sensors.hlp

MATLAB在飞行动力学和控制中应用的工具

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 Sensor dynamics / subtract initial conditions
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 Subsystem of APILOT1, APILOT2, and APILOT3 (APILOT1 only con-
 tains the subtraction part of this subsystem).

 This subsystem contains the dynamics of the sensor models for
 the output signals from the non-linear aircraft model BEAVER.
  Since the control laws often require deviations from the nominal
 values of the outputs in stead of the output signals themselves,
 this block also determines the differences between the measured
 signals and their initial values.

 The current implementation is actually only intended to provide
 a framework for future enhancements of the autopilot models: only
 a few airdata-sensor models have actually been implemented! The
 most important is a quantization effect in the altitude measure-
 ment due to a relatively large least-significant bit used in the
 airdata computer. Sensormodels for the other signals (including
 similar sampling or quantization effects) can easily be implemen-
 ted in the framework from this subsystem.

 More info
 =========
 See APILOT.HLP for more general information about the 'Beaver'
 autopilot simulation system.

 References
 ==========
 [1]  M.O. Rauw, A SIMULINK environment for Flight Dynamics and
      Control analysis - Application to the DHC-2 'Beaver',
      PART II! Graduate's thesis, Delft University of Technology,
      Faculty of Aerospace Engineering, Delft, 1993.

 [2]  P.N.H. Wever, Ontwerp en implementatie van de regelwetten
      van de De Havilland DHC-2 'Beaver' (in Dutch). Graduate's
      thesis, Delft University of Technology, Faculty of Aero-
      space Engineering, Delft, 1993.

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The FDC toolbox, Copyright Marc Rauw 1994-1998.