Design of a SDINS using the nonlinear observer

비선형 관측기를 이용한 스트랩다운 관성항법시스템 구성

  • 유명종 (서울대학교 전기공학부) ;
  • 이장규 (서울대학교 전기공학부) ;
  • 박찬국 (광운대학교 제어계측공학과) ;
  • 심덕선 (중아대학교 전자전기공학부)
  • Published : 2000.10.01

Abstract

The nonlinear observers are proposed for a nonlinear system. To improve the characteristics such as a stability, a convergence, and an H$\sub$$\infty$/ filter performance criterion, we utilize and H$\sub$$\infty$/ filter Riccati equation or a modified H$\sub$$\infty$/ filter Riccati equation with a freedom parameter. Using the Lyapunov, the characteristics of the observer are analyzed. Then the in-flight alignment for a strapdown inertial navigation system(SDINS) is designed using the observer proposed. Simulation results show that the observer with the modified H$\sub$$\infty$/ fitter Riccati equation effectively improve the performance of the in-flight alignment.

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