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INS/GPS Integration System Using Adaptive Filter with Estimating Measurement Noise Variance

측정잡음 분산추정 적응필터를 이용한 INS/GPS 결합 시스템

  • Published : 2007.07.01

Abstract

The INS/GPS integration system is designed by employing an adaptive filter that can estimate the measurement noise variance using the residual of the filter. To verify the efficiency of the proposed loosely-coupled INS/GPS integration system, simulation is performed by assuming that GPS information has large position errors. Simulation results show that the proposed integration system with the adaptive filter is more effective in estimating the position and attitude errors than those with the Extended Kalman Filter.

Keywords

References

  1. P. S. Maybeck, Stochastic Models, Estimation, and Control, vol. 2, New York: Academic Press, 1979
  2. C. Hihe, T. Moore, and M. Smith, 'Adaptive Kalman filtering for low cost INS/GPS,' Proceedings of the Institute of Navigion GPS-2002, pp. 1143-1147
  3. D. Choukroun, I. Y. Bar-Itzhack, and Y. Oshman, 'Novel quaternion Kalman filter,' Proceedings of the American Institute of Aeronautics and Astronautics, AIAA 2002-4460, 2002
  4. 유명종, 박찬주, 김현백, '레이다 보정형 스트랩다운 관성항법 시스템을 위한 적응필터 구성,' 제어.자동화.시스템공학 논문지, 제 9 권, 제 6 호, pp. 420-424, 2003
  5. 유명종, 'INS/GPS를 위한 적응필터 구성,' 제어.자동화.시스템공학 논문지, 제 11 권, 제 8 호, pp. 717-725, 2005 https://doi.org/10.5302/J.ICROS.2005.11.8.717
  6. 엄태윤, '확장된 가관측행렬의 영공간을 이용한 잡음 공분산 추정 기법 연구,' 서울대학교 공학박사 학위논문, 2000
  7. A. H. Mohamed and K. P. Schwarz, 'Adaptive Kalman filtering for INS/GPS,' Journal of Geodesy, vol. 73, pp.193-203, 1999 https://doi.org/10.1007/s001900050236
  8. O. S. Salychev, Applied Inertial Navigation: Problems and Solutions, Moscow Russia, BMSTU Press, 2004
  9. D. Damjanovic and J. Schiefele, 'Enhancing general aviation safety with synthetic vision systems,' Proceedings of Institute of Navigation NTM, 423-432, 2000
  10. Y. Oshman and M. Koifman, 'Robust navigation using the global positioning system in the presence of spoofing,' AIAA Journal of Guidance, Control, and Dynamics, vol. 29, no. 1, pp. 95-104, 2006 https://doi.org/10.2514/1.6493
  11. 유명종, 전창배, '자세오차 및 속도오차 미분방정식에 따른 속도보정 SDINS의 칼만필터 성능분석,' 95 한국자동 화제어학술회의 논문집, pp. 1065-1068, 1995
  12. 유명종, 이장규, 박찬국, 'Lyapunov 변환을 이용한 SDINS 등가 오차모델,' 제어.자동화.시스템공학 논문지, 제 8 권, 제 2 호, pp. 167-177, 2002
  13. M.-J. Yu, J. G. Lee, and H.-W. Park, 'Comparison of SDINS inflight alignment using equivalent error model,' IEEE Transaction on Aerospace and Electronic Systems, vol. 35, no. 3, pp. 1046-1054, 1999 https://doi.org/10.1109/7.784073
  14. M.-J. Yu, J. G. Lee, and C. G. Park, 'Nonlinear robust observer design for strapdown INS in-flight alignment,' IEEE Transaction on Aerospace and Electronic Systems, vol. 40, no. 3, pp. 797-807, 2004 https://doi.org/10.1109/TAES.2004.1337455
  15. K. Reif, S. Gunther, E. Yaz, and R. Unbehauen, 'Stochastic stability of the discret-time extended Kalman filter,' IEEE Transaction on Automatic Control, vol. 44, no. 4, pp. 714-728, 1999 https://doi.org/10.1109/9.754809