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| >> TestJSBSim Run 737 example Current directory: C:\Users\Administrator\AppData\Local\JSBSimI/O config input: ex737cruise_io
JSBSim S-Function is initializing...
JSBSim Flight Dynamics Model v1.2.0 [GitHub build 1191/commit 4864e7389676bc0e9ac487b087650db74a31204c] Nov 5 2023 13:53:35 [JSBSim-ML v2.0]
JSBSim startup beginning ...
Simulation dt set to 0.008333 Setting up JSBSim with standard 'aircraft', 'engine', and 'system' paths. Loading aircraft '737' ... Reading Aircraft Configuration File: 737 Version: 2.0
This aircraft model is a BETA release!!!
This aircraft model probably will not fly as expected.
Use this model for development purposes ONLY!!!
Description: Models a Boeing 737. Model Author: Dave Culp Creation Date: 2006-01-04 Version: $Revision: 1.43 $
Aircraft Metrics: WingArea: 1171 WingSpan: 94.7 Incidence: 0 Chord: 12.31 H. Tail Area: 348 H. Tail Arm: 48.04 V. Tail Area: 297 V. Tail Arm: 44.5 Eyepoint (x, y, z): 80 , -30 , 70 Ref Pt (x, y, z): 625 , 0 , 24 Visual Ref Pt (x, y, z): 0 , 0 , 0
Mass and Balance: baseIxx: 562000 slug-ft2 baseIyy: 1.473e+06 slug-ft2 baseIzz: 1.894e+06 slug-ft2 baseIxy: -0 slug-ft2 baseIxz: 8000 slug-ft2 baseIyz: -0 slug-ft2 Empty Weight: 83000 lbm CG (x, y, z): 639 , 0 , -40
Ground Reactions: BOGEY Nose Gear Location: 158 , 0 , -84 Spring Constant: 90000 Damping Constant: 4000 (linear) Rebound Damping Constant: 8000 (linear) Dynamic Friction: 0.5 Static Friction: 0.8 Rolling Friction: 0.02 Steering Type: STEERABLE Grouping: NONE Max Steer Angle: 35 Retractable: 1 BOGEY Left Main Gear Location: 648 , -100 , -84 Spring Constant: 120000 Damping Constant: 10000 (linear) Rebound Damping Constant: 20000 (linear) Dynamic Friction: 0.5 Static Friction: 0.8 Rolling Friction: 0.02 Steering Type: FIXED Grouping: LEFT Max Steer Angle: 0 Retractable: 1 BOGEY Right Main Gear Location: 648 , 100 , -84 Spring Constant: 120000 Damping Constant: 10000 (linear) Rebound Damping Constant: 20000 (linear) Dynamic Friction: 0.5 Static Friction: 0.8 Rolling Friction: 0.02 Steering Type: FIXED Grouping: RIGHT Max Steer Angle: 0 Retractable: 1
Propulsion: (FUEL) tank holds 10200 lbs. FUEL currently at 98.0392 Tank location (X, Y, Z): 520, -80, -18 Effective radius: 0 inches Initial temperature: -9999 Fahrenheit Priority: 1 (FUEL) tank holds 10200 lbs. FUEL currently at 98.0392 Tank location (X, Y, Z): 520, 80, -18 Effective radius: 0 inches Initial temperature: -9999 Fahrenheit Priority: 1 (FUEL) tank holds 15000 lbs. FUEL currently at 26.6667 Tank location (X, Y, Z): 480, 0, -18 Effective radius: 0 inches Initial temperature: -9999 Fahrenheit Priority: 1 2 dimensional table with 6 rows, 8 columns. -10000.0000 0.0000 10000.0000 20000.0000 30000.0000 40000.0000 50000.0000 60000.0000 0.0000 0.0420 0.0436 0.0528 0.0694 0.0899 0.1183 0.1467 0.0000 0.2000 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342 0.0000 0.4000 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203 0.0000 0.6000 0.0000 0.0000 0.0000 0.0000 0.0276 0.0718 0.1073 0.0000 0.8000 0.0000 0.0000 0.0000 0.0000 0.0174 0.0468 0.0900 0.0000 1.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0422 0.0700 0.0000 Function: propulsion/engine[0]/IdleThrust 2 dimensional table with 7 rows, 8 columns. -10000.0000 0.0000 10000.0000 20000.0000 30000.0000 40000.0000 50000.0000 60000.0000 0.0000 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490 0.0000 0.2000 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430 0.0000 0.4000 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450 0.0000 0.6000 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540 0.0000 0.8000 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700 0.0000 1.0000 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950 0.0000 1.2000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 Function: propulsion/engine[0]/MilThrust X = 540.0000 Y = -193.0000 Z = -40.0000 Pitch = 0.0000 degrees Yaw = 0.0000 degrees 2 dimensional table with 6 rows, 8 columns. -10000.0000 0.0000 10000.0000 20000.0000 30000.0000 40000.0000 50000.0000 60000.0000 0.0000 0.0420 0.0436 0.0528 0.0694 0.0899 0.1183 0.1467 0.0000 0.2000 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342 0.0000 0.4000 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203 0.0000 0.6000 0.0000 0.0000 0.0000 0.0000 0.0276 0.0718 0.1073 0.0000 0.8000 0.0000 0.0000 0.0000 0.0000 0.0174 0.0468 0.0900 0.0000 1.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0422 0.0700 0.0000 Function: propulsion/engine[1]/IdleThrust 2 dimensional table with 7 rows, 8 columns. -10000.0000 0.0000 10000.0000 20000.0000 30000.0000 40000.0000 50000.0000 60000.0000 0.0000 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490 0.0000 0.2000 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430 0.0000 0.4000 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450 0.0000 0.6000 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540 0.0000 0.8000 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700 0.0000 1.0000 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950 0.0000 1.2000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 Function: propulsion/engine[1]/MilThrust X = 540.0000 Y = 193.0000 Z = -40.0000 Pitch = 0.0000 degrees Yaw = 0.0000 degrees
FCS: FCS: 737
Channel Pitch
Loading Component "Pitch Trim Sum" of type: SUMMER Minimum limit: constant value -1.000000 Maximum limit: constant value 1.000000 INPUTS: elevator-cmd-norm pitch-trim-cmd-norm OUTPUT: pitch-trim-sum
Loading Component "Elevator Control" of type: AEROSURFACE_SCALE INPUT: pitch-trim-sum GAIN: constant value 1.000000 OUTPUT: elevator-pos-rad OUTPUT: elevator-control In/Out Mapping: Input MIN: -1.0000 Input MAX: 1.0000 Output MIN: -0.3000 Output MAX: 0.3000
Loading Component "Elevator Normalized" of type: AEROSURFACE_SCALE INPUT: elevator-pos-rad GAIN: constant value 1.000000 OUTPUT: elevator-pos-norm OUTPUT: elevator-normalized In/Out Mapping: Input MIN: -0.3000 Input MAX: 0.3000 Output MIN: -1.0000 Output MAX: 1.0000
Channel Roll
Loading Component "Roll Trim Sum" of type: SUMMER Minimum limit: constant value -1.000000 Maximum limit: constant value 1.000000 INPUTS: aileron-cmd-norm roll-trim-cmd-norm OUTPUT: roll-trim-sum
Loading Component "Left Aileron Control" of type: AEROSURFACE_SCALE INPUT: roll-trim-sum GAIN: constant value 1.000000 OUTPUT: left-aileron-pos-rad OUTPUT: left-aileron-control In/Out Mapping: Input MIN: -1.0000 Input MAX: 1.0000 Output MIN: -0.3500 Output MAX: 0.3500
Loading Component "Right Aileron Control" of type: AEROSURFACE_SCALE INPUT: -roll-trim-sum GAIN: constant value 1.000000 OUTPUT: right-aileron-pos-rad OUTPUT: right-aileron-control In/Out Mapping: Input MIN: -1.0000 Input MAX: 1.0000 Output MIN: -0.3500 Output MAX: 0.3500
Loading Component "Left aileron Normalized" of type: AEROSURFACE_SCALE INPUT: left-aileron-pos-rad GAIN: constant value 1.000000 OUTPUT: left-aileron-pos-norm OUTPUT: left-aileron-normalized In/Out Mapping: Input MIN: -0.3500 Input MAX: 0.3500 Output MIN: -1.0000 Output MAX: 1.0000
Loading Component "Right aileron Normalized" of type: AEROSURFACE_SCALE INPUT: right-aileron-pos-rad GAIN: constant value 1.000000 OUTPUT: right-aileron-pos-norm OUTPUT: right-aileron-normalized In/Out Mapping: Input MIN: -0.3500 Input MAX: 0.3500 Output MIN: -1.0000 Output MAX: 1.0000
Channel Yaw
Loading Component "Rudder Command Sum" of type: SUMMER Minimum limit: constant value -1.000000 Maximum limit: constant value 1.000000 INPUTS: rudder-cmd-norm yaw-trim-cmd-norm OUTPUT: rudder-command-sum
Loading Component "Yaw Damper" of type: SCHEDULED_GAIN 1 dimensional table with 3 rows. 0.0000 0.0000 0.1000 0.0000 0.1100 1.0000 INPUT: r-aero-rad_sec GAIN: constant value 1.000000 OUTPUT: yaw-damper Scheduled by table: 1 dimensional table with 3 rows. 0.0000 0.0000 0.1000 0.0000 0.1100 1.0000
Loading Component "Yaw Damper Final" of type: SCHEDULED_GAIN 1 dimensional table with 3 rows. 0.0000 0.0000 0.1000 0.0000 0.1100 1.0000 INPUT: yaw-damper GAIN: constant value 1.000000 OUTPUT: yaw-damper-final Scheduled by table: 1 dimensional table with 3 rows. 0.0000 0.0000 0.1000 0.0000 0.1100 1.0000
Loading Component "Rudder Sum" of type: SUMMER Minimum limit: constant value -1.000000 Maximum limit: constant value 1.000000 INPUTS: rudder-command-sum yaw-damper-final OUTPUT: rudder-sum
Loading Component "Rudder Control" of type: AEROSURFACE_SCALE INPUT: rudder-sum GAIN: constant value 1.000000 OUTPUT: rudder-pos-rad OUTPUT: rudder-control In/Out Mapping: Input MIN: -1.0000 Input MAX: 1.0000 Output MIN: -0.3500 Output MAX: 0.3500
Loading Component "Rudder Normalized" of type: AEROSURFACE_SCALE INPUT: rudder-pos-rad GAIN: constant value 1.000000 OUTPUT: rudder-pos-norm OUTPUT: rudder-normalized In/Out Mapping: Input MIN: -0.3500 Input MAX: 0.3500 Output MIN: -1.0000 Output MAX: 1.0000
Channel Flaps
Loading Component "Flaps Control" of type: KINEMATIC INPUT: flap-cmd-norm DETENTS: 9 0.0000 0.0000 0.1250 5.0000 0.2500 4.0000 0.3750 3.0000 0.5000 2.0000 0.6250 2.0000 0.7500 2.0000 0.8750 2.0000 1.0000 2.0000 OUTPUT: flap-pos-norm OUTPUT: flaps-control
Channel Landing Gear
Loading Component "Gear Control" of type: KINEMATIC INPUT: gear-cmd-norm DETENTS: 2 0.0000 0.0000 1.0000 5.0000 OUTPUT: gear-pos-norm OUTPUT: gear-control
Channel Flight Spoilers
Loading Component "Flight Spoilers Control" of type: KINEMATIC INPUT: speedbrake-cmd-norm DETENTS: 2 0.0000 0.0000 1.0000 0.6000 OUTPUT: speedbrake-pos-norm OUTPUT: flight-spoilers-control
Channel Ground Spoilers
Loading Component "Ground Spoilers Control" of type: KINEMATIC INPUT: spoiler-cmd-norm DETENTS: 2 0.0000 0.0000 1.0000 0.6000 OUTPUT: spoiler-pos-norm OUTPUT: ground-spoilers-control 1 dimensional table with 10 rows. 0.0000 0.0480 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 Function: aero/function/kCDge 1 dimensional table with 13 rows. 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 Function: aero/function/kCLge 1 dimensional table with 2 rows. 0.0000 1.0000 0.1000 0.8500 Function: aero/function/kCLsb 1 dimensional table with 2 rows. 0.0000 1.0000 0.1000 0.6000 Function: aero/function/kCLsp
Aerodynamics (Lift|Side|Drag axes):
1 dimensional table with 5 rows. -1.5700 1.5000 -0.2600 0.0420 0.0000 0.0210 0.2600 0.0420 1.5700 1.5000 Function: aero/coefficient/CD0 Function: aero/coefficient/CDi 1 dimensional table with 4 rows. 0.0000 0.0000 0.7900 0.0000 1.1000 0.0230 1.8000 0.0150 Function: aero/coefficient/CDmach Function: aero/coefficient/CDflap Function: aero/coefficient/CDgear Function: aero/coefficient/CDsb Function: aero/coefficient/CDsp 1 dimensional table with 5 rows. -1.5700 1.2300 -0.2600 0.0500 0.0000 0.0000 0.2600 0.0500 1.5700 1.2300 Function: aero/coefficient/CDbeta Function: aero/coefficient/CDde Function: aero/coefficient/CYb 1 dimensional table with 4 rows. -0.2000 -0.6800 0.0000 0.2000 0.2300 1.2000 0.4600 0.2000 Function: aero/coefficient/CLalpha Function: aero/coefficient/dCLflap Function: aero/coefficient/CLde Function: aero/coefficient/Clb Function: aero/coefficient/Clp Function: aero/coefficient/Clr 1 dimensional table with 2 rows. 0.0000 0.1000 2.0000 0.0330 Function: aero/coefficient/Clda Function: aero/coefficient/Cldr Function: aero/coefficient/Cmalpha 1 dimensional table with 2 rows. 0.0000 -1.2000 2.0000 -0.3000 Function: aero/coefficient/Cmde Function: aero/coefficient/Cmq Function: aero/coefficient/Cmadot Function: aero/coefficient/Cnb Function: aero/coefficient/Cnr Function: aero/coefficient/Cndr
Input data set: 0
Input data set: 1
Declared properties
'737' Aircraft File has been successfully loaded! Reset file: 'cruise_init' . Winsock DLL loaded ... Creating input TCP socket on port 5137 Successfully bound to TCP input socket on port 5137
Winsock DLL loaded ... Creating input UDP socket on port 5139 Successfully bound to UDP input socket on port 5139
Mass Properties Report (English units: lbf, in, slug-ft^2) Weight CG-X CG-Y CG-Z Ixx Iyy Izz Ixy Ixz Iyz Base Vehicle 83000.0 639.0 0.0 -40.0 562000.0 1473000.0 1894000.0 -0.0 8000.0 -0.0 0 Fuel 10000 520 -80 -18 0 0 0 1 Fuel 10000 520 80 -18 0 0 0 2 Fuel 4000 480 0 -18 0 0 0 Total: 107000.0 610.8 0.0 -35.1 591572.3 1539552.7 1986235.4 0.0 19109.1 0.0
End of vehicle configuration loading. -------------------------------------------------------------------------------
Simulation completed. Remember to reset the program by typing clearSF in the matlab command window! JSBSim S-Function Reset
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