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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2008, Vol. 29 ›› Issue (2): 467-471.

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Application of D-optimal Test Design Method in Testing of Dynamically Tuned Gyroscope

Fu Li, Liu Wenli   

  1. School of Automatic Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics
  • Received:2007-07-20 Revised:2007-12-13 Online:2008-03-15 Published:2008-03-15
  • Contact: Fu Li

Abstract:

In order to obtain a better estimate of the accelerationinsensitive drift rate, accelerationsensitive drift rate coefficients and misalignment angles of the assumed performance model of the twodegree of freedom dynamically tuned gyroscope, a new D-optimal eightposition test method is proposed, according to the D-optimal test design method and the symmetric separate design idea of orthogonal design. A search method in the whole orthogonal space is used to verify the D-optimal property of the new test method.

Key words: optimal , test , design,  , dynamically , tuned , gyroscope,  , error , model,  , drift , testing,  , eight-position

CLC Number: