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读取飞机xml文件：a 1982 Cessna 172P
"C:\jsbsim-master\aircraft\c172p\c172p.xml"
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JSBSim Flight Dynamics Model v1.2.0.dev1 Oct 5 2024 21:22:03
[JSBSim-ML v2.0]
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Reading Aircraft Configuration File: Cessna C-172 Skyhawk II
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 1982 Cessna 172P.
Model Author: Tony Peden
Creation Date: 1999-01-01
Version: $Revision: 1.91 $
Aircraft Metrics:
WingArea: 174.000000
WingSpan: 36.000000
Incidence: 0.000000
Chord: 4.900000
H. Tail Area: 21.900000
H. Tail Arm: 15.700000
V. Tail Area: 16.500000
V. Tail Arm: 15.700000
Eyepoint (x, y, z): 37.000000 , 0.000000 , 48.000000
Ref Pt (x, y, z): 43.200000 , 0.000000 , 59.400000
Visual Ref Pt (x, y, z): 42.600000 , 0.000000 , 38.500000
Mass and Balance:
baseIxx: 948.000000 slug-ft2
baseIyy: 1346.000000 slug-ft2
baseIzz: 1967.000000 slug-ft2
baseIxy: -0.000000 slug-ft2
baseIxz: 0.000000 slug-ft2
baseIyz: -0.000000 slug-ft2
Empty Weight: 1454.000000 lbm
CG (x, y, z): 41.000000 , 0.000000 , 36.500000
Point Mass Object: 190.000000 lbs. at X, Y, Z (in.): 36.000000 -14.000000 24.000000
Point Mass Object: 140.000000 lbs. at X, Y, Z (in.): 36.000000 14.000000 24.000000
Point Mass Object: 130.000000 lbs. at X, Y, Z (in.): 60.000000 -14.000000 24.000000
Point Mass Object: 106.000000 lbs. at X, Y, Z (in.): 60.000000 14.000000 24.000000
Point Mass Object: 120.000000 lbs. at X, Y, Z (in.): 95.000000 0.000000 24.000000
Point Mass Object: 80.000000 lbs. at X, Y, Z (in.): 41.000000 144.000000 36.000000
Ground Reactions:
BOGEY Nose Gear
Location: -6.800000 , 0.000000 , -20.000000
Spring Constant: 1800.000000
Damping Constant: 500.000000 (linear)
Rebound Damping Constant: 2000.000000 (linear)
Dynamic Friction: 0.500000
Static Friction: 0.800000
Rolling Friction: 0.022000
Steering Type: STEERABLE
Grouping: NONE
Max Steer Angle: 10.000000
Retractable: 0
BOGEY Left Main Gear
Location: 58.200000 , -50.250000 , -18.460000
Spring Constant: 5400.000000
Damping Constant: 160.000000 (linear)
Rebound Damping Constant: 320.000000 (linear)
Dynamic Friction: 0.500000
Static Friction: 0.800000
Rolling Friction: 0.022000
Steering Type: FIXED
Grouping: LEFT
Max Steer Angle: 0.000000
Retractable: 0
BOGEY Right Main Gear
Location: 58.200000 , 50.250000 , -18.460000
Spring Constant: 0.000000
Damping Constant: 0.000000 (linear)
Rebound Damping Constant: 0.000000 (linear)
Dynamic Friction: 0.500000
Static Friction: 0.800000
Rolling Friction: 0.022000
Steering Type: FIXED
Grouping: RIGHT
Max Steer Angle: 0.000000
Retractable: 0
STRUCTURE TAIL_SKID
Location: 188.000000 , 0.000000 , 8.000000
Spring Constant: 20000.000000
Damping Constant: 1000.000000 (linear)
Rebound Damping Constant: 1000.000000 (linear)
Dynamic Friction: 0.200000
Static Friction: 0.200000
STRUCTURE LEFT_TIP
Location: 43.200000 , -214.800000 , 59.400000
Spring Constant: 10000.000000
Damping Constant: 2000.000000 (linear)
Rebound Damping Constant: 2000.000000 (linear)
Dynamic Friction: 0.200000
Static Friction: 0.200000
STRUCTURE RIGHT_TIP
Location: 43.200000 , 214.800000 , 59.400000
Spring Constant: 10000.000000
Damping Constant: 2000.000000 (linear)
Rebound Damping Constant: 2000.000000 (linear)
Dynamic Friction: 0.200000
Static Friction: 0.200000
Propulsion:
(FUEL) tank holds 130.000000 lbs. FUEL
currently at 100.000000% of maximum capacity
Tank location (X, Y, Z): 48.000000, -112.000000, 59.400000
Effective radius: 29.400000 inches
Initial temperature: -9999.000000 Fahrenheit
Priority: 1
(FUEL) tank holds 130.000000 lbs. FUEL
currently at 100.000000% of maximum capacity
Tank location (X, Y, Z): 48.000000, 112.000000, 59.400000
Effective radius: 29.400000 inches
Initial temperature: -9999.000000 Fahrenheit
Priority: 1
1 dimensional table with 25 rows.
0.0000 0.0730
0.1000 0.0730
0.2000 0.0720
0.3000 0.0710
0.4000 0.0690
0.5000 0.0660
0.6000 0.0620
0.7000 0.0550
0.8000 0.0450
0.9000 0.0340
1.0000 0.0240
1.1000 0.0130
1.2000 -0.0060
1.3000 -0.0130
1.4000 -0.0240
1.5000 -0.0340
1.6000 -0.0450
1.7000 -0.0550
1.8000 -0.0620
1.9000 -0.0660
2.0000 -0.0690
2.1000 -0.0710
2.2000 -0.0720
2.3000 -0.0730
5.0000 -0.0730
1 dimensional table with 26 rows.
0.0000 0.0660
0.1000 0.0700
0.2000 0.0700
0.3000 0.0660
0.4000 0.0600
0.5000 0.0530
0.6000 0.0501
0.7000 0.0469
0.8000 0.0426
0.9000 0.0360
1.0000 0.0282
1.1000 0.0191
1.2000 0.0155
1.3000 0.0191
1.4000 0.0282
1.5000 0.0360
1.6000 0.0426
1.7000 0.0469
1.8000 0.0501
1.9000 0.0516
2.0000 0.0525
2.1000 0.0525
2.2000 0.0522
2.3000 0.0511
2.4000 0.0504
5.0000 0.0493
1 dimensional table with 2 rows.
0.8500 1.0000
1.0500 0.8000
1 dimensional table with 3 rows.
0.8500 1.0000
1.0500 1.8000
2.0000 1.4000
Propeller Name: Fixed-Pitch 75-inch Two-Blade Propeller
IXX = 1.6700
Diameter = 6.2500 ft.
Number of Blades = 2
Gear Ratio = 1.0000
Minimum Pitch = 22.0000
Maximum Pitch = 22.0000
Minimum RPM = 0.0000
Maximum RPM = 0.0000
X = -37.7000
Y = 0.0000
Z = 26.6000
Pitch = 0.0000 degrees
Yaw = 0.0000 degrees
Engine Name: IO320
MinManifoldPressure: 10.0000
MaxManifoldPressure: 28.5000
MinMaP (Pa): 33863.8000
MaxMaP (Pa): 96511.8300
Displacement: 320.0000
Bore: 5.1250
Stroke: 4.3750
Cylinders: 4.0000
Cylinders Head Mass: 2.0000
Compression Ratio: 8.5000
MaxHP: 160.0000
Cycles: 4.0000
IdleRPM: 550.0000
MaxRPM: 2700.0000
Throttle Constant: 29.6506
ISFC: 0.3200
Volumetric Efficiency: 0.8500
PeakMeanPistonSpeed_fps: 100.0000
Intake Impedance Factor: 0.1519
Dynamic FMEP Factor: 18400.0000
Static FMEP Factor: 46500.0000
Starter Motor Torque: 64.0000
Starter Motor RPM: 1100.0000
Combustion Efficiency table:
1 dimensional table with 12 rows.
0.0000 0.9800
0.9000 0.9800
1.0000 0.9700
1.0500 0.9500
1.1000 0.9000
1.1500 0.8500
1.2000 0.7900
1.3000 0.7000
1.4000 0.6300
1.5000 0.5700
1.6000 0.5250
2.0000 0.3450
Mixture Efficiency Correlation table:
1 dimensional table with 15 rows.
0.0500 0.0000
0.0514 0.0086
0.0518 0.2155
0.0543 0.4828
0.0584 0.7069
0.0631 0.8362
0.0694 0.9310
0.0779 1.0000
0.0885 1.0000
0.0927 0.9828
0.1012 0.9310
0.1145 0.7241
0.1216 0.4569
0.1244 0.2328
0.1250 0.0000
System: Navigation
Channel Heading
Loading Component "navigation/actual-heading-rad" of type: SENSOR
INPUT: heading-true-rad
Bias: 0.0030
OUTPUT: actual-heading-rad
System: Fuel content in volume
System: Mixture control
Channel Automatic Mixture Control
Loading Component "systems/mixture-cmd-norm" of type: FCS_FUNCTION
1 dimensional table with 2 rows.
0.0000 0.0000
2117.0000 1.0000
OUTPUT: mixture-cmd-norm
OUTPUT: mixture-cmd-norm
Declared properties
guidance/target_wp_latitude_rad (initial value: 0.0000)
guidance/target_wp_longitude_rad (initial value: 0.0000)
guidance/specified-heading-rad (initial value: 0.0000)
guidance/heading-selector-switch (initial value: 0.0000)
System: GNC Utilities
Channel Guidance Waypoint Heading Director
Loading Component "guidance/wp-heading-rad" of type: WAYPOINT_HEADING
Loading Component "guidance/wp-distance" of type: WAYPOINT_DISTANCE
Loading Component "guidance/wp-heading-deg" of type: PURE_GAIN
INPUT: wp-heading-rad
GAIN: constant value 57.300000
OUTPUT: wp-heading-deg
Channel Included Angle to Heading
Loading Component "guidance/selected_target_heading" of type: SWITCH
Switch default value is: wp-heading-rad
Switch takes test 1 value (specified-heading-rad)
if all of the following are true: {
heading-selector-switch eq constant value 1.000000
}
OUTPUT: selected_target_heading
Loading Component "guidance/angle-to-heading-rad" of type: ANGLE
Declared properties
ap/roll-attitude-mode (initial value: 0.0000)
ap/autopilot-roll-on (initial value: 0.0000)
guidance/roll-angle-limit (initial value: 0.5240)
guidance/roll-rate-limit (initial value: 0.1740)
ap/roll-angle-saturation (initial value: 0.0000)
Overriding properties
Overriding value for property guidance/roll-angle-limit
(old value: 0.5240 new value: 0.5230)
Overriding value for property guidance/roll-rate-limit
(old value: 0.1740 new value: 0.1740)
System: Autopilot
Channel Heading Hold
Loading Component "ap/roll-control-autopilot-on" of type: SWITCH
Switch default value is: constant value 0.000000
Switch takes test 1 value (constant value 1.000000)
if all of the following are true: {
autopilot-roll-on ne constant value 0.000000
}
OUTPUT: roll-control-autopilot-on
Loading Component "ap/roll-autopilot-windup-trigger" of type: SWITCH
Switch default value is: constant value 1.000000
Switch takes test 1 value (constant value 1.000000)
if all of the following are true: {
roll-angle-saturation ne constant value 0.000000
}
Switch takes test 2 value (constant value 0.000000)
if all of the following are true: {
roll-control-autopilot-on gt constant value 0.000000
}
OUTPUT: roll-autopilot-windup-trigger
Loading Component "ap/limited-roll-angle-rad" of type: PURE_GAIN
Minimum limit: -roll-angle-limit
Maximum limit: roll-angle-limit
INPUT: angle-to-heading-rad
GAIN: constant value 1.000000
OUTPUT: limited-roll-angle-rad
Loading Component "ap/roll-attitude-selector" of type: SWITCH
Switch default value is: constant value 0.000000
Switch takes test 1 value (limited-roll-angle-rad)
if all of the following are true: {
roll-attitude-mode eq constant value 1.000000
}
OUTPUT: roll-attitude-selector
Loading Component "ap/limited-roll-angle-error" of type: SUMMER
INPUTS:
roll-attitude-selector
-phi-rad
OUTPUT: limited-roll-angle-error
Loading Component "ap/roll-rate-pid-control" of type: PID
Minimum limit: -roll-rate-limit
Maximum limit: roll-rate-limit
INPUT: limited-roll-angle-error
OUTPUT: roll-rate-pid-control
Loading Component "ap/total-limited-roll-rate" of type: PURE_GAIN
INPUT: roll-rate-limit
GAIN: constant value 2.000000
OUTPUT: total-limited-roll-rate
Loading Component "ap/roll-rate-saturation" of type: DEADBAND
INPUT: roll-rate-pid-control
DEADBAND WIDTH: total-limited-roll-rate
GAIN: 1.0000
OUTPUT: roll-rate-saturation
Loading Component "ap/limited-roll-rate-error" of type: SUMMER
INPUTS:
roll-rate-pid-control
-p-aero-rad_sec
OUTPUT: limited-roll-rate-error
Loading Component "ap/roll-command-pid-control" of type: PID
INPUT: limited-roll-rate-error
OUTPUT: roll-command-pid-control
Loading Component "ap/roll-cmd-smoother" of type: LAG_FILTER
INPUT: roll-command-pid-control
C[1]: constant value 100.000000
OUTPUT: roll-cmd-smoother
Loading Component "ap/roll-cmd-norm-output" of type: SWITCH
Switch default value is: constant value 0.000000
Switch takes test 1 value (roll-cmd-smoother)
if all of the following are true: {
roll-control-autopilot-on ne constant value 0.000000
}
OUTPUT: roll-cmd-norm-output
Loading Component "ap/roll-command-selector-steering" of type: SWITCH
Switch default value is: constant value 0.000000
Switch takes test 1 value (roll-cmd-norm-output)
if all of the following are true: {
roll-control-autopilot-on == constant value 1.000000
WOW == constant value 1.000000
}
OUTPUT: steer-cmd-norm
OUTPUT: roll-command-selector-steering
Declared properties
ap/attitude_hold (initial value: 0.0000)
ap/altitude_hold (initial value: 0.0000)
ap/heading_hold (initial value: 0.0000)
ap/altitude_setpoint (initial value: 0.0000)
ap/heading_setpoint (initial value: 0.0000)
ap/aileron_cmd (initial value: 0.0000)
ap/elevator_cmd (initial value: 0.0000)
ap/airspeed_setpoint (initial value: 0.0000)
ap/airspeed_hold (initial value: 0.0000)
ap/throttle-cmd-norm (initial value: 0.0000)
ap/hdg-roll-err-c1 (initial value: 0.5000)
ap/roll-pid-kp (initial value: 50.0000)
ap/roll-pid-ki (initial value: 5.0000)
ap/roll-pid-kd (initial value: 17.0000)
Autopilot: C-172X Autopilot
Channel Roll wing leveler
Loading Component "fcs/attitude/sensor/phi-rad" of type: SENSOR
Frame delay: 240 frames (2.0000 sec)
INPUT: phi-rad
Quantized output (property: attitude/sensor/quantized/phi-rad)
Bits: 12
Min value: -3.1416
Max value: 3.1416
(span: 6.2832, granularity: 0.0015)
Bias: 0.0010
Sensor lag: 0.5000
Noise variance (percent): 0.0500
Random noise is gaussian distributed.
OUTPUT: phi-rad
Loading Component "fcs/wing-leveler-ap-on-off" of type: SWITCH
Switch default value is: constant value -1.000000
Switch takes test 1 value (constant value 0.000000)
if all of the following are true: {
attitude_hold == constant value 1.000000
}
OUTPUT: wing-leveler-ap-on-off
Loading Component "fcs/roll-ap-error-pid" of type: PID
INPUT: phi-rad
OUTPUT: roll-ap-error-pid
Loading Component "fcs/roll-ap-autoswitch" of type: SWITCH
Switch default value is: constant value 0.000000
Switch takes test 1 value (-roll-ap-error-pid)
if all of the following are true: {
attitude_hold == constant value 1.000000
}
OUTPUT: roll-ap-autoswitch
Channel Roll heading hold
Loading Component "fcs/heading-true-degrees" of type: PURE_GAIN
INPUT: heading-true-rad
GAIN: constant value 57.300000
OUTPUT: heading-true-degrees
Loading Component "fcs/heading-error" of type: SUMMER
INPUTS:
-heading-true-degrees
heading_setpoint
OUTPUT: heading-error
Loading Component "fcs/heading-error-bias-switch" of type: SWITCH
Switch default value is: constant value 0.000000
Switch takes test 1 value (constant value 360.000000)
if all of the following are true: {
heading-error lt constant value -180.000000
}
Switch takes test 2 value (constant value -360.000000)
if all of the following are true: {
heading-error gt constant value 180.000000
}
OUTPUT: heading-error-bias-switch
Loading Component "fcs/heading-corrected" of type: SUMMER
Minimum limit: constant value -30.000000
Maximum limit: constant value 30.000000
INPUTS:
heading-error-bias-switch
heading-error
OUTPUT: heading-corrected
Loading Component "fcs/heading-command" of type: PURE_GAIN
INPUT: heading-corrected
GAIN: constant value 0.017450
OUTPUT: heading-command
Loading Component "fcs/heading-roll-error-lag" of type: LAG_FILTER
INPUT: heading-command
C[1] is the value of property: hdg-roll-err-c1
OUTPUT: heading-roll-error-lag
Loading Component "fcs/heading-roll-error" of type: SUMMER
INPUTS:
heading-roll-error-lag
-phi-rad
OUTPUT: heading-roll-error
Loading Component "fcs/heading-roll-error-switch" of type: SWITCH
Switch default value is: constant value 0.000000
Switch takes test 1 value (heading-roll-error)
if all of the following are true: {
heading_hold == constant value 1.000000
}
OUTPUT: heading-roll-error-switch
Loading Component "fcs/heading-pi-controller" of type: PID
INPUT: heading-roll-error-switch
OUTPUT: heading-pi-controller
Loading Component "fcs/roll-command-selector" of type: SWITCH
Switch default value is: constant value 0.000000
Switch takes test 1 value (heading-pi-controller)
if all of the following are true: {
heading_hold == constant value 1.000000
WOW == constant value 0.000000
}
Switch takes test 2 value (roll-ap-autoswitch)
if all of the following are true: {
attitude_hold == constant value 1.000000
WOW == constant value 0.000000
}
OUTPUT: aileron_cmd
OUTPUT: roll-command-selector
Channel Pitch altitude hold
Loading Component "fcs/altitude-error" of type: SUMMER
Minimum limit: constant value -100.000000
Maximum limit: constant value 100.000000
INPUTS:
altitude_setpoint
-h-agl-ft
OUTPUT: altitude-error
Loading Component "fcs/alt-error-lag" of type: LAG_FILTER
INPUT: altitude-error
C[1]: constant value 1.000000
OUTPUT: alt-error-lag
Loading Component "fcs/hdot-command" of type: SCHEDULED_GAIN
1 dimensional table with 13 rows.
0.0000 0.1200
1000.0000 0.1100
2000.0000 0.1000
3000.0000 0.0960
4000.0000 0.0930
5000.0000 0.0860
6000.0000 0.0780
7000.0000 0.0690
8000.0000 0.0610
9000.0000 0.0530
10000.0000 0.0450
11000.0000 0.0370
12000.0000 0.0280
INPUT: alt-error-lag
GAIN: constant value 1.000000
OUTPUT: hdot-command
Scheduled by table:
1 dimensional table with 13 rows.
0.0000 0.1200
1000.0000 0.1100
2000.0000 0.1000
3000.0000 0.0960
4000.0000 0.0930
5000.0000 0.0860
6000.0000 0.0780
7000.0000 0.0690
8000.0000 0.0610
9000.0000 0.0530
10000.0000 0.0450
11000.0000 0.0370
12000.0000 0.0280
Loading Component "fcs/hdot-error" of type: SUMMER
INPUTS:
hdot-command
-h-dot-fps
OUTPUT: hdot-error
Loading Component "fcs/ap-alt-hold-switch" of type: SWITCH
Switch default value is: constant value 0.000000
Switch takes test 1 value (hdot-error)
if all of the following are true: {
altitude_hold == constant value 1.000000
}
OUTPUT: ap-alt-hold-switch
Loading Component "fcs/windup-trigger" of type: DEADBAND
INPUT: elevator-pos-deg
DEADBAND WIDTH: constant value 46.000000
GAIN: 1.0000
OUTPUT: windup-trigger
Loading Component "fcs/altitude-hold-pid" of type: PID
Minimum limit: constant value -1.000000
Maximum limit: constant value 1.000000
INPUT: ap-alt-hold-switch
OUTPUT: altitude-hold-pid
Loading Component "fcs/elevator" of type: PURE_GAIN
INPUT: altitude-hold-pid
GAIN: constant value -1.000000
OUTPUT: elevator_cmd
OUTPUT: elevator
FCS: c172
Channel Pitch
Loading Component "fcs/pitch-trim-sum" of type: SUMMER
Minimum limit: constant value -1.000000
Maximum limit: constant value 1.000000
INPUTS:
elevator_cmd
elevator-cmd-norm
pitch-trim-cmd-norm
OUTPUT: pitch-trim-sum
Loading Component "fcs/elevator-control" of type: AEROSURFACE_SCALE
INPUT: pitch-trim-sum
GAIN: constant value 0.017450
OUTPUT: elevator-control
In/Out Mapping:
Input MIN: -1.0000
Input MAX: 1.0000
Output MIN: -28.0000
Output MAX: 23.0000
Loading Component "fcs/elevator-actuator" of type: ACTUATOR
Minimum limit: constant value -0.340000
Maximum limit: constant value 0.340000
INPUT: elevator-control
OUTPUT: elevator-pos-rad
OUTPUT: elevator-actuator
Bias: 0.0020
Actuator lag: constant value 60.000000
Hysteresis width: 0.0500
Channel Roll
Loading Component "fcs/roll-trim-sum" of type: SUMMER
Minimum limit: constant value -1.000000
Maximum limit: constant value 1.000000
INPUTS:
aileron_cmd
roll-cmd-norm-output
aileron-cmd-norm
roll-trim-cmd-norm
OUTPUT: roll-trim-sum
Loading Component "fcs/left-aileron-control" of type: AEROSURFACE_SCALE
INPUT: roll-trim-sum
GAIN: constant value 0.017450
OUTPUT: left-aileron-control
In/Out Mapping:
Input MIN: -1.0000
Input MAX: 1.0000
Output MIN: -20.0000
Output MAX: 15.0000
Loading Component "fcs/left-aileron-actuator" of type: ACTUATOR
Minimum limit: constant value -0.350000
Maximum limit: constant value 0.260000
INPUT: left-aileron-control
OUTPUT: left-aileron-pos-rad
OUTPUT: left-aileron-actuator
Increasing rate limit: constant value 1.570000
Decreasing rate limit: constant value 1.570000
Loading Component "fcs/right-aileron-control" of type: AEROSURFACE_SCALE
INPUT: -roll-trim-sum
GAIN: constant value 0.017450
OUTPUT: right-aileron-control
In/Out Mapping:
Input MIN: -1.0000
Input MAX: 1.0000
Output MIN: -20.0000
Output MAX: 15.0000
Loading Component "fcs/right-aileron-actuator" of type: ACTUATOR
Minimum limit: constant value -0.350000
Maximum limit: constant value 0.260000
INPUT: right-aileron-control
OUTPUT: right-aileron-pos-rad
OUTPUT: right-aileron-actuator
Increasing rate limit: constant value 1.570000
Decreasing rate limit: constant value 1.570000
Loading Component "fcs/effective-aileron-pos" of type: SUMMER
INPUTS:
left-aileron-pos-rad
-right-aileron-pos-rad
OUTPUT: effective-aileron-pos
Channel Yaw
Loading Component "fcs/yaw-trim-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: yaw-trim-sum
Loading Component "fcs/rudder-control" of type: AEROSURFACE_SCALE
INPUT: yaw-trim-sum
GAIN: constant value 0.017450
OUTPUT: rudder-pos-rad
OUTPUT: rudder-control
In/Out Mapping:
Input MIN: -1.0000
Input MAX: 1.0000
Output MIN: -16.0000
Output MAX: 16.0000
Channel Flaps
Loading Component "fcs/flaps-control" of type: KINEMATIC
INPUT: flap-cmd-norm
DETENTS: 4
0.0000 0.0000
10.0000 2.0000
20.0000 1.0000
30.0000 1.0000
OUTPUT: flap-pos-deg
OUTPUT: flaps-control
Loading Component "fcs/flap-position-normalizer" of type: AEROSURFACE_SCALE
INPUT: flap-pos-deg
GAIN: constant value 1.000000
OUTPUT: flap-pos-norm
OUTPUT: flap-position-normalizer
In/Out Mapping:
Input MIN: 0.0000
Input MAX: 30.0000
Output MIN: 0.0000
Output MAX: 1.0000
Function: aero/angle/right_wing_tip_alpha
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/ground-effect-factor-lift
1 dimensional table with 13 rows.
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
Function: aero/function/ground-effect-factor-drag
Aerodynamics (Lift|Side|Drag axes):
2 dimensional table with 17 rows, 2 columns.
0.0000 1.0000
-0.0900 -0.2200 -0.2200
0.0000 0.2500 0.2500
0.0900 0.7300 0.7300
0.1000 0.8300 0.7800
0.1200 0.9200 0.7900
0.1400 1.0200 0.8100
0.1600 1.0800 0.8200
0.1700 1.1300 0.8300
0.1900 1.1900 0.8500
0.2100 1.2500 0.8600
0.2400 1.3500 0.8800
0.2600 1.4400 0.9000
0.2800 1.4700 0.9200
0.3000 1.4300 0.9500
0.3200 1.3800 0.9900
0.3400 1.3000 1.0500
0.3600 1.1500 1.1500
Function: aero/coefficient/CLwbh
1 dimensional table with 4 rows.
0.0000 0.0000
10.0000 0.2500
20.0000 0.3000
30.0000 0.3500
Function: aero/coefficient/CLDf
Function: aero/coefficient/CLDe
Function: aero/coefficient/CLadot
Function: aero/coefficient/CLq
2 dimensional table with 21 rows, 13 columns.
-10.0000 -5.0000 -4.0000 -3.0000 -2.0000 -1.0000 0.0000 1.0000 2.0000 3.0000 4.0000 5.0000 10.0000
-10.0000 4.5792 4.6831 4.6957 4.7054 4.7125 4.7167 4.7181 4.7167 4.7125 4.7055 4.6957 4.6832 4.5794
-9.0000 4.5886 4.6926 4.7052 4.7150 4.7221 4.7263 4.7277 4.7263 4.7221 4.7151 4.7053 4.6927 4.5887
-8.0000 4.5947 4.6989 4.7115 4.7214 4.7284 4.7326 4.7340 4.7326 4.7284 4.7214 4.7116 4.6990 4.5949
-7.0000 4.5977 4.7019 4.7146 4.7244 4.7314 4.7357 4.7371 4.7357 4.7315 4.7244 4.7146 4.7020 4.5979
-6.0000 4.5975 4.7017 4.7143 4.7241 4.7312 4.7354 4.7368 4.7354 4.7312 4.7242 4.7144 4.7018 4.5976
-5.0000 4.5940 4.6981 4.7107 4.7206 4.7276 4.7318 4.7332 4.7318 4.7276 4.7206 4.7108 4.6982 4.5942
-4.0000 4.5874 4.6913 4.7039 4.7137 4.7207 4.7249 4.7263 4.7249 4.7207 4.7137 4.7039 4.6914 4.5875
-3.0000 4.5775 4.6812 4.6937 4.7035 4.7105 4.7147 4.7161 4.7147 4.7105 4.7036 4.6938 4.6813 4.5777
-2.0000 4.5644 4.6678 4.6803 4.6900 4.6970 4.7012