4] gear/drag-coef[5] gear/drag-coef[6] Delta_drag_due_to_flap_deflection aero/qbar-psf metrics/Sw-sqft aero/function/kCDge fcs/flap-pos-deg 0.0000 0.0000 10.0000 0.0070 20.0000 0.0120 30.0000 0.0180
Drag_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/function/kCDge aero/alpha-radfcs/flap-pos-deg 0 10 20 30 -0.0873 0.0041 0 0.0005 0.0014 -0.0698 0.0013 0.0004 0.0025 0.0041 -0.0524 0.0001 0.0023 0.0059 0.0084 -0.0349 0.0003 0.0057 0.0108 0.0141 -0.0175 0.002 0.0105 0.0172 0.0212 0.0000 0.0052 0.0168 0.0251 0.0299 0.0175 0.0099 0.0248 0.0346 0.0402 0.0349 0.0162 0.0342 0.0457 0.0521 0.0524 0.024 0.0452 0.0583 0.0655 0.0698 0.0334 0.0577 0.0724 0.0804 0.0873 0.0442 0.0718 0.0881 0.0968 0.1047 0.0566 0.0874 0.1053 0.1148 0.1222 0.0706 0.1045 0.124 0.1343 0.1396 0.086 0.1232 0.1442 0.1554 0.1571 0.0962 0.1353 0.1573 0.169 0.1745 0.1069 0.1479 0.1708 0.183 0.1920 0.118 0.161 0.1849 0.1975 0.2094 0.1298 0.1746 0.1995 0.2126 0.2269 0.1424 0.1892 0.2151 0.2286 0.2443 0.1565 0.2054 0.2323 0.2464 0.3491 0.2537 0.3298 0.3755 0.3983 0.5236 0.45 0.585 0.666 0.7065 0.6981 0.7 0.91 1.036 1.099 0.8727 1 1.3 1.48 1.57 1.0472 1.35 1.755 1.998 2.1195 1.2217 1.5 1.95 2.22 2.355 1.3963 1.57 2.041 2.3236 2.4649 1.5710 1.6 2.08 2.368 2.512
gear/drag-coef[1] gear/drag-coef[2] gear/drag-coef[3] gear/drag-coef[4] gear/drag-coef[5] gear/drag-coef[6] Drag_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/mag-elevator-pos-rad 0.0000 Drag_due_to_sideslip aero/qbar-psf metrics/Sw-sqft aero/mag-beta-rad 0.1500 gear/drag-coef[1] gear/drag-coef[2] gear/drag-coef[3] gear/drag-coef[4] gear/drag-coef[5] gear/drag-coef[6] Drag_due_to_door_left aero/qbar-psf metrics/Sw-sqft /sim/model/door-positions/leftDoor/position-norm-effective 0.0300 Drag_due_to_door_right aero/qbar-psf metrics/Sw-sqft /sim/model/door-positions/rightDoor/position-norm-effective 0.0300 Drag_due_to_door_left aero/qbar-psf metrics/Sw-sqft /sim/model/door-positions/baggageDoor/position-norm-effective 0.0300 Drag_due_to_window_left aero/qbar-psf metrics/Sw-sqft /sim/model/door-positions/leftWindow/position-norm 0.0010 Drag_due_to_window_right aero/qbar-psf metrics/Sw-sqft /sim/model/door-positions/rightWindow/position-norm 0.0010 Side_force_due_to_beta aero/qbar-psf metrics/Sw-sqft aero/beta-radfcs/flap-pos-deg 0.0000 30.0000 -0.3490 0.1370 0.1060 0.0000 0.0000 0.0000 0.3490 -0.1370 -0.1060
Side_force_due_to_rudder aero/qbar-psf metrics/Sw-sqft fcs/rudder-pos-rad 0.150 Lift_due_to_alpha aero/qbar-psf metrics/Sw-sqft aero/function/kCLge aero/alpha-radaero/stall-hyst-norm 0.00 1.00 -0.09 -0.22 -0.22 0.00 0.25 0.25 0.09 0.73 0.73 0.10 0.83 0.78 0.12 0.92 0.79 0.14 1.02 0.81 0.16 1.08 0.82 0.17 1.13 0.83 0.19 1.19 0.85 0.21 1.25 0.86 0.24 1.35 0.88 0.26 1.44 0.90 0.28 1.47 0.92 0.30 1.43 0.95 0.32 1.38 0.99 0.34 1.30 1.05 0.36 1.15 1.15 0.52 1.47 1.47 0.70 1.65 1.65 0.87 1.47 1.47 1.05 1.17 1.17 1.57 0.01 0.01
aero/function/total-wing-damage 0.0000 1 1.0000 0
Delta_lift_due_to_flap_deflection aero/qbar-psf metrics/Sw-sqft aero/function/kCLge fcs/flap-pos-deg 0.0000 0.0000 10.0000 0.2000 20.0000 0.3000 30.0000 0.3500
Lift_due_to_Elevator_Deflection aero/qbar-psf metrics/Sw-sqft fcs/elevator-pos-rad 0.4300 Lift_due_to_alpha_rate aero/qbarUW-psf metrics/Sw-sqft aero/alphadot-rad_sec aero/ci2vel 1.7000 Lift_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft velocities/q-aero-rad_sec aero/ci2vel 3.9000 Roll_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad -0.092 aero/alpha-wing-rad 0.279 1 0.297 3.5
Roll_moment_due_to_roll_rate_(roll_damping) aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/p-aero-rad_sec -0.484 Roll_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec fcs/flap-pos-deg 0.0000 0.0798 30 0.1246
aero/alpha-wing-radvelocities/r-aero-rad_secaero/stall-hyst-norm -0.15 -0.1 0 0.1 0.15 0.279 1 1 1 1 1 0.297 35 30 1 30 35 0.5 5 5 1 5 5 -0.15 -0.1 0 0.1 0.15 0.297 35 30 1 30 35 0.5 5 5 1 5 5
Roll_moment_due_to_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/aileron-pos-rad-avgd 0.229 aero/alpha-wing-radaero/stall-hyst-norm 0 1 0.279 1 0.3 0.297 0.3 0.3 0.611 -0.1 -0.1
aero/function/total-wing-damage 0.0000 1 1.0000 0
Roll_moment_due_to_rudder aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad 0.0147 Roll_moment_due_to_damaged_left_wing aero/qbar-psf metrics/Sw-sqft metrics/bw-ft wing-damage/left-wing -0.3 Roll_moment_due_to_damaged_right_wing aero/qbar-psf metrics/Sw-sqft metrics/bw-ft wing-damage/right-wing 0.3 Pitching_moment_at_zero_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/qbar-psf 13.6 0.09 21.2 0.04
Pitch_moment_due_to_alpha aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/alpha-rad -1.8 aero/alpha-deg 20 1 25 0.6 35 0.4 45 0.5 55 0.4 65 0.2 90 0.1
Pitch_moment_due_to_pitch_rate aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel velocities/q-aero-rad_sec -12.4000 Pitch_moment_due_to_alpha_rate aero/qbarUW-psf metrics/Sw-sqft metrics/cbarw-ft aero/ci2vel aero/alphadot-rad_sec -7.2700 Pitch_moment_due_to_elevator_deflection aero/function/qbar-induced-psf metrics/Sw-sqft metrics/cbarw-ft fcs/elevator-pos-rad -1.28 fcs/elevator-pos-radaero/alpha-deg 18 25 35 45 55 65 90 -0.49 1 0.5 0.2 0.1 0.1 0.1 0.1 0 1 0.6 0.3 0.15 0.1 0.1 0.1 0.40 1 0.9 0.8 0.7 0.6 0.5 0.4
Delta_pitching_moment_due_to_flap_deflection aero/qbar-psf metrics/Sw-sqft metrics/cbarw-ft fcs/flap-pos-deg 0.0000 0.0000 10.0000 -0.0654 20.0000 -0.0981 30.0000 -0.1140
0.7 Yaw_moment_due_to_beta aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/beta-rad -0.3490 -0.0205 0.0000 0.0000 0.3490 0.0205
Yaw_moment_due_to_spiraling_propwash aero/function/qbar-propwash-psf metrics/Sw-sqft metrics/bw-ft -0.05 aero/coefficient/spiral-propwash-coeff Yaw_moment_due_to_yaw_rate aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_sec -0.0937 Yaw_moment_due_to_flat_spin aero/qbar-psf metrics/Sw-sqft metrics/bw-ft aero/bi2vel velocities/r-aero-rad_secaero/alpha-wing-rad 0.279 0.4 -15 0 0 -5 0 0 -3 0 -0.25 -1 0 0 0 0 0 1 0 0 3 0 0.25 5 0 0 15 0 0
Yaw_moment_due_to_aileron aero/qbar-psf metrics/Sw-sqft metrics/bw-ft fcs/aileron-pos-rad-avgd aero/alpha-wing-radaero/beta-rad -0.35 0 0.35 0 -0.0216 -0.0216 -0.0216 0.070 -0.039 -0.0786 -0.039 0.094 -0.025 -0.0504 -0.025
aero/function/total-wing-damage 0.0000 1 1.0000 0
Yaw_moment_due_to_rudder aero/function/qbar-induced-psf metrics/Sw-sqft metrics/bw-ft fcs/rudder-pos-rad -0.0645 32.6 0 38.5 1.0 0.0 0.0 32.6 0 38.5 0.0 1.0 0.0 32.6 0 38.5 0.0 0.0 -1.0 20.6 0 38.5 0.0 0.0 -1.0 44.6 0 38.5 0.0 0.0 -1.0 32.6 -12.0 38.5 1.0 0.0 0.0 32.6 12.0 38.5 1.0 0.0 0.0 32.6 -12.0 38.5 0.0 0.0 -1.0 32.6 12.0 38.5 0.0 0.0 -1.0 0.1188 -2.2998 0.4008 0.0 0.0 1.0 0.1188 2.2998 0.4008 0.0 0.0 1.0 4.7116 0.0000 -0.6663 0.0 0.0 1.0 32.0 0.0 52.5 1.0 0.0 0.0 1.0 0.0 0.0 0.0 0.0 0.0 1.0 0.0 0.0 0.0 0.0 0.0 0.0 1.0 0.0 0.0 0.0 1.0 1.0 0.0 0.0 4.7116 0.0000 -0.6663 0.0 0.0 0.0