A precise parameter estimation of an air vehicle without a priori information

사전 정보가 없는 비행체의 정밀 파라미터 추정

  • 김정한 (한국항공대학교 대학원 항공우주기계공학과) ;
  • 박근범 (한국항공대학교 대학원 항공우주기계공학과) ;
  • 송용규 (한국항공대학교 항공우주 및 기계공학부) ;
  • 황익호 (국방과학연구소) ;
  • 최동균 (국방과학연구소)
  • Received : 2010.08.20
  • Accepted : 2010.09.12
  • Published : 2010.09.30

Abstract

This paper deals with the precise parameter estimation of an air vehicle without a priori information. First, Recursive Least Squares technique, which is an equation error method and does not require any a priori information, is applied and then the extended Kalman filter is used to tune parameters more precisely. To show the performance, a nonlinear longitudinal missile model is simulated and the parameters are estimated. The results show that this consecutive application of the techniques gives a very good estimation performance.

Keywords

References

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