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JSBSim

读取飞机xml文件:a 1982 Cessna 172P

"C:\jsbsim-master\aircraft\c172p\c172p.xml"

上面是文件位置,下面是读取的结果

     JSBSim Flight Dynamics Model v1.2.0.dev1 Oct  5 2024 21:22:03
            [JSBSim-ML v2.0]

JSBSim startup beginning ...

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  4.7026  4.7012  4.6970  4.6901  4.6803  4.6679  4.5646  
        -1.0000 4.5481  4.6511  4.6636  4.6733  4.6802  4.6844  4.6858  4.6844  4.6803  4.6733  4.6636  4.6512  4.5483  
        0.0000  4.5287  4.6312  4.6436  4.6533  4.6602  4.6644  4.6657  4.6644  4.6602  4.6533  4.6437  4.6313  4.5289  
        1.0000  4.5061  4.6081  4.6204  4.6301  4.6369  4.6411  4.6425  4.6411  4.6370  4.6301  4.6205  4.6082  4.5063  
        2.0000  4.4805  4.5818  4.5941  4.6036  4.6105  4.6146  4.6160  4.6146  4.6105  4.6037  4.5942  4.5819  4.4806  
        3.0000  4.4517  4.5524  4.5646  4.5741  4.5809  4.5850  4.5863  4.5850  4.5809  4.5741  4.5647  4.5525  4.4519  
        4.0000  4.4200  4.5199  4.5320  4.5414  4.5482  4.5522  4.5536  4.5522  4.5482  4.5415  4.5321  4.5200  4.4202  
        5.0000  4.3853  4.4844  4.4964  4.5057  4.5124  4.5164  4.5178  4.5164  4.5124  4.5058  4.4964  4.4845  4.3855  
        6.0000  4.3476  4.4459  4.4578  4.4670  4.4736  4.4776  4.4790  4.4777  4.4737  4.4671  4.4578  4.4460  4.3478  
        7.0000  4.3072  4.4044  4.4162  4.4254  4.4320  4.4359  4.4372  4.4359  4.4320  4.4254  4.4163  4.4045  4.3074  
        8.0000  4.2639  4.3602  4.3718  4.3809  4.3874  4.3913  4.3926  4.3913  4.3874  4.3810  4.3719  4.3603  4.2641  
        9.0000  4.2180  4.3131  4.3247  4.3336  4.3401  4.3439  4.3452  4.3439  4.3401  4.3337  4.3247  4.3132  4.2181  
        10.0000 4.1694  4.2634  4.2748  4.2837  4.2900  4.2938  4.2951  4.2938  4.2900  4.2837  4.2749  4.2635  4.1695  
    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        4.5893  4.6934  4.7060  4.7158  4.7228  4.7270  4.7284  4.7270  4.7228  4.7158  4.7060  4.6934  4.5894
        -9.0000 4.5968  4.7011  4.7137  4.7235  4.7306  4.7348  4.7362  4.7348  4.7306  4.7236  4.7137  4.7011  4.5970  
        -8.0000 4.6012  4.7055  4.7181  4.7280  4.7350  4.7393  4.7407  4.7393  4.7351  4.7280  4.7182  4.7056  4.6013  
        -7.0000 4.6024  4.7067  4.7193  4.7292  4.7362  4.7404  4.7418  4.7404  4.7362  4.7292  4.7194  4.7068  4.6025  
        -6.0000 4.6003  4.7046  4.7172  4.7270  4.7341  4.7383  4.7397  4.7383  4.7341  4.7271  4.7173  4.7047  4.6005  
        -5.0000 4.5951  4.6992  4.7118  4.7216  4.7286  4.7329  4.7343  4.7329  4.7287  4.7217  4.7119  4.6993  4.5952  
        -4.0000 4.5866  4.6905  4.7031  4.7129  4.7199  4.7241  4.7255  4.7241  4.7199  4.7129  4.7032  4.6906  4.5868  
        -3.0000 4.5749  4.6786  4.6911  4.7009  4.7079  4.7121  4.7135  4.7121  4.7079  4.7009  4.6912  4.6786  4.5751  
        -2.0000 4.5601  4.6633  4.6758  4.6856  4.6926  4.6967  4.6981  4.6968  4.6926  4.6856  4.6759  4.6634  4.5603  
        -1.0000 4.5421  4.6449  4.6573  4.6670  4.6740  4.6782  4.6796  4.6782  4.6740  4.6671  4.6574  4.6450  4.5422  
        0.0000  4.5209  4.6232  4.6356  4.6453  4.6522  4.6563  4.6577  4.6564  4.6522  4.6453  4.6357  4.6233  4.5211  
        1.0000  4.4967  4.5984  4.6107  4.6203  4.6272  4.6313  4.6327  4.6313  4.6272  4.6204  4.6108  4.5985  4.4968  
        2.0000  4.4693  4.5704  4.5827  4.5922  4.5990  4.6031  4.6045  4.6031  4.5991  4.5923  4.5827  4.5705  4.4695  
        3.0000  4.4390  4.5394  4.5515  4.5610  4.5677  4.5718  4.5732  4.5718  4.5678  4.5610  4.5516  4.5394  4.4392  
        4.0000  4.4056  4.5052  4.5173  4.5267  4.5334  4.5374  4.5388  4.5375  4.5334  4.5267  4.5174  4.5053  4.4058  
        5.0000  4.3694  4.4681  4.4801  4.4894  4.4961  4.5001  4.5014  4.5001  4.4961  4.4894  4.4802  4.4682  4.3696  
        6.0000  4.3303  4.4281  4.4399  4.4491  4.4558  4.4597  4.4610  4.4597  4.4558  4.4492  4.4400  4.4282  4.3305  
        7.0000  4.2883  4.3852  4.3969  4.4060  4.4126  4.4165  4.4178  4.4165  4.4126  4.4061  4.3970  4.3853  4.2885  
        8.0000  4.2437  4.3395  4.3511  4.3601  4.3666  4.3705  4.3718  4.3705  4.3666  4.3602  4.3511  4.3396  4.2439  
        9.0000  4.1964  4.2911  4.3025  4.3114  4.3178  4.3217  4.3230  4.3217  4.3179  4.3115  4.3026  4.2912  4.1966  
        10.0000 4.1465  4.2400  4.2513  4.2601  4.2665  4.2702  4.2715  4.2703  4.2665  4.2602  4.2514  4.2401  4.1467  
    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        4.6003  4.7047  4.7173  4.7272  4.7342  4.7384  4.7399  4.7385  4.7342  4.7272  4.7174  4.7048  4.6005
        -9.0000 4.6043  4.7087  4.7213  4.7312  4.7382  4.7425  4.7439  4.7425  4.7383  4.7312  4.7214  4.7088  4.6044  
        -8.0000 4.6050  4.7095  4.7221  4.7319  4.7390  4.7432  4.7446  4.7432  4.7390  4.7320  4.7222  4.7095  4.6052  
        -7.0000 4.6026  4.7069  4.7196  4.7294  4.7364  4.7407  4.7421  4.7407  4.7365  4.7295  4.7196  4.7070  4.6028  
        -6.0000 4.5970  4.7011  4.7138  4.7236  4.7306  4.7348  4.7363  4.7349  4.7307  4.7236  4.7138  4.7012  4.5971  
        -5.0000 4.5881  4.6921  4.7047  4.7145  4.7215  4.7257  4.7271  4.7257  4.7215  4.7145  4.7047  4.6922  4.5883  
        -4.0000 4.5761  4.6798  4.6923  4.7021  4.7091  4.7133  4.7147  4.7133  4.7091  4.7022  4.6924  4.6799  4.5763  
        -3.0000 4.5610  4.6642  4.6767  4.6865  4.6935  4.6977  4.6991  4.6977  4.6935  4.6865  4.6768  4.6643  4.5611  
        -2.0000 4.5426  4.6455  4.6579  4.6676  4.6746  4.6787  4.6801  4.6788  4.6746  4.6677  4.6580  4.6456  4.5428  
        -1.0000 4.5212  4.6235  4.6359  4.6456  4.6525  4.6566  4.6580  4.6567  4.6525  4.6456  4.6360  4.6236  4.5214  
        0.0000  4.4967  4.5984  4.6108  4.6204  4.6272  4.6313  4.6327  4.6314  4.6273  4.6204  4.6108  4.5985  4.4969  
        1.0000  4.4691  4.5702  4.5825  4.5920  4.5988  4.6029  4.6043  4.6029  4.5989  4.5920  4.5825  4.5703  4.4693  
        2.0000  4.4386  4.5389  4.5511  4.5606  4.5673  4.5714  4.5728  4.5714  4.5674  4.5606  4.5512  4.5390  4.4387  
        3.0000  4.4051  4.5046  4.5167  4.5261  4.5328  4.5368  4.5382  4.5369  4.5328  4.5261  4.5168  4.5047  4.4052  
        4.0000  4.3687  4.4674  4.4793  4.4886  4.4953  4.4993  4.5007  4.4993  4.4953  4.4887  4.4794  4.4675  4.3688  
        5.0000  4.3294  4.4272  4.4391  4.4483  4.4549  4.4589  4.4602  4.4589  4.4549  4.4483  4.4391  4.4273  4.3296  
        6.0000  4.2874  4.3842  4.3959  4.4051  4.4116  4.4155  4.4169  4.4156  4.4117  4.4051  4.3960  4.3843  4.2876  
        7.0000  4.2427  4.3385  4.3501  4.3591  4.3656  4.3695  4.3708  4.3695  4.3656  4.3592  4.3501  4.3386  4.2429  
        8.0000  4.1954  4.2900  4.3015  4.3104  4.3168  4.3207  4.3219  4.3207  4.3169  4.3105  4.3016  4.2901  4.1956  
        9.0000  4.1455  4.2390  4.2503  4.2591  4.2655  4.2692  4.2705  4.2693  4.2655  4.2592  4.2504  4.2391  4.1457  
        10.0000 4.0932  4.1854  4.1966  4.2053  4.2116  4.2153  4.2165  4.2153  4.2116  4.2054  4.1967  4.1855  4.0934  
    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        4.5994  4.7037  4.7163  4.7261  4.7332  4.7374  4.7388  4.7374  4.7332  4.7262  4.7164  4.7038  4.5995
        -9.0000 4.5997  4.7040  4.7166  4.7265  4.7335  4.7377  4.7391  4.7377  4.7335  4.7265  4.7167  4.7041  4.5998  
        -8.0000 4.5968  4.7011  4.7137  4.7235  4.7305  4.7348  4.7362  4.7348  4.7306  4.7236  4.7137  4.7011  4.5970  
        -7.0000 4.5908  4.6949  4.7075  4.7173  4.7243  4.7285  4.7299  4.7285  4.7243  4.7173  4.7075  4.6949  4.5910  
        -6.0000 4.5816  4.6854  4.6980  4.7078  4.7148  4.7190  4.7204  4.7190  4.7148  4.7078  4.6981  4.6855  4.5818  
        -5.0000 4.5693  4.6728  4.6853  4.6951  4.7021  4.7063  4.7077  4.7063  4.7021  4.6951  4.6854  4.6729  4.5694  
        -4.0000 4.5537  4.6569  4.6694  4.6791  4.6861  4.6902  4.6917  4.6903  4.6861  4.6792  4.6694  4.6570  4.5539  
        -3.0000 4.5351  4.6378  4.6502  4.6599  4.6669  4.6710  4.6724  4.6710  4.6669  4.6600  4.6503  4.6379  4.5353  
        -2.0000 4.5134  4.6156  4.6280  4.6376  4.6445  4.6486  4.6500  4.6486  4.6445  4.6376  4.6280  4.6157  4.5136  
        -1.0000 4.4886  4.5902  4.6025  4.6121  4.6190  4.6231  4.6245  4.6231  4.6190  4.6122  4.6026  4.5903  4.4888  
        0.0000  4.4609  4.5618  4.5740  4.5835  4.5903  4.5944  4.5958  4.5944  4.5904  4.5836  4.5741  4.5619  4.4610  
        1.0000  4.4301  4.5303  4.5424  4.5519  4.5586  4.5627  4.5641  4.5627  4.5587  4.5519  4.5425  4.5304  4.4303  
        2.0000  4.3964  4.4958  4.5079  4.5172  4.5239  4.5280  4.5293  4.5280  4.5240  4.5173  4.5079  4.4959  4.3966  
        3.0000  4.3599  4.4584  4.4704  4.4797  4.4863  4.4903  4.4916  4.4903  4.4863  4.4797  4.4704  4.4585  4.3601  
        4.0000  4.3206  4.4182  4.4300  4.4392  4.4458  4.4497  4.4511  4.4498  4.4458  4.4392  4.4301  4.4183  4.3207  
        5.0000  4.2785  4.3751  4.3868  4.3959  4.4024  4.4064  4.4077  4.4064  4.4025  4.3960  4.3869  4.3752  4.2787  
        6.0000  4.2338  4.3293  4.3409  4.3499  4.3564  4.3602  4.3615  4.3603  4.3564  4.3500  4.3410  4.3294  4.2339  
        7.0000  4.1864  4.2809  4.2923  4.3012  4.3076  4.3114  4.3127  4.3115  4.3077  4.3013  4.2924  4.2810  4.1866  
        8.0000  4.1366  4.2299  4.2412  4.2500  4.2563  4.2601  4.2613  4.2601  4.2563  4.2501  4.2413  4.2300  4.1368  
        9.0000  4.0844  4.1764  4.1876  4.1963  4.2025  4.2062  4.2075  4.2062  4.2025  4.1963  4.1876  4.1765  4.0845  
        10.0000 4.0298  4.1206  4.1315  4.1401  4.1462  4.1499  4.1512  4.1499  4.1463  4.1402  4.1316  4.1207  4.0299  
    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        4.5863  4.6903  4.7029  4.7127  4.7197  4.7240  4.7254  4.7240  4.7198  4.7128  4.7030  4.6904  4.5864
        -9.0000 4.5830  4.6869  4.6995  4.7093  4.7163  4.7205  4.7220  4.7206  4.7164  4.7094  4.6996  4.6870  4.5832  
        -8.0000 4.5766  4.6803  4.6929  4.7027  4.7097  4.7139  4.7153  4.7139  4.7097  4.7027  4.6929  4.6804  4.5767  
        -7.0000 4.5670  4.6705  4.6830  4.6928  4.6998  4.7040  4.7054  4.7040  4.6998  4.6928  4.6831  4.6706  4.5671  
        -6.0000 4.5543  4.6574  4.6699  4.6797  4.6866  4.6908  4.6922  4.6908  4.6867  4.6797  4.6700  4.6575  4.5544  
        -5.0000 4.5384  4.6412  4.6537  4.6634  4.6703  4.6745  4.6759  4.6745  4.6703  4.6634  4.6537  4.6413  4.5386  
        -4.0000 4.5195  4.6218  4.6342  4.6439  4.6508  4.6549  4.6563  4.6549  4.6508  4.6439  4.6343  4.6219  4.5196  
        -3.0000 4.4975  4.5993  4.6116  4.6212  4.6281  4.6322  4.6336  4.6322  4.6281  4.6213  4.6117  4.5994  4.4976  
        -2.0000 4.4724  4.5736  4.5859  4.5954  4.6023  4.6064  4.6078  4.6064  4.6023  4.5955  4.5860  4.5737  4.4726  
        -1.0000 4.4444  4.5450  4.5571  4.5666  4.5734  4.5775  4.5788  4.5775  4.5734  4.5667  4.5572  4.5450  4.4446  
        0.0000  4.4135  4.5133  4.5254  4.5348  4.5415  4.5456  4.5469  4.5456  4.5415  4.5348  4.5254  4.5134  4.4136  
        1.0000  4.3796  4.4786  4.4906  4.5000  4.5066  4.5107  4.5120  4.5107  4.5067  4.5000  4.4907  4.4787  4.3798  
        2.0000  4.3429  4.4411  4.4530  4.4622  4.4689  4.4728  4.4742  4.4729  4.4689  4.4623  4.4530  4.4412  4.3431  
        3.0000  4.3035  4.4007  4.4125  4.4217  4.4282  4.4322  4.4335  4.4322  4.4283  4.4217  4.4126  4.4008  4.3037  
        4.0000  4.2614  4.3576  4.3693  4.3783  4.3848  4.3887  4.3900  4.3887  4.3849  4.3784  4.3693  4.3577  4.2616  
        5.0000  4.2166  4.3118  4.3233  4.3323  4.3387  4.3426  4.3439  4.3426  4.3388  4.3324  4.3234  4.3119  4.2168  
        6.0000  4.1693  4.2634  4.2748  4.2836  4.2900  4.2938  4.2951  4.2938  4.2900  4.2837  4.2748  4.2635  4.1695  
        7.0000  4.1195  4.2124  4.2237  4.2324  4.2387  4.2425  4.2437  4.2425  4.2388  4.2325  4.2238  4.2125  4.1197  
        8.0000  4.0674  4.1590  4.1701  4.1788  4.1850  4.1887  4.1899  4.1887  4.1850  4.1789  4.1702  4.1591  4.0675  
        9.0000  4.0129  4.1033  4.1143  4.1228  4.1289  4.1326  4.1338  4.1326  4.1289  4.1228  4.1143  4.1034  4.0131  
        10.0000 3.9562  4.0453  4.0561  4.0645  4.0705  4.0741  4.0754  4.0742  4.0706  4.0646  4.0562  4.0454  3.9564  
    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        4.5612  4.6646  4.6771  4.6869  4.6939  4.6981  4.6995  4.6981  4.6939  4.6869  4.6772  4.6647  4.5613
        -9.0000 4.5543  4.6575  4.6700  4.6798  4.6867  4.6909  4.6923  4.6909  4.6868  4.6798  4.6701  4.6576  4.5544  
        -8.0000 4.5443  4.6473  4.6597  4.6694  4.6764  4.6806  4.6820  4.6806  4.6764  4.6695  4.6598  4.6473  4.5444  
        -7.0000 4.5311  4.6338  4.6462  4.6559  4.6628  4.6670  4.6684  4.6670  4.6629  4.6560  4.6463  4.6339  4.5313  
        -6.0000 4.5149  4.6172  4.6296  4.6392  4.6461  4.6503  4.6516  4.6503  4.6461  4.6393  4.6296  4.6173  4.5151  
        -5.0000 4.4956  4.5974  4.6097  4.6193  4.6262  4.6303  4.6317  4.6304  4.6262  4.6194  4.6098  4.5975  4.4958  
        -4.0000 4.4733  4.5745  4.5868  4.5964  4.6032  4.6073  4.6087  4.6073  4.6032  4.5964  4.5869  4.5746  4.4734  
        -3.0000 4.4480  4.5486  4.5608  4.5703  4.5771  4.5812  4.5825  4.5812  4.5771  4.5703  4.5609  4.5487  4.4481  
        -2.0000 4.4197  4.5197  4.5318  4.5412  4.5480  4.5520  4.5534  4.5520  4.5480  4.5413  4.5318  4.5198  4.4198  
        -1.0000 4.3885  4.4877  4.4998  4.5091  4.5158  4.5198  4.5212  4.5199  4.5159  4.5092  4.4998  4.4878  4.3887  
        0.0000  4.3545  4.4529  4.4648  4.4741  4.4808  4.4848  4.4861  4.4848  4.4808  4.4742  4.4649  4.4530  4.3546  
        1.0000  4.3176  4.4152  4.4270  4.4362  4.4428  4.4468  4.4481  4.4468  4.4429  4.4363  4.4271  4.4153  4.3178  
        2.0000  4.2781  4.3747  4.3864  4.3956  4.4021  4.4060  4.4073  4.4060  4.4021  4.3956  4.3865  4.3748  4.2783  
        3.0000  4.2359  4.3315  4.3431  4.3521  4.3586  4.3625  4.3638  4.3625  4.3586  4.3522  4.3432  4.3316  4.2361  
        4.0000  4.1911  4.2857  4.2971  4.3061  4.3124  4.3163  4.3176  4.3163  4.3125  4.3061  4.2972  4.2858  4.1913  
        5.0000  4.1438  4.2373  4.2486  4.2574  4.2637  4.2675  4.2688  4.2675  4.2638  4.2575  4.2487  4.2374  4.1440  
        6.0000  4.0941  4.1864  4.1976  4.2063  4.2125  4.2162  4.2175  4.2163  4.2125  4.2063  4.1976  4.1865  4.0942  
        7.0000  4.0420  4.1331  4.1441  4.1527  4.1589  4.1626  4.1638  4.1626  4.1589  4.1528  4.1442  4.1332  4.0422  
        8.0000  3.9877  4.0775  4.0884  4.0968  4.1029  4.1065  4.1078  4.1066  4.1029  4.0969  4.0884  4.0776  3.9878  
        9.0000  3.9312  4.0197  4.0304  4.0387  4.0447  4.0483  4.0495  4.0483  4.0448  4.0388  4.0305  4.0198  3.9314  
        10.0000 3.8726  3.9598  3.9703  3.9785  3.9844  3.9880  3.9891  3.9880  3.9845  3.9786  3.9704  3.9599  3.8728  
    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        4.5240  4.6266  4.6390  4.6487  4.6556  4.6597  4.6611  4.6597  4.6556  4.6487  4.6390  4.6266  4.5241
        -9.0000 4.5135  4.6158  4.6282  4.6378  4.6447  4.6489  4.6503  4.6489  4.6448  4.6379  4.6282  4.6159  4.5136  
        -8.0000 4.4999  4.6019  4.6142  4.6238  4.6307  4.6348  4.6362  4.6349  4.6307  4.6239  4.6143  4.6019  4.5000  
        -7.0000 4.4832  4.5848  4.5971  4.6067  4.6135  4.6176  4.6190  4.6177  4.6136  4.6067  4.5972  4.5849  4.4834  
        -6.0000 4.4635  4.5646  4.5769  4.5864  4.5932  4.5973  4.5987  4.5973  4.5932  4.5864  4.5769  4.5647  4.4637  
        -5.0000 4.4408  4.5414  4.5536  4.5630  4.5698  4.5739  4.5753  4.5739  4.5699  4.5631  4.5536  4.5415  4.4410  
        -4.0000 4.4152  4.5151  4.5272  4.5366  4.5434  4.5474  4.5488  4.5474  4.5434  4.5367  4.5273  4.5152  4.4153  
        -3.0000 4.3866  4.4858  4.4979  4.5072  4.5139  4.5179  4.5193  4.5180  4.5139  4.5073  4.4979  4.4859  4.3868  
        -2.0000 4.3552  4.4536  4.4656  4.4749  4.4815  4.4855  4.4868  4.4855  4.4815  4.4749  4.4656  4.4537  4.3553  
        -1.0000 4.3209  4.4186  4.4304  4.4396  4.4462  4.4502  4.4515  4.4502  4.4462  4.4397  4.4305  4.4187  4.3211  
        0.0000  4.2839  4.3807  4.3924  4.4015  4.4081  4.4120  4.4133  4.4120  4.4081  4.4016  4.3925  4.3808  4.2841  
        1.0000  4.2442  4.3401  4.3517  4.3607  4.3672  4.3711  4.3724  4.3711  4.3672  4.3608  4.3517  4.3402  4.2444  
        2.0000  4.2019  4.2968  4.3082  4.3172  4.3236  4.3274  4.3287  4.3275  4.3236  4.3172  4.3083  4.2968  4.2021  
        3.0000  4.1570  4.2508  4.2622  4.2711  4.2774  4.2812  4.2825  4.2812  4.2774  4.2711  4.2623  4.2509  4.1572  
        4.0000  4.1097  4.2024  4.2136  4.2224  4.2286  4.2324  4.2337  4.2324  4.2287  4.2224  4.2137  4.2025  4.1099  
        5.0000  4.0600  4.1515  4.1626  4.1713  4.1774  4.1812  4.1824  4.1812  4.1775  4.1713  4.1627  4.1516  4.0602  
        6.0000  4.0080  4.0983  4.1093  4.1178  4.1239  4.1275  4.1288  4.1276  4.1239  4.1178  4.1093  4.0984  4.0082  
        7.0000  3.9538  4.0429  4.0536  4.0620  4.0680  4.0717  4.0729  4.0717  4.0681  4.0621  4.0537  4.0429  3.9540  
        8.0000  3.8975  3.9852  3.9958  4.0041  4.0100  4.0136  4.0148  4.0136  4.0101  4.0042  3.9959  3.9853  3.8977  
        9.0000  3.8392  3.9255  3.9360  3.9441  3.9500  3.9535  3.9546  3.9535  3.9500  3.9442  3.9361  3.9256  3.8393  
        10.0000 3.7789  3.8639  3.8741  3.8822  3.8879  3.8913  3.8925  3.8914  3.8879  3.8822  3.8742  3.8640  3.7791  
    3 dimensional table with 7 breakpoints, 7 tables.
        -5.0000
    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  4.7026  4.7012  4.6970  4.6901  4.6803  4.6679  4.5646  
        -1.0000 4.5481  4.6511  4.6636  4.6733  4.6802  4.6844  4.6858  4.6844  4.6803  4.6733  4.6636  4.6512  4.5483  
        0.0000  4.5287  4.6312  4.6436  4.6533  4.6602  4.6644  4.6657  4.6644  4.6602  4.6533  4.6437  4.6313  4.5289  
        1.0000  4.5061  4.6081  4.6204  4.6301  4.6369  4.6411  4.6425  4.6411  4.6370  4.6301  4.6205  4.6082  4.5063  
        2.0000  4.4805  4.5818  4.5941  4.6036  4.6105  4.6146  4.6160  4.6146  4.6105  4.6037  4.5942  4.5819  4.4806  
        3.0000  4.4517  4.5524  4.5646  4.5741  4.5809  4.5850  4.5863  4.5850  4.5809  4.5741  4.5647  4.5525  4.4519  
        4.0000  4.4200  4.5199  4.5320  4.5414  4.5482  4.5522  4.5536  4.5522  4.5482  4.5415  4.5321  4.5200  4.4202  
        5.0000  4.3853  4.4844  4.4964  4.5057  4.5124  4.5164  4.5178  4.5164  4.5124  4.5058  4.4964  4.4845  4.3855  
        6.0000  4.3476  4.4459  4.4578  4.4670  4.4736  4.4776  4.4790  4.4777  4.4737  4.4671  4.4578  4.4460  4.3478  
        7.0000  4.3072  4.4044  4.4162  4.4254  4.4320  4.4359  4.4372  4.4359  4.4320  4.4254  4.4163  4.4045  4.3074  
        8.0000  4.2639  4.3602  4.3718  4.3809  4.3874  4.3913  4.3926  4.3913  4.3874  4.3810  4.3719  4.3603  4.2641  
        9.0000  4.2180  4.3131  4.3247  4.3336  4.3401  4.3439  4.3452  4.3439  4.3401  4.3337  4.3247  4.3132  4.2181  
        10.0000 4.1694  4.2634  4.2748  4.2837  4.2900  4.2938  4.2951  4.2938  4.2900  4.2837  4.2749  4.2635  4.1695  

        0.0000
    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        4.5893  4.6934  4.7060  4.7158  4.7228  4.7270  4.7284  4.7270  4.7228  4.7158  4.7060  4.6934  4.5894
        -9.0000 4.5968  4.7011  4.7137  4.7235  4.7306  4.7348  4.7362  4.7348  4.7306  4.7236  4.7137  4.7011  4.5970  
        -8.0000 4.6012  4.7055  4.7181  4.7280  4.7350  4.7393  4.7407  4.7393  4.7351  4.7280  4.7182  4.7056  4.6013  
        -7.0000 4.6024  4.7067  4.7193  4.7292  4.7362  4.7404  4.7418  4.7404  4.7362  4.7292  4.7194  4.7068  4.6025  
        -6.0000 4.6003  4.7046  4.7172  4.7270  4.7341  4.7383  4.7397  4.7383  4.7341  4.7271  4.7173  4.7047  4.6005  
        -5.0000 4.5951  4.6992  4.7118  4.7216  4.7286  4.7329  4.7343  4.7329  4.7287  4.7217  4.7119  4.6993  4.5952  
        -4.0000 4.5866  4.6905  4.7031  4.7129  4.7199  4.7241  4.7255  4.7241  4.7199  4.7129  4.7032  4.6906  4.5868  
        -3.0000 4.5749  4.6786  4.6911  4.7009  4.7079  4.7121  4.7135  4.7121  4.7079  4.7009  4.6912  4.6786  4.5751  
        -2.0000 4.5601  4.6633  4.6758  4.6856  4.6926  4.6967  4.6981  4.6968  4.6926  4.6856  4.6759  4.6634  4.5603  
        -1.0000 4.5421  4.6449  4.6573  4.6670  4.6740  4.6782  4.6796  4.6782  4.6740  4.6671  4.6574  4.6450  4.5422  
        0.0000  4.5209  4.6232  4.6356  4.6453  4.6522  4.6563  4.6577  4.6564  4.6522  4.6453  4.6357  4.6233  4.5211  
        1.0000  4.4967  4.5984  4.6107  4.6203  4.6272  4.6313  4.6327  4.6313  4.6272  4.6204  4.6108  4.5985  4.4968  
        2.0000  4.4693  4.5704  4.5827  4.5922  4.5990  4.6031  4.6045  4.6031  4.5991  4.5923  4.5827  4.5705  4.4695  
        3.0000  4.4390  4.5394  4.5515  4.5610  4.5677  4.5718  4.5732  4.5718  4.5678  4.5610  4.5516  4.5394  4.4392  
        4.0000  4.4056  4.5052  4.5173  4.5267  4.5334  4.5374  4.5388  4.5375  4.5334  4.5267  4.5174  4.5053  4.4058  
        5.0000  4.3694  4.4681  4.4801  4.4894  4.4961  4.5001  4.5014  4.5001  4.4961  4.4894  4.4802  4.4682  4.3696  
        6.0000  4.3303  4.4281  4.4399  4.4491  4.4558  4.4597  4.4610  4.4597  4.4558  4.4492  4.4400  4.4282  4.3305  
        7.0000  4.2883  4.3852  4.3969  4.4060  4.4126  4.4165  4.4178  4.4165  4.4126  4.4061  4.3970  4.3853  4.2885  
        8.0000  4.2437  4.3395  4.3511  4.3601  4.3666  4.3705  4.3718  4.3705  4.3666  4.3602  4.3511  4.3396  4.2439  
        9.0000  4.1964  4.2911  4.3025  4.3114  4.3178  4.3217  4.3230  4.3217  4.3179  4.3115  4.3026  4.2912  4.1966  
        10.0000 4.1465  4.2400  4.2513  4.2601  4.2665  4.2702  4.2715  4.2703  4.2665  4.2602  4.2514  4.2401  4.1467  

        10.0000
    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        4.6003  4.7047  4.7173  4.7272  4.7342  4.7384  4.7399  4.7385  4.7342  4.7272  4.7174  4.7048  4.6005
        -9.0000 4.6043  4.7087  4.7213  4.7312  4.7382  4.7425  4.7439  4.7425  4.7383  4.7312  4.7214  4.7088  4.6044  
        -8.0000 4.6050  4.7095  4.7221  4.7319  4.7390  4.7432  4.7446  4.7432  4.7390  4.7320  4.7222  4.7095  4.6052  
        -7.0000 4.6026  4.7069  4.7196  4.7294  4.7364  4.7407  4.7421  4.7407  4.7365  4.7295  4.7196  4.7070  4.6028  
        -6.0000 4.5970  4.7011  4.7138  4.7236  4.7306  4.7348  4.7363  4.7349  4.7307  4.7236  4.7138  4.7012  4.5971  
        -5.0000 4.5881  4.6921  4.7047  4.7145  4.7215  4.7257  4.7271  4.7257  4.7215  4.7145  4.7047  4.6922  4.5883  
        -4.0000 4.5761  4.6798  4.6923  4.7021  4.7091  4.7133  4.7147  4.7133  4.7091  4.7022  4.6924  4.6799  4.5763  
        -3.0000 4.5610  4.6642  4.6767  4.6865  4.6935  4.6977  4.6991  4.6977  4.6935  4.6865  4.6768  4.6643  4.5611  
        -2.0000 4.5426  4.6455  4.6579  4.6676  4.6746  4.6787  4.6801  4.6788  4.6746  4.6677  4.6580  4.6456  4.5428  
        -1.0000 4.5212  4.6235  4.6359  4.6456  4.6525  4.6566  4.6580  4.6567  4.6525  4.6456  4.6360  4.6236  4.5214  
        0.0000  4.4967  4.5984  4.6108  4.6204  4.6272  4.6313  4.6327  4.6314  4.6273  4.6204  4.6108  4.5985  4.4969  
        1.0000  4.4691  4.5702  4.5825  4.5920  4.5988  4.6029  4.6043  4.6029  4.5989  4.5920  4.5825  4.5703  4.4693  
        2.0000  4.4386  4.5389  4.5511  4.5606  4.5673  4.5714  4.5728  4.5714  4.5674  4.5606  4.5512  4.5390  4.4387  
        3.0000  4.4051  4.5046  4.5167  4.5261  4.5328  4.5368  4.5382  4.5369  4.5328  4.5261  4.5168  4.5047  4.4052  
        4.0000  4.3687  4.4674  4.4793  4.4886  4.4953  4.4993  4.5007  4.4993  4.4953  4.4887  4.4794  4.4675  4.3688  
        5.0000  4.3294  4.4272  4.4391  4.4483  4.4549  4.4589  4.4602  4.4589  4.4549  4.4483  4.4391  4.4273  4.3296  
        6.0000  4.2874  4.3842  4.3959  4.4051  4.4116  4.4155  4.4169  4.4156  4.4117  4.4051  4.3960  4.3843  4.2876  
        7.0000  4.2427  4.3385  4.3501  4.3591  4.3656  4.3695  4.3708  4.3695  4.3656  4.3592  4.3501  4.3386  4.2429  
        8.0000  4.1954  4.2900  4.3015  4.3104  4.3168  4.3207  4.3219  4.3207  4.3169  4.3105  4.3016  4.2901  4.1956  
        9.0000  4.1455  4.2390  4.2503  4.2591  4.2655  4.2692  4.2705  4.2693  4.2655  4.2592  4.2504  4.2391  4.1457  
        10.0000 4.0932  4.1854  4.1966  4.2053  4.2116  4.2153  4.2165  4.2153  4.2116  4.2054  4.1967  4.1855  4.0934  

        20.0000
    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        4.5994  4.7037  4.7163  4.7261  4.7332  4.7374  4.7388  4.7374  4.7332  4.7262  4.7164  4.7038  4.5995
        -9.0000 4.5997  4.7040  4.7166  4.7265  4.7335  4.7377  4.7391  4.7377  4.7335  4.7265  4.7167  4.7041  4.5998  
        -8.0000 4.5968  4.7011  4.7137  4.7235  4.7305  4.7348  4.7362  4.7348  4.7306  4.7236  4.7137  4.7011  4.5970  
        -7.0000 4.5908  4.6949  4.7075  4.7173  4.7243  4.7285  4.7299  4.7285  4.7243  4.7173  4.7075  4.6949  4.5910  
        -6.0000 4.5816  4.6854  4.6980  4.7078  4.7148  4.7190  4.7204  4.7190  4.7148  4.7078  4.6981  4.6855  4.5818  
        -5.0000 4.5693  4.6728  4.6853  4.6951  4.7021  4.7063  4.7077  4.7063  4.7021  4.6951  4.6854  4.6729  4.5694  
        -4.0000 4.5537  4.6569  4.6694  4.6791  4.6861  4.6902  4.6917  4.6903  4.6861  4.6792  4.6694  4.6570  4.5539  
        -3.0000 4.5351  4.6378  4.6502  4.6599  4.6669  4.6710  4.6724  4.6710  4.6669  4.6600  4.6503  4.6379  4.5353  
        -2.0000 4.5134  4.6156  4.6280  4.6376  4.6445  4.6486  4.6500  4.6486  4.6445  4.6376  4.6280  4.6157  4.5136  
        -1.0000 4.4886  4.5902  4.6025  4.6121  4.6190  4.6231  4.6245  4.6231  4.6190  4.6122  4.6026  4.5903  4.4888  
        0.0000  4.4609  4.5618  4.5740  4.5835  4.5903  4.5944  4.5958  4.5944  4.5904  4.5836  4.5741  4.5619  4.4610  
        1.0000  4.4301  4.5303  4.5424  4.5519  4.5586  4.5627  4.5641  4.5627  4.5587  4.5519  4.5425  4.5304  4.4303  
        2.0000  4.3964  4.4958  4.5079  4.5172  4.5239  4.5280  4.5293  4.5280  4.5240  4.5173  4.5079  4.4959  4.3966  
        3.0000  4.3599  4.4584  4.4704  4.4797  4.4863  4.4903  4.4916  4.4903  4.4863  4.4797  4.4704  4.4585  4.3601  
        4.0000  4.3206  4.4182  4.4300  4.4392  4.4458  4.4497  4.4511  4.4498  4.4458  4.4392  4.4301  4.4183  4.3207  
        5.0000  4.2785  4.3751  4.3868  4.3959  4.4024  4.4064  4.4077  4.4064  4.4025  4.3960  4.3869  4.3752  4.2787  
        6.0000  4.2338  4.3293  4.3409  4.3499  4.3564  4.3602  4.3615  4.3603  4.3564  4.3500  4.3410  4.3294  4.2339  
        7.0000  4.1864  4.2809  4.2923  4.3012  4.3076  4.3114  4.3127  4.3115  4.3077  4.3013  4.2924  4.2810  4.1866  
        8.0000  4.1366  4.2299  4.2412  4.2500  4.2563  4.2601  4.2613  4.2601  4.2563  4.2501  4.2413  4.2300  4.1368  
        9.0000  4.0844  4.1764  4.1876  4.1963  4.2025  4.2062  4.2075  4.2062  4.2025  4.1963  4.1876  4.1765  4.0845  
        10.0000 4.0298  4.1206  4.1315  4.1401  4.1462  4.1499  4.1512  4.1499  4.1463  4.1402  4.1316  4.1207  4.0299  

        30.0000
    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        4.5863  4.6903  4.7029  4.7127  4.7197  4.7240  4.7254  4.7240  4.7198  4.7128  4.7030  4.6904  4.5864
        -9.0000 4.5830  4.6869  4.6995  4.7093  4.7163  4.7205  4.7220  4.7206  4.7164  4.7094  4.6996  4.6870  4.5832  
        -8.0000 4.5766  4.6803  4.6929  4.7027  4.7097  4.7139  4.7153  4.7139  4.7097  4.7027  4.6929  4.6804  4.5767  
        -7.0000 4.5670  4.6705  4.6830  4.6928  4.6998  4.7040  4.7054  4.7040  4.6998  4.6928  4.6831  4.6706  4.5671  
        -6.0000 4.5543  4.6574  4.6699  4.6797  4.6866  4.6908  4.6922  4.6908  4.6867  4.6797  4.6700  4.6575  4.5544  
        -5.0000 4.5384  4.6412  4.6537  4.6634  4.6703  4.6745  4.6759  4.6745  4.6703  4.6634  4.6537  4.6413  4.5386  
        -4.0000 4.5195  4.6218  4.6342  4.6439  4.6508  4.6549  4.6563  4.6549  4.6508  4.6439  4.6343  4.6219  4.5196  
        -3.0000 4.4975  4.5993  4.6116  4.6212  4.6281  4.6322  4.6336  4.6322  4.6281  4.6213  4.6117  4.5994  4.4976  
        -2.0000 4.4724  4.5736  4.5859  4.5954  4.6023  4.6064  4.6078  4.6064  4.6023  4.5955  4.5860  4.5737  4.4726  
        -1.0000 4.4444  4.5450  4.5571  4.5666  4.5734  4.5775  4.5788  4.5775  4.5734  4.5667  4.5572  4.5450  4.4446  
        0.0000  4.4135  4.5133  4.5254  4.5348  4.5415  4.5456  4.5469  4.5456  4.5415  4.5348  4.5254  4.5134  4.4136  
        1.0000  4.3796  4.4786  4.4906  4.5000  4.5066  4.5107  4.5120  4.5107  4.5067  4.5000  4.4907  4.4787  4.3798  
        2.0000  4.3429  4.4411  4.4530  4.4622  4.4689  4.4728  4.4742  4.4729  4.4689  4.4623  4.4530  4.4412  4.3431  
        3.0000  4.3035  4.4007  4.4125  4.4217  4.4282  4.4322  4.4335  4.4322  4.4283  4.4217  4.4126  4.4008  4.3037  
        4.0000  4.2614  4.3576  4.3693  4.3783  4.3848  4.3887  4.3900  4.3887  4.3849  4.3784  4.3693  4.3577  4.2616  
        5.0000  4.2166  4.3118  4.3233  4.3323  4.3387  4.3426  4.3439  4.3426  4.3388  4.3324  4.3234  4.3119  4.2168  
        6.0000  4.1693  4.2634  4.2748  4.2836  4.2900  4.2938  4.2951  4.2938  4.2900  4.2837  4.2748  4.2635  4.1695  
        7.0000  4.1195  4.2124  4.2237  4.2324  4.2387  4.2425  4.2437  4.2425  4.2388  4.2325  4.2238  4.2125  4.1197  
        8.0000  4.0674  4.1590  4.1701  4.1788  4.1850  4.1887  4.1899  4.1887  4.1850  4.1789  4.1702  4.1591  4.0675  
        9.0000  4.0129  4.1033  4.1143  4.1228  4.1289  4.1326  4.1338  4.1326  4.1289  4.1228  4.1143  4.1034  4.0131  
        10.0000 3.9562  4.0453  4.0561  4.0645  4.0705  4.0741  4.0754  4.0742  4.0706  4.0646  4.0562  4.0454  3.9564  

        40.0000
    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        4.5612  4.6646  4.6771  4.6869  4.6939  4.6981  4.6995  4.6981  4.6939  4.6869  4.6772  4.6647  4.5613
        -9.0000 4.5543  4.6575  4.6700  4.6798  4.6867  4.6909  4.6923  4.6909  4.6868  4.6798  4.6701  4.6576  4.5544  
        -8.0000 4.5443  4.6473  4.6597  4.6694  4.6764  4.6806  4.6820  4.6806  4.6764  4.6695  4.6598  4.6473  4.5444  
        -7.0000 4.5311  4.6338  4.6462  4.6559  4.6628  4.6670  4.6684  4.6670  4.6629  4.6560  4.6463  4.6339  4.5313  
        -6.0000 4.5149  4.6172  4.6296  4.6392  4.6461  4.6503  4.6516  4.6503  4.6461  4.6393  4.6296  4.6173  4.5151  
        -5.0000 4.4956  4.5974  4.6097  4.6193  4.6262  4.6303  4.6317  4.6304  4.6262  4.6194  4.6098  4.5975  4.4958  
        -4.0000 4.4733  4.5745  4.5868  4.5964  4.6032  4.6073  4.6087  4.6073  4.6032  4.5964  4.5869  4.5746  4.4734  
        -3.0000 4.4480  4.5486  4.5608  4.5703  4.5771  4.5812  4.5825  4.5812  4.5771  4.5703  4.5609  4.5487  4.4481  
        -2.0000 4.4197  4.5197  4.5318  4.5412  4.5480  4.5520  4.5534  4.5520  4.5480  4.5413  4.5318  4.5198  4.4198  
        -1.0000 4.3885  4.4877  4.4998  4.5091  4.5158  4.5198  4.5212  4.5199  4.5159  4.5092  4.4998  4.4878  4.3887  
        0.0000  4.3545  4.4529  4.4648  4.4741  4.4808  4.4848  4.4861  4.4848  4.4808  4.4742  4.4649  4.4530  4.3546  
        1.0000  4.3176  4.4152  4.4270  4.4362  4.4428  4.4468  4.4481  4.4468  4.4429  4.4363  4.4271  4.4153  4.3178  
        2.0000  4.2781  4.3747  4.3864  4.3956  4.4021  4.4060  4.4073  4.4060  4.4021  4.3956  4.3865  4.3748  4.2783  
        3.0000  4.2359  4.3315  4.3431  4.3521  4.3586  4.3625  4.3638  4.3625  4.3586  4.3522  4.3432  4.3316  4.2361  
        4.0000  4.1911  4.2857  4.2971  4.3061  4.3124  4.3163  4.3176  4.3163  4.3125  4.3061  4.2972  4.2858  4.1913  
        5.0000  4.1438  4.2373  4.2486  4.2574  4.2637  4.2675  4.2688  4.2675  4.2638  4.2575  4.2487  4.2374  4.1440  
        6.0000  4.0941  4.1864  4.1976  4.2063  4.2125  4.2162  4.2175  4.2163  4.2125  4.2063  4.1976  4.1865  4.0942  
        7.0000  4.0420  4.1331  4.1441  4.1527  4.1589  4.1626  4.1638  4.1626  4.1589  4.1528  4.1442  4.1332  4.0422  
        8.0000  3.9877  4.0775  4.0884  4.0968  4.1029  4.1065  4.1078  4.1066  4.1029  4.0969  4.0884  4.0776  3.9878  
        9.0000  3.9312  4.0197  4.0304  4.0387  4.0447  4.0483  4.0495  4.0483  4.0448  4.0388  4.0305  4.0198  3.9314  
        10.0000 3.8726  3.9598  3.9703  3.9785  3.9844  3.9880  3.9891  3.9880  3.9845  3.9786  3.9704  3.9599  3.8728  

        50.0000
    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        4.5240  4.6266  4.6390  4.6487  4.6556  4.6597  4.6611  4.6597  4.6556  4.6487  4.6390  4.6266  4.5241
        -9.0000 4.5135  4.6158  4.6282  4.6378  4.6447  4.6489  4.6503  4.6489  4.6448  4.6379  4.6282  4.6159  4.5136  
        -8.0000 4.4999  4.6019  4.6142  4.6238  4.6307  4.6348  4.6362  4.6349  4.6307  4.6239  4.6143  4.6019  4.5000  
        -7.0000 4.4832  4.5848  4.5971  4.6067  4.6135  4.6176  4.6190  4.6177  4.6136  4.6067  4.5972  4.5849  4.4834  
        -6.0000 4.4635  4.5646  4.5769  4.5864  4.5932  4.5973  4.5987  4.5973  4.5932  4.5864  4.5769  4.5647  4.4637  
        -5.0000 4.4408  4.5414  4.5536  4.5630  4.5698  4.5739  4.5753  4.5739  4.5699  4.5631  4.5536  4.5415  4.4410  
        -4.0000 4.4152  4.5151  4.5272  4.5366  4.5434  4.5474  4.5488  4.5474  4.5434  4.5367  4.5273  4.5152  4.4153  
        -3.0000 4.3866  4.4858  4.4979  4.5072  4.5139  4.5179  4.5193  4.5180  4.5139  4.5073  4.4979  4.4859  4.3868  
        -2.0000 4.3552  4.4536  4.4656  4.4749  4.4815  4.4855  4.4868  4.4855  4.4815  4.4749  4.4656  4.4537  4.3553  
        -1.0000 4.3209  4.4186  4.4304  4.4396  4.4462  4.4502  4.4515  4.4502  4.4462  4.4397  4.4305  4.4187  4.3211  
        0.0000  4.2839  4.3807  4.3924  4.4015  4.4081  4.4120  4.4133  4.4120  4.4081  4.4016  4.3925  4.3808  4.2841  
        1.0000  4.2442  4.3401  4.3517  4.3607  4.3672  4.3711  4.3724  4.3711  4.3672  4.3608  4.3517  4.3402  4.2444  
        2.0000  4.2019  4.2968  4.3082  4.3172  4.3236  4.3274  4.3287  4.3275  4.3236  4.3172  4.3083  4.2968  4.2021  
        3.0000  4.1570  4.2508  4.2622  4.2711  4.2774  4.2812  4.2825  4.2812  4.2774  4.2711  4.2623  4.2509  4.1572  
        4.0000  4.1097  4.2024  4.2136  4.2224  4.2286  4.2324  4.2337  4.2324  4.2287  4.2224  4.2137  4.2025  4.1099  
        5.0000  4.0600  4.1515  4.1626  4.1713  4.1774  4.1812  4.1824  4.1812  4.1775  4.1713  4.1627  4.1516  4.0602  
        6.0000  4.0080  4.0983  4.1093  4.1178  4.1239  4.1275  4.1288  4.1276  4.1239  4.1178  4.1093  4.0984  4.0082  
        7.0000  3.9538  4.0429  4.0536  4.0620  4.0680  4.0717  4.0729  4.0717  4.0681  4.0621  4.0537  4.0429  3.9540  
        8.0000  3.8975  3.9852  3.9958  4.0041  4.0100  4.0136  4.0148  4.0136  4.0101  4.0042  3.9959  3.9853  3.8977  
        9.0000  3.8392  3.9255  3.9360  3.9441  3.9500  3.9535  3.9546  3.9535  3.9500  3.9442  3.9361  3.9256  3.8393  
        10.0000 3.7789  3.8639  3.8741  3.8822  3.8879  3.8913  3.8925  3.8914  3.8879  3.8822  3.8742  3.8640  3.7791  

    Function: aero/coefficient/CLalpha
    Function: aero/coefficient/CDo
    1 dimensional table with 4 rows.
        0.0000  0.0000
        10.0000 0.0070
        20.0000 0.0120
        30.0000 0.0180
    Function: aero/coefficient/CDDf
    2 dimensional table with 26 rows, 4 columns.
                0.0000  10.0000 20.0000 30.0000
        -0.0873 0.0041  0.0000  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 0.0020  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  0.0240  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  0.1240  0.1343
        0.1396  0.0860  0.1232  0.1442  0.1554
        0.1571  0.0962  0.1353  0.1573  0.1690
        0.1745  0.1069  0.1479  0.1708  0.1830
        0.1920  0.1180  0.1610  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
        0.2618  0.1727  0.2240  0.2521  0.2667
        0.2793  0.1782  0.2302  0.2587  0.2735
        0.2967  0.1716  0.2227  0.2507  0.2653
        0.3142  0.1618  0.2115  0.2388  0.2531
        0.3316  0.1475  0.1951  0.2214  0.2351
        0.3491  0.1097  0.1512  0.1744  0.1866
    Function: aero/coefficient/CDwbh
    Function: aero/coefficient/CDDe
    Function: aero/coefficient/CDbeta
    1 dimensional table with 3 rows.
        -0.3490 0.1080
        0.0000  0.0000
        0.3490  -0.1080
    Function: aero/coefficient/CYb
    Function: aero/coefficient/CYda
    Function: aero/coefficient/CYdr
    Function: aero/coefficient/CYp
    Function: aero/coefficient/CYr
    1 dimensional table with 3 rows.
        -0.3490 0.0311
        0.0000  0.0000
        0.3490  -0.0311
    Function: aero/coefficient/Clb
    Function: aero/coefficient/Clp
    1 dimensional table with 2 rows.
        0.0000  0.0800
        0.0940  0.1900
    Function: aero/coefficient/Clr
    Function: aero/coefficient/Clda
    Function: aero/coefficient/Cldr
    Function: aero/coefficient/Cmalpha
    1 dimensional table with 4 rows.
        0.0000  0.0000
        10.0000 -0.0300
        20.0000 -0.0500
        30.0000 -0.0600
    Function: aero/coefficient/CmDf
    Function: aero/coefficient/Cmq
    Function: aero/coefficient/Cmadot
    Function: aero/coefficient/Cmo
    Function: aero/coefficient/Cmde
    1 dimensional table with 3 rows.
        -0.3490 -0.0227
        0.0000  0.0000
        0.3490  0.0227
    Function: aero/coefficient/Cnb
    Function: aero/coefficient/Cnp
    Function: aero/coefficient/Cnr
    Function: aero/coefficient/Cnda
    Function: aero/coefficient/Cndr

  Output data set: 0
    Function: velocities/pi-deg_sec

脚本xml文件:C172-01A 滑跑起飞过程

"C:\jsbsim-master\scripts\c1723.xml"

上面是文件位置,下面是读取结果。

一共六个事件:

  1. 发动机启动
    在0.25秒时刻启动发动机,并配置自动驾驶仪以保持飞机的滚转角
  2. 开始滑跑
    飞机在3秒时刻释放刹车并开始滑跑,同时将襟翼设置为10度以增加升力,为飞机的加速和随后的起飞做准备
  3. 爬升
    达到51节校准空速时触发抬头操作,离地并开始爬升
  4. 设置自动驾驶高度6000英尺
    达到51节校准空速后延迟10秒触发,设置自动驾驶仪的目标高度为6000英尺。
  5. 调整油门/襟翼
    飞机离地高度达到1000英尺时触发,执行的操作包括收回襟翼和设置新的航向。
  6. 每分钟输出飞行状态信息
Script: "C172-01A takeoff run"
  begins at 0.0000 seconds and runs to 200.0083 seconds with dt = 0.008333 (120.000000 Hz)

Local property: left-brake-cmd-norm = 1.000000
Local property: center-brake-cmd-norm = 1.000000
Local property: right-brake-cmd-norm = 1.000000
Local property: randomseed = 2498.000000
Local property: heading-selector-switch = 1.000000
Local property: specified-heading-rad = 3.490000
Local property: run_id = 1.000000
Local property: notify-time-trigger = 0.000000
Event 0 (engine start):
  When first triggered, executes once  if all of the following are true: {
    sim-time-sec >= constant value 0.250000
  }
  Actions taken:
    {
      set fcs/throttle-cmd-norm to 1.000000 (constant via ramp with time constant 0.500000)
      set propulsion/magneto_cmd to 3.000000 (constant via step)
      set propulsion/starter_cmd to 1.000000 (constant via step)
      set ap/roll-attitude-mode to 1.000000 (constant via step)
      set ap/autopilot-roll-on to 1.000000 (constant via step)
    }
  Notifications:
    {
      run id
      hdg-roll-err-c1
      a-pilot-x-ft sec2
      a-pilot-y-ft sec2
      a-pilot-z-ft sec2
      n-pilot-x-norm
      n-pilot-y-norm
      n-pilot-z-norm
      Nz
      pdot-rad sec2
      qdot-rad sec2
      rdot-rad sec2
      udot-ft sec2
      vdot-ft sec2
      wdot-ft sec2
      h-dot-fps
      v-north-fps
      v-east-fps
      v-down-fps
      u-fps
      v-fps
      w-fps
      p-rad sec
      q-rad sec
      r-rad sec
      pi-rad sec
      qi-rad sec
      ri-rad sec
      eci-velocity-mag-fps
      vc-fps
      vc-kts
      ve-fps
      ve-kts
      vtrue-fps
      vtrue-kts
      machU
      p-aero-rad sec
      q-aero-rad sec
      r-aero-rad sec
      phidot-rad sec
      thetadot-rad sec
      psidot-rad sec
      u-aero-fps
      v-aero-fps
      w-aero-fps
      vt-fps
      mach
      vg-fps
    }

Event 1 (Begin roll):
  When first triggered, executes once  if all of the following are true: {
    sim-time-sec >= constant value 3.000000
  }
  Actions taken:
    {
      set fcs/left-brake-cmd-norm to 0.000000 (constant via step)
      set fcs/right-brake-cmd-norm to 0.000000 (constant via step)
      set fcs/center-brake-cmd-norm to 0.000000 (constant via step)
      set fcs/flap-cmd-norm to 0.330000 (constant via step)
      set fcs/elevator-cmd-norm to 0.000000 (constant via step)
    }
  Notifications:
    {
      vc-kts
      h-agl-ft
      lat-geod-deg
      geod-alt-ft
      throttle-pos-norm
      mixture-pos-norm
      weight-lbs
      propeller-rpm
    }

Event 2 (Rotate):
  When first triggered, executes once  if all of the following are true: {
    vc-kts >= constant value 51.000000
  }
  Actions taken:
    {
      set ap/altitude_setpoint to 1000.000000 (constant via step)
      set ap/altitude_hold to 1.000000 (constant via step)
    }
  Notifications:
    {
      vc-kts
      h-agl-ft
      lat-geod-deg
      geod-alt-ft
      throttle-pos-norm
      mixture-pos-norm
      weight-lbs
      propeller-rpm
    }

Event 3 (Set autopilot for 6000 ft.):
  When first triggered, executes once  if all of the following are true: {
    vc-kts >= constant value 51.000000
  }
  Actions taken (after a delay of 10.000000 secs):
    {
      set ap/altitude_setpoint to 6000.000000 (constant via step)
      set simulation/output/log_rate_hz to 10.000000 (constant via step)
    }
  Notifications:
    {
      vc-kts
      h-agl-ft
      lat-geod-deg
      geod-alt-ft
      throttle-pos-norm
      mixture-pos-norm
      weight-lbs
      propeller-rpm
    }

Event 4 (Adjust throttle/flaps):
  When first triggered, executes once  if all of the following are true: {
    h-agl-ft >= constant value 1000.000000
  }
  Actions taken:
    {
      set fcs/flap-cmd-norm to 0.000000 (constant via step)
      set guidance/specified-heading-rad to 1.750000 (constant via step)
      set ap/roll-attitude-mode to 1.000000 (constant via step)
      set simulation/write-state-file to 2.000000 (constant via step)
    }

Event 5 (Time Notify):
  Whenever triggered, executes once  if all of the following are true: {
    sim-time-sec >= notify-time-trigger
  }
  Actions taken:
    {
      set simulation/notify-time-trigger to 60.000000 (delta via step)
    }
  Notifications:
    {
      vc-kts
      h-agl-ft
      lat-geod-deg
      geod-alt-ft
      throttle-pos-norm
      mixture-pos-norm
      weight-lbs
      propeller-rpm
    }

Output filename change from ./JSBout172B.csv from aircraft configuration file to c1723.csv specified on command line

配置信息:

GEAR_CONTACT: 0.000000 seconds: Nose Gear 1
GEAR_CONTACT: 0.000000 seconds: Left Main Gear 1
GEAR_CONTACT: 0.000000 seconds: Right Main Gear 1
    Simulation parameters logged
    Rate parameters logged
    Velocity parameters logged
    Mass parameters logged
    Propagate parameters logged
    FCS parameters logged
    Propulsion parameters logged
    Properties logged:
      - vrp-gc-latitude_deg
      - vrp-longitude_deg
      - vrp-radius-ft

  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                        1454.0    41.0     0.0    36.5       948.0      1346.0      1967.0        -0.0         0.0        -0.0
0   PILOT                                190.0    36.0   -14.0    24.0         0.0         0.0         0.0        -0.0         0.0        -0.0
1   CO-PILOT                             140.0    36.0    14.0    24.0         0.0         0.0         0.0        -0.0         0.0        -0.0
2   PASSENGER 1                          130.0    60.0   -14.0    24.0         0.0         0.0         0.0        -0.0         0.0        -0.0
3   PASSENGER 2                          106.0    60.0    14.0    24.0         0.0         0.0         0.0        -0.0         0.0        -0.0
4   LUGGAGE                              120.0    95.0     0.0    24.0         0.0         0.0         0.0        -0.0         0.0        -0.0
5   PesticideBomb                         80.0    41.0   144.0    36.0         0.0         0.0         0.0        -0.0         0.0        -0.0
0   Fuel                                   130      48    -112    59.4      9.7013      9.7013      9.7013
1   Fuel                                   130      48     112    59.4      9.7013      9.7013      9.7013
                                                                                                                        
    Total:                            2480.0    45.5     4.2    35.4      2095.7      1505.0      3150.4       -10.8        13.6         4.0

End of vehicle configuration loading.
-------------------------------------------------------------------------------

Simulation Configuration
------------------------
Mass Properties Model:
Ground Reactions Model:
Aerodynamics Model:
Propulsion Model:

------------------------------------------------------------------
State Report at sim time: 0.000000 seconds
  Position
    ECI:   -1636354.08174152, -18107108.71473717, 10325659.96215431 (x,y,z, in ft)
    ECEF:  -1636354.081742 , -18107108.714737 , 10325659.962154 (x,y,z, in ft)
    Local: 29.759526, -95.163839, 4.305018 (geodetic lat, lon, alt ASL in deg and ft)

  Orientation
    ECI:   180, -60.24047397481984, 84.836161 (phi, theta, psi in deg)
    Local: -1.192708005548819e-15, -7.951386703658792e-15, 7.951386703658792e-16 (phi, theta, psi in deg)

  Velocity
    ECI:   1320.391190653657, -119.3248214477856, 0 (x,y,z in ft/s)
    ECEF:  0, 0, 0 (x,y,z in ft/s)
    Local: 0.000000 , 0.000000 , 0.000000 (n,e,d in ft/sec)
    Body:  0.000000 , 0.000000 , 0.000000 (u,v,w in ft/sec)

  Body Rates (relative to given frame, expressed in body frame)
    ECI:   0.003627054262170481, 0, -0.002073832402526141 (p,q,r in deg/s)
    ECEF:  0, 0, 0 (p,q,r in deg/s)

JSBSim开始运行上面的脚本文件:

每分钟获取状态信息:

---- JSBSim Execution beginning ... --------------------------------------------


Time Notify (Event 5) executed at time: 0.008333
    Cal. airspeed (kts):   = 0.000000
    Altitude (AGL, ft):    = 4.305000
    Latitude (geod, deg):  = 29.759526
    Altitude (geod, ft):   = 4.305000
    Throttle pos:          = 0.000000
    Mixture pos:           = 0.999480
    Weight (lbs):          = 2480.000000
    Propeller RPM:         = 0.000000
  1. 然后运行第一个事件,启动发动机,输出结果如下:

Start: Wednesday October 09 2024 09:42:48 (HH:MM:SS)

engine start (Event 0) executed at time: 0.258333
    Sim Run ID:  = 1.000000
    ap/hdg-roll-err-c1 = 0.500000
    accelerations/a-pilot-x-ft_sec2 = -0.092034
    accelerations/a-pilot-y-ft_sec2 = -0.437431
    accelerations/a-pilot-z-ft_sec2 = -32.050636
    accelerations/n-pilot-x-norm = -0.002861
    accelerations/n-pilot-y-norm = -0.013596
    accelerations/n-pilot-z-norm = -0.996164
    accelerations/Nz = 0.996318
    accelerations/pdot-rad_sec2 = -0.067422
    accelerations/qdot-rad_sec2 = 0.020971
    accelerations/rdot-rad_sec2 = -0.000187
    accelerations/udot-ft_sec2 = -0.093934
    accelerations/vdot-ft_sec2 = -0.267800
    accelerations/wdot-ft_sec2 = 0.054013
    velocities/h-dot-fps = -0.016088
    velocities/v-north-fps = -0.035222
    velocities/v-east-fps = 0.113689
    velocities/v-down-fps = 0.016088
    velocities/u-fps = -0.035240
    velocities/v-fps = 0.113768
    velocities/w-fps = 0.015483
    velocities/p-rad_sec = 0.026447
    velocities/q-rad_sec = 0.008187
    velocities/r-rad_sec = -0.000011
    velocities/pi-rad_sec = 0.026511
    velocities/qi-rad_sec = 0.008187
    velocities/ri-rad_sec = -0.000047
    velocities/eci-velocity-mag-fps = 1325.885657
    velocities/vc-fps = 0.120095
    velocities/vc-kts = 0.071154
    velocities/ve-fps = 0.120095
    velocities/ve-kts = 0.071154
    velocities/vtrue-fps = 0.120103
    velocities/vtrue-kts = 0.071159
    velocities/machU = -0.000032
    velocities/p-aero-rad_sec = 0.026447
    velocities/q-aero-rad_sec = 0.008187
    velocities/r-aero-rad_sec = -0.000011
    velocities/phidot-rad_sec = 0.026447
    velocities/thetadot-rad_sec = 0.008187
    velocities/psidot-rad_sec = 0.000030
    velocities/u-aero-fps = -0.035240
    velocities/v-aero-fps = 0.113768
    velocities/w-aero-fps = 0.015483
    velocities/vt-fps = 0.120103
    velocities/mach = 0.000108
    velocities/vg-fps = 0.119020
  1. 在3秒时刻释放刹车并开始滑跑,同时将襟翼设置为10度以增加升力
Begin roll (Event 1) executed at time: 3.008333
    Cal. airspeed (kts):   = 0.105720
    Altitude (AGL, ft):    = 4.312023
    Latitude (geod, deg):  = 29.759526
    Altitude (geod, ft):   = 4.312023
    Throttle pos:          = 1.000000
    Mixture pos:           = 0.999480
    Weight (lbs):          = 2479.983615
    Propeller RPM:         = 2166.873237

  1. 爬升
    达到51节校准空速时触发抬头操作,离地并开始爬升
Rotate (Event 2) executed at time: 21.908333
    Cal. airspeed (kts):   = 51.003221
    Altitude (AGL, ft):    = 4.423090
    Latitude (geod, deg):  = 29.758661
    Altitude (geod, ft):   = 4.423090
    Throttle pos:          = 1.000000
    Mixture pos:           = 0.999476
    Weight (lbs):          = 2479.585758
    Propeller RPM:         = 2560.350200

GEAR_CONTACT: 23.533333 seconds: Nose Gear 0
GEAR_CONTACT: 23.808333 seconds: Right Main Gear 0
GEAR_CONTACT: 24.375000 seconds: Left Main Gear 0

Takeoff report for Nose Gear (Liftoff at time: 28.525000 seconds)
  Distance traveled:                988.154557 ft,     301.189509 meters
  Distance traveled (over 50'):     1472.140712 ft,     448.708489 meters
  [Altitude (ASL): 53.240946 ft. / 16.227840 m  | Temperature: 58.810135 F / 14.894519 C]
  [Velocity (KCAS): 55.815511]

Takeoff report for Left Main Gear (Liftoff at time: 28.600000 seconds)
  Distance traveled:                1068.259685 ft,     325.605552 meters
  Distance traveled (over 50'):     1479.055988 ft,     450.816265 meters
  [Altitude (ASL): 54.671069 ft. / 16.663742 m  | Temperature: 58.805035 F / 14.891686 C]
  [Velocity (KCAS): 55.681726]

Takeoff report for Right Main Gear (Liftoff at time: 28.600000 seconds)
  Distance traveled:                1013.999199 ft,     309.066956 meters
  Distance traveled (over 50'):     1479.055988 ft,     450.816265 meters
  [Altitude (ASL): 54.671069 ft. / 16.663742 m  | Temperature: 58.805035 F / 14.891686 C]
  [Velocity (KCAS): 55.681726]

  1. 设置自动驾驶高度6000英尺
    达到51节校准空速后延迟10秒触发,设置自动驾驶仪的目标高度为6000英尺。

Set autopilot for 6000 ft. (Event 3) executed at time: 31.916667
    Cal. airspeed (kts):   = 50.655934
    Altitude (AGL, ft):    = 110.267642
    Latitude (geod, deg):  = 29.756287
    Altitude (geod, ft):   = 110.267642
    Throttle pos:          = 1.000000
    Mixture pos:           = 0.995662
    Weight (lbs):          = 2479.366278
    Propeller RPM:         = 2566.273189

  1. 每分钟输出飞行状态信息

Time Notify (Event 5) executed at time: 60.008333
    Cal. airspeed (kts):   = 50.544889
    Altitude (AGL, ft):    = 364.636889
    Latitude (geod, deg):  = 29.749774
    Altitude (geod, ft):   = 364.636889
    Throttle pos:          = 1.000000
    Mixture pos:           = 0.986538
    Weight (lbs):          = 2478.758519
    Propeller RPM:         = 2566.218544


Time Notify (Event 5) executed at time: 120.000000
    Cal. airspeed (kts):   = 47.863100
    Altitude (AGL, ft):    = 889.310518
    Latitude (geod, deg):  = 29.736128
    Altitude (geod, ft):   = 889.310518
    Throttle pos:          = 1.000000
    Mixture pos:           = 0.967928
    Weight (lbs):          = 2477.479562
    Propeller RPM:         = 2545.877527
  1. 调整油门/襟翼
    飞机离地高度达到1000英尺时触发,执行的操作包括收回襟翼和设置新的航向。

Adjust throttle/flaps (Event 4) executed at time: 133.441667

Time Notify (Event 5) executed at time: 180.000000
    Cal. airspeed (kts):   = 52.703078
    Altitude (AGL, ft):    = 1439.148798
    Latitude (geod, deg):  = 29.729021
    Altitude (geod, ft):   = 1439.148798
    Throttle pos:          = 1.000000
    Mixture pos:           = 0.948737
    Weight (lbs):          = 2476.210045
    Propeller RPM:         = 2578.831079
    
End: Wednesday October 09 2024 10:15:34 (HH:MM:SS)

仿真后获取的数据曲线:

横坐标为时间
迎角、侧滑角单位是度
在这里插入图片描述

在这里插入图片描述

高度变化曲线:
在这里插入图片描述
速度曲线:
在这里插入图片描述
襟翼控制曲线:
在这里插入图片描述

在这里插入图片描述

在这里插入图片描述
发动机推力曲线:

在这里插入图片描述

发动机转速曲线
在这里插入图片描述

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