<xsl:value-of select="@name"/>
Configuration File Version:
Release level:
License:
[File Information] [Metrics] [Mass and Balance] [Ground Reactions] [Buoyant Forces] [External Reactions] [Propulsion] [System: ] [System: ] [Autopilot] [Flight Control] [Aerodynamics] [Input] [Output]

FILE INFORMATION
Author[s] ,
File created
Description
Model version
References:
Notes:
Limitations:

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METRICS
Wing span ()
Wing area ()
Chord ()
Horizontal tail area ()
Horizontal tail arm ()
Vertical tail area ()
Vertical tail arm ()
Aerodynamic reference point location () , ,
Visual reference point location (): , ,
Eyepoint location (): , ,
is an invalid location!

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MASS AND BALANCE
Moments of Inertia
Ixx ()
Iyy ()
Izz ()
Ixy ()
Ixz ()
Iyz ()
Empty Weight ()
Center of Gravity (CG) Location: () , ,
Weight ():
Position (): , ,

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GROUND REACTIONS
Bogey: Position (): , ,
Static friction coefficient:
Dynamic friction coefficient:
Rolling friction coefficient:
Spring constant ():
Damping constant ():
Maximum steering angle ():
Contact point: Stuff

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PROPULSION
Engine: [Defined in file: .xml] Engine location: [, , ] (Unit: )
Thruster: [Defined in file: .xml]

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ABCDEFGHIJKLMNOPQRSTUVWXYZ abcdefghijklmnopqrstuvwxyz-
System:
Channel

Component: , Type: Lag filter
Component property name: fcs/
Input:
Filter:
s +
Integrator
Component property name: fcs/
Input:
Filter:
s
Trigger property: Lead-lag filter
Component property name: fcs/
Input:
Filter: s +
s +
Second order filter
Component property name: fcs/
Input:
Filter: s2 + s +
s2 + s +
Washout filter
Component property name: fcs/
Input:
Filter: s
s +
Gain
Component property name: fcs/
Input:
Scheduled gain
Component property name: fcs/
Input:
Aerosurface scale
Component property name: fcs/
Input:
Summer
Component property name: fcs/
Input:
Deadband
Component property name: fcs/
Input:
Switch
Component property name: fcs/
Input:

  • If all of the following tests are true: If any of the following tests are true: If all of the following tests are true:
    then the switch value is:
  • Otherwise, the value is:

Kinematic
Component property name: fcs/
Input:
Function
Component property name: fcs/
Input:
PID Controller
Component property name: fcs/
Input:
Proportional gain (kp):
Integral gain (ki):
Derivative gain (kd):
Trigger property: Minimum limit:
Maximum limit:
Output to:

System: [Defined in file: .xml]

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ABCDEFGHIJKLMNOPQRSTUVWXYZ abcdefghijklmnopqrstuvwxyz-
Autopilot:
Channel

Component: , Type: Lag filter
Component property name: fcs/
Input:
Filter:
s +
Integrator
Component property name: fcs/
Input:
Filter:
s
Trigger property: Lead-lag filter
Component property name: fcs/
Input:
Filter: s +
s +
Second order filter
Component property name: fcs/
Input:
Filter: s2 + s +
s2 + s +
Washout filter
Component property name: fcs/
Input:
Filter: s
s +
Gain
Component property name: fcs/
Input:
Scheduled gain
Component property name: fcs/
Input:
Aerosurface scale
Component property name: fcs/
Input:
Summer
Component property name: fcs/
Input:
Deadband
Component property name: fcs/
Input:
Switch
Component property name: fcs/
Input:

  • If all of the following tests are true: If any of the following tests are true: If all of the following tests are true:
    then the switch value is:
  • Otherwise, the value is:

Kinematic
Component property name: fcs/
Input:
Function
Component property name: fcs/
Input:
PID Controller
Component property name: fcs/
Input:
Proportional gain (kp):
Integral gain (ki):
Derivative gain (kd):
Trigger property: Minimum limit:
Maximum limit:
Output to:

Autopilot: [Defined in file: .xml]

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ABCDEFGHIJKLMNOPQRSTUVWXYZ abcdefghijklmnopqrstuvwxyz-
FLIGHT CONTROL
Channel

Component: , Type: Lag filter
Component property name: fcs/
Input:
Filter:
s +
Integrator
Component property name: fcs/
Input:
Filter:
s
Trigger property: Lead-lag filter
Component property name: fcs/
Input:
Filter: s +
s +
Second order filter
Component property name: fcs/
Input:
Filter: s2 + s +
s2 + s +
Washout filter
Component property name: fcs/
Input:
Filter: s
s +
Gain
Component property name: fcs/
Input:
Scheduled gain
Component property name: fcs/
Input:
Aerosurface scale
Component property name: fcs/
Input:
Summer
Component property name: fcs/
Input:
Deadband
Component property name: fcs/
Input:
Switch
Component property name: fcs/
Input:

  • If all of the following tests are true: If any of the following tests are true: If all of the following tests are true:
    then the switch value is:
  • Otherwise, the value is:

Kinematic
Component property name: fcs/
Input:
Function
Component property name: fcs/
Input:
PID Controller
Component property name: fcs/
Input:
Proportional gain (kp):
Integral gain (ki):
Derivative gain (kd):
Trigger property: Minimum limit:
Maximum limit:
Output to:


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AERODYNAMICS
The aerodynamics specification for this aircraft consists of function[s] and force components in axes.
Global Functions

Axis


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INPUT
Input accepted on port .

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OUTPUT

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[ () () (table) ] (βrad) (αrad) (Sw) (bw) (qbar) (CL2) (M) [bw/(2V)] ()