Angular Rate and Acceleration Matching Algorithm in Aircraft in Consideration of Flexure

비행체에서 유연성을 고려한 각속도 및 가속도정합 알고리즘

  • Yang, Cheol-Kwan (Dept.of Electronics Electric Engineering, Chungang University) ;
  • Shim, Duk-Sun (Dept.of Electronics Electric Engineering, Chungang University)
  • 양철관 (중앙대학교 전자전기공학부) ;
  • 심덕선 (중앙대학교 전자전기공학부)
  • Published : 2000.12.01

Abstract

In this paper we propose an angular rate and acceleration matching method for initial transfer alignment in aircraft. The conventional angular rate and acceleration matching method performs compensation for the lever arm effects between the master and slave INS before initial alignment. However, the conventional method does not take the flexure angular acceleration into account and thus is not effective when the flexure angular acceleration is large. We propose a new angular rate and acceleration matching method to cope with the flexure acceleration between the master and slave INS and compare the results with those of the conventional method by simulation. The simulation results show that the proposed matching method is better than the conventional matching method in case of large flexure acceleration.

Keywords

References

  1. M. B. Pszczel and D. Bucco, 'Review of techniques for in-flight transfer alignment,' Guided Weapons Technical Memorandum 012, AR-006-607, Department of Defence, Australia, 1992
  2. K. Spalding, 'An efficient rapid transfer alignment filter,' AIAA Paper, pp. 1276-1286, 1992
  3. A. M. Schneider, 'Kalman filter formulations for transfer alignment of strapdown inertial units,' Journal of the INStitute of Navigation, pp. 72-89, vol. 30, no. 1, Spring 1983
  4. C. Y. Zhang, 'Scheme of alignment for strapdown inertial navigation systems', Proceedings of the ICAS, pp. 1304-1310, July, 1992
  5. H. C. Salzwedel and K. M. Kessler, 'Transfer of alignment and calibration of multiple sensors in Flexible Systems,' Proceedings of the 24th CDC, pp. 1932-1937, December, 1985 https://doi.org/10.1109/CDC.1985.268919
  6. J. J. Deyst JR, and A. A. Sutherland JR., 'Strapdown inertial system alignment using statistical filters : A simplified formulation,' AIAA Journal, pp. 452-456, vol. 11, no. 4, November, 1973
  7. D. Goshen-Meskin and I. Y. Bar-Itzheck, 'Observability analysis of inertial navigation systems during in-flight alignment,' AIAA Journal, pp. 1056-1067, vol. 28, no. 41988
  8. D. Goshen-Meskin and I. Y. Bar-Itzhack, 'Observability analysis of piece-wise constant systems-part II : Application to inertial navigation in-flight alignment,' IEEE Transactions on Aerospace and Electronic Systems, pp. 1068-1075, vol. 28, no. 4, October, 1992 https://doi.org/10.1109/7.165368
  9. Gelb, A.(ed.), Applied Optimal Estimation, M.I.T. Press, Cambridge, Mass., 1974
  10. G. M. Siouris, Aerospace Avionics Systems, Academic Press Inc, 1993
  11. 송기원, 전창배, 김현백, '스크랩다운 관성항법장치의 각을 이용한 초기전달 정렬기법,' '93한국자동제어학술회의논문집, pp. 29-33, 1993
  12. 송기원, 전창배, 김현백, 유준, '수평축 자세운동이 있는 배에서의 전달정렬 알고리즘 설계,' Proceedings of the 11th KACC, pp. 672-675, October, 1996