rendered paste body 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