상태변수 추정을 이용한 김발형 관성항법시스템의 교정기법에 대한 연구

Calibration of gimballed inertial navigation systems using state estimation

  • 김갑진 (한양대학교 제어계측공학과) ;
  • 송택렬 (한양대학교 제어계측공학과)
  • Kim, Gap-Jin (Dept. of Control and Instrumentation Engineering, Hanyang University) ;
  • Song, Taek-Ryeol (Dept. of Control and Instrumentation Engineering, Hanyang University)
  • 발행 : 1998.02.01

초록

Gimballed Inertial Navigation Systems(GINS) are sophisticated autonomous electro-mechanical systems which supply the position, velocity and attitude of the vehicle on which they are mounted. In order to maintain accuracy of outputs, the GINS are required to regularly calibrate senior errors. However, existing calibration methods take up a long time due to multiposition alignments needed to increase accuracy. A particular system formulation for calibration of a GINS is proposed to enhance system observability and thus to expedite calibration procedure. Performance of the proposed calibration method is compared with existing methods such as Schuler test and muliposition alignment. Simulation studies show the proposed system formulation associated with a suggested suboptimal filter is accurate as well as efficient in error identification essential to GINS calibration.

키워드

참고문헌

  1. Inertial Navigation System Analysis K. R. Britting
  2. Aerospace Avionics Systems G. M. Siouris
  3. Inertial Guidance G. R. Pitman
  4. Modern Navigation, Guidance, and Control Processing C. F. Lin
  5. IEEE transactions on Aerospace and Electronics Systems v.29 no.4 Muliposition alignment of strapdown inertial navigation systems J. G. Lee;C. G. Park;H. W. Park
  6. IEEE Transactions on Aerospace and Electronic Systems v.28 no.1 Error estimation of INS ground alignment through observability analysis Y. F. Jiang;Y. P. Lin
  7. Journal of Guidance, Control and Dynamics v.11 no.3 Control theoretic approach to inertial navigation systems I. Y. Bar-Itzhack;N. Berman
  8. IEEE Transactions on Aerospace and Electronic Systems v.AES-5 no.3 Ground testing of inertial navigators to improve dynamic performance G. L. Perreault
  9. Linear System Theory and Design C. T. Chen
  10. Software Design Document for FIN 1041 Inertial Navigation System GEC Ferranti
  11. '95 한국자동제어학술회의 논문집 칼만필터를 이용한 김블형 관성항법시스템의 교정기법 김천중;최상욱;박홍원;유준
  12. '95 한국자동제어학술회의 논문집 속도오차 초기화를 이용한 김블형 관성항법시스템의 교정기법 김천중;박정화;유명종;박홍원
  13. IEEE Transactions on Aerospace and Electronic Systems v.28 no.4 Observability analysis of piece-wise constant systems-Part 1 : theory D. Goshen-Meskin;I. Y. Bar-Itzhack
  14. IEEE Transactions on Aeros-pace and Electronic Systems v.28 no.4 Observability analysis of piece-wise constant systems-Part 2 : application to inertial navigation in-flight alignment D. Goshen-Meskin;I. Y. Bar-Itzhack
  15. Stochastic Models, Estimation, and Control P. S. Maybeck