JSBSim Flight Dynamics Model v0.9.10.111805 [cfg file spec v2.0] JSBSim startup beginning ... Reading Aircraft Configuration File: A300B2-103 Version: 2.0 This aircraft model is an ALPHA release!!! This aircraft model may not even properly load, and probably will not fly as expected. Use this model for development purposes ONLY!!! Model Author: Aeromatic v 0.9 Creation Date: now Version: 0.0 Description: Models a A300B2-103. Aircraft Metrics: WingArea: 2798.9 WingSpan: 147.11 Incidence: 1.833 Chord: 21.686 H. Tail Area: 747.554 H. Tail Arm: 82.243 V. Tail Area: 486.529 V. Tail Arm: 84.695 Eyepoint (x, y, z): 147.77 , -30 , 70 Ref Pt (x, y, z): 1204.5 , 0 , -5.926 Visual Ref Pt (x, y, z): 0 , 0 , 0 Mass and Balance: baseIxx: 1.90335e+06 slug-ft2 baseIyy: 6.28872e+06 slug-ft2 baseIzz: 7.76786e+06 slug-ft2 baseIxy: -0 slug-ft2 baseIxz: -0 slug-ft2 baseIyz: -0 slug-ft2 EmptyWeight: 189002 lbm CG (x, y, z): 1204.5 , 0 , -29.74 Ground Reactions: BOGEY NOSE Location: 513.917 , 0 , -189.37 Spring Constant: 90625.5 Damping Constant: 30208.5 Dynamic Friction: 0.5 Static Friction: 0.8 Rolling Friction: 0.02 Steering Type: STEERABLE Grouping: NONE Max Steer Angle: 5 Retractable: 0 BOGEY LEFT_MAIN_FWD Location: 1218.85 , -188.976 , -189.37 Spring Constant: 151042 Damping Constant: 30208.5 Dynamic Friction: 0.5 Static Friction: 0.8 Rolling Friction: 0.02 Steering Type: FIXED Grouping: LEFT Max Steer Angle: 0 Retractable: 0 BOGEY LEFT_MAIN_AFT Location: 1273.85 , -188.976 , -189.37 Spring Constant: 151042 Damping Constant: 30208.5 Dynamic Friction: 0.5 Static Friction: 0.8 Rolling Friction: 0.02 Steering Type: FIXED Grouping: LEFT Max Steer Angle: 0 Retractable: 0 BOGEY RIGHT_MAIN_FWD Location: 1218.85 , 188.976 , -189.37 Spring Constant: 151042 Damping Constant: 30208.5 Dynamic Friction: 0.5 Static Friction: 0.8 Rolling Friction: 0.02 Steering Type: FIXED Grouping: RIGHT Max Steer Angle: 0 Retractable: 0 BOGEY RIGHT_MAIN_AFT Location: 1273.85 , 188.976 , -189.37 Spring Constant: 151042 Damping Constant: 30208.5 Dynamic Friction: 0.5 Static Friction: 0.8 Rolling Friction: 0.02 Steering Type: FIXED Grouping: RIGHT Max Steer Angle: 0 Retractable: 0 STRUCTURE LEFT_WING Location: 1489.87 , -882.607 , 29.32 Spring Constant: 302085 Damping Constant: 60417 Dynamic Friction: 0.5 Static Friction: 0.8 STRUCTURE RIGHT_WING Location: 1489.87 , 882.607 , 29.32 Spring Constant: 302085 Damping Constant: 60417 Dynamic Friction: 0.5 Static Friction: 0.8 Propulsion: X = 1489.87 Y = -882.607 Z = -29.32 Pitch = 0 Yaw = 0 2 dimensional table with 6 rows, 7 columns. -10000.0000 0.0000 10000.0000 20000.0000 30000.0000 40000.0000 50000.0000 0.0000 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467 0.2000 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342 0.4000 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203 0.6000 0.0000 0.0000 0.0000 0.0000 0.0276 0.0718 0.1073 0.8000 0.0000 0.0000 0.0000 0.0000 0.0474 0.0868 0.0900 1.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0552 0.0800 Function: IdleThrust 2 dimensional table with 8 rows, 7 columns. -10000.0000 0.0000 10000.0000 20000.0000 30000.0000 40000.0000 50000.0000 0.0000 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490 0.2000 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430 0.4000 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450 0.6000 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540 0.8000 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700 1.0000 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950 1.2000 1.4850 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250 1.4000 1.5941 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630 Function: MilThrust X = 1489.8670 Y = 882.6070 Z = -29.3200 Pitch = 0.0000 Yaw = 0.0000 2 dimensional table with 6 rows, 7 columns. -10000.0000 0.0000 10000.0000 20000.0000 30000.0000 40000.0000 50000.0000 0.0000 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467 0.2000 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342 0.4000 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203 0.6000 0.0000 0.0000 0.0000 0.0000 0.0276 0.0718 0.1073 0.8000 0.0000 0.0000 0.0000 0.0000 0.0474 0.0868 0.0900 1.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0552 0.0800 Function: IdleThrust 2 dimensional table with 8 rows, 7 columns. -10000.0000 0.0000 10000.0000 20000.0000 30000.0000 40000.0000 50000.0000 0.0000 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490 0.2000 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430 0.4000 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450 0.6000 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540 0.8000 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700 1.0000 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950 1.2000 1.4850 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250 1.4000 1.5941 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630 Function: MilThrust FUEL tank holds 29506.5000 lbs. FUEL currently at 1.0000% of maximum capacity Tank location (X, Y, Z): 1149.8270, -307.2840, -24.2920 Effective radius: 0.0000 inches Initial temperature: -9999.0000 Fahrenheit FUEL tank holds 29506.5000 lbs. FUEL currently at 1.0000% of maximum capacity Tank location (X, Y, Z): 1149.8270, 307.2840, -24.2920 Effective radius: 0.0000 inches Initial temperature: -9999.0000 Fahrenheit Flight Control (FCS: FCS: A300B2-103) Loading Component "Pitch Trim Sum" of type: SUMMER INPUTS: elevator-cmd-norm pitch-trim-cmd-norm CLIPTO: -1.0000, 1.0000 Loading Component "Elevator Control" of type: AEROSURFACE_SCALE INPUT: pitch-trim-sum GAIN: 0.0180 OUTPUT: elevator-pos-rad In/Out Mapping: Input MIN: -1.0000 Input MAX: 1.0000 Output MIN: -30.0000 Output MAX: 15.0000 Loading Component "Elevator position normalized" of type: AEROSURFACE_SCALE INPUT: elevator-pos-deg GAIN: 1.0000 OUTPUT: elevator-pos-norm In/Out Mapping: Input MIN: -30.0000 Input MAX: 15.0000 Output MIN: -1.0000 Output MAX: 1.0000 Loading Component "Roll Trim Sum" of type: SUMMER INPUTS: aileron-cmd-norm roll-trim-cmd-norm CLIPTO: -1.0000, 1.0000 Loading Component "Left Aileron Control" of type: AEROSURFACE_SCALE INPUT: roll-trim-sum GAIN: 0.0200 OUTPUT: left-aileron-pos-rad In/Out Mapping: Input MIN: -1.0000 Input MAX: 1.0000 Output MIN: -25.0000 Output MAX: 25.0000 Loading Component "Right Aileron Control" of type: AEROSURFACE_SCALE INPUT: -roll-trim-sum GAIN: 0.0200 OUTPUT: right-aileron-pos-rad In/Out Mapping: Input MIN: -1.0000 Input MAX: 1.0000 Output MIN: -25.0000 Output MAX: 25.0000 Loading Component "Left Aileron position normalized" of type: AEROSURFACE_SCALE INPUT: left-aileron-pos-deg GAIN: 1.0000 OUTPUT: left-aileron-pos-norm In/Out Mapping: Input MIN: -25.0000 Input MAX: 25.0000 Output MIN: -0.7500 Output MAX: 1.0000 Loading Component "Right Aileron position normalized" of type: AEROSURFACE_SCALE INPUT: right-aileron-pos-deg GAIN: 1.0000 OUTPUT: right-aileron-pos-norm In/Out Mapping: Input MIN: -25.0000 Input MAX: 25.0000 Output MIN: -0.7500 Output MAX: 1.0000 Loading Component "Yaw Damper Rate" of type: PURE_GAIN INPUT: r-rad_sec GAIN: 2.0000 Loading Component "Yaw Damper Beta" of type: PURE_GAIN INPUT: beta-rad GAIN: -5.0000 Loading Component "Yaw Trim Sum" of type: SUMMER INPUTS: rudder-cmd-norm yaw-trim-cmd-norm CLIPTO: -1.0000, 1.0000 Loading Component "Rudder Sum" of type: SUMMER INPUTS: yaw-trim-sum yaw-damper-rate yaw-damper-beta CLIPTO: -1.0000, 1.0000 Loading Component "Rudder Control" of type: AEROSURFACE_SCALE INPUT: rudder-sum GAIN: 0.0175 OUTPUT: rudder-pos-rad In/Out Mapping: Input MIN: -1.0000 Input MAX: 1.0000 Output MIN: -25.0000 Output MAX: 25.0000 Loading Component "Rudder position normalized" of type: AEROSURFACE_SCALE INPUT: rudder-pos-deg GAIN: 1.0000 OUTPUT: rudder-pos-norm In/Out Mapping: Input MIN: -25.0000 Input MAX: 25.0000 Output MIN: -1.0000 Output MAX: 1.0000 Loading Component "Flaps Control" of type: KINEMATIC INPUT: flap-cmd-norm DETENTS: 2 0.0000 0.0000 25.0000 25.0000 OUTPUT: flap-pos-deg Loading Component "Flap position normalized" of type: AEROSURFACE_SCALE INPUT: flap-pos-deg GAIN: 1.0000 OUTPUT: flap-pos-norm In/Out Mapping: Input MIN: 0.0000 Input MAX: 25.0000 Output MIN: 0.0000 Output MAX: 1.0000 Loading Component "Gear Control" of type: KINEMATIC INPUT: gear-cmd-norm DETENTS: 2 0.0000 0.0000 1.0000 10.0000 OUTPUT: gear-pos-norm Loading Component "Speedbrake" of type: KINEMATIC INPUT: speedbrake-cmd-norm DETENTS: 2 0.0000 0.0000 1.0000 2.0000 OUTPUT: speedbrake-pos-norm Aerodynamics: 1 dimensional table with 5 rows. -0.2000 -0.6800 0.0000 0.2000 0.2300 1.2000 0.6000 0.6000 0.0000 0.0000 Function: aero/coefficient/CLalpha Function: aero/coefficient/dCLflap Function: aero/coefficient/dCLsb Function: aero/coefficient/CLde 1 dimensional table with 6 rows. -1.5700 1.5000 -0.2600 0.0260 0.0000 0.0200 0.2600 0.0260 1.5700 1.5000 0.0000 0.0000 Function: aero/coefficient/CD0 Function: aero/coefficient/CDi 1 dimensional table with 5 rows. 0.0000 0.0000 0.7900 0.0000 1.1000 0.0230 1.8000 0.0150 0.0000 0.0000 Function: aero/coefficient/CDmach Function: aero/coefficient/CDflap Function: aero/coefficient/CDgear Function: aero/coefficient/CDsb 1 dimensional table with 6 rows. -1.5700 1.2300 -0.2600 0.0500 0.0000 0.0000 0.2600 0.0500 1.5700 1.2300 0.0000 0.0000 Function: aero/coefficient/CDbeta Function: aero/coefficient/CDde Function: aero/coefficient/CYb Function: aero/coefficient/Clb Function: aero/coefficient/Clp Function: aero/coefficient/Clr 1 dimensional table with 3 rows. 0.0000 0.1000 2.0000 0.0330 0.0000 0.0000 Function: aero/coefficient/Clda Function: aero/coefficient/Cldr Function: aero/coefficient/Cmalpha 1 dimensional table with 3 rows. 0.0000 -1.2000 2.0000 -0.3000 0.0000 0.0000 Function: aero/coefficient/Cmde Function: aero/coefficient/Cmq Function: aero/coefficient/Cmadot Function: aero/coefficient/Cnb Function: aero/coefficient/Cnr Function: aero/coefficient/Cndr Function: aero/coefficient/Cnda JSBSim startup complete open /dev/[sound/]dsp: Device or resource busy Audio initialization failed! There was an error opening the ALC device Reading xml electrical system model from /usr/local/FlightGear/share/FlightGear/data/Aircraft/Generic/generic-electrical.xml Incorrect path in configuration file. Touchdown report for NOSE Sink rate at contact: 0.0000 fps, 0.0000 mps Contact ground speed: 0.0000 knots, 0.0000 mps Maximum contact force: 1124843.6956 lbs, 5003304.7578 Newtons Maximum strut travel: 148.9440 inches, 378.3178 cm Distance traveled: 0.0000 ft, 0.0000 meters Touchdown report for LEFT_MAIN_FWD Sink rate at contact: 0.0000 fps, 0.0000 mps Contact ground speed: 0.0000 knots, 0.0000 mps Maximum contact force: 1940411.5936 lbs, 8630950.7683 Newtons Maximum strut travel: 154.1615 inches, 391.5702 cm Distance traveled: 0.0000 ft, 0.0000 meters Touchdown report for LEFT_MAIN_AFT Sink rate at contact: 0.0000 fps, 0.0000 mps Contact ground speed: 0.0000 knots, 0.0000 mps Maximum contact force: 1945534.4276 lbs, 8653737.1340 Newtons Maximum strut travel: 154.5685 inches, 392.6040 cm Distance traveled: 0.0000 ft, 0.0000 meters Touchdown report for RIGHT_MAIN_FWD Sink rate at contact: 0.0000 fps, 0.0000 mps Contact ground speed: 0.0000 knots, 0.0000 mps Maximum contact force: 1940411.5934 lbs, 8630950.7674 Newtons Maximum strut travel: 154.1615 inches, 391.5702 cm Distance traveled: 0.0000 ft, 0.0000 meters Touchdown report for RIGHT_MAIN_AFT Sink rate at contact: 0.0000 fps, 0.0000 mps Contact ground speed: 0.0000 knots, 0.0000 mps Maximum contact force: 1945534.4277 lbs, 8653737.1344 Newtons Maximum strut travel: 154.5685 inches, 392.6040 cm Distance traveled: 0.0000 ft, 0.0000 meters Touchdown report for LEFT_WING Sink rate at contact: 0.0000 fps, 0.0000 mps Contact ground speed: 0.0000 knots, 0.0000 mps Maximum contact force: 0.0000 lbs, 0.0000 Newtons Maximum strut travel: 0.0000 inches, 0.0000 cm Distance traveled: 0.0000 ft, 0.0000 meters Touchdown report for RIGHT_WING Sink rate at contact: 0.0000 fps, 0.0000 mps Contact ground speed: 0.0000 knots, 0.0000 mps Maximum contact force: 0.0000 lbs, 0.0000 Newtons Maximum strut travel: 0.0000 inches, 0.0000 cm Distance traveled: 0.0000 ft, 0.0000 meters altitude = 495.0879 sea level radius = 20892403.7404 latitude = 0.7579 longitude = 0.0239 Ground Trim Initial Theta: 0.0000 Used gear unit 1 as aft and 0 as forward Sorry, wdot doesn't appear to be trimmable Trim failed Trim Results: Altitude AGL: 15.00 wdot: 3.22e+01 Tolerance: 1e-03 Failed Pitch Angle: 0.00 qdot: -2.74e-05 Tolerance: 1e-04 Passed Trim Statistics: Total Iterations: 1 Sub-iterations: wdot: 0 average: 0.00 successful: 0 stability: 2.00 qdot: 0 average: 0.00 successful: 1 stability: 2.00 Run Count: 22