A fast initial alignment method for strapdown inertial navigation system on stationary base

IEEE Transactions on Aerospace and Electronic Systems

Volumn 32, Issue 4, 1996, Pages 1501-1505

  Cheng, Jiang ^a   De Wan, Fang Jun ^a  

^a SOUTHEAST UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER AIDED ANALYSIS; COMPUTER SIMULATION; ERROR ANALYSIS; MATHEMATICAL MODELS; PARAMETER ESTIMATION;

ALIGNMENT METHODS; ERROR AZIMUTHS; STRAPDOWN INERTIAL NAVIGATION SYSTEM;

INERTIAL NAVIGATION SYSTEMS;

EID: 0030258958     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/7.543871     Document Type: Article

References (6)

1. Lee, J. G., Park, C. G., and Park, H. W. (1993) Multiposition alignment of strapdown ineitial navigation system. IEEE Transactions on Aerospace and Electronic Systems, 29, 4 (Oct. 1993), 1323-1328.
2. Jiang, Y. K, and Lin, Y. P. (1992) Error estimation of INS ground alignment through observability analysis, IEEE Transactions on Aerospace and Electronic. Systems, 28, 1 (Jan. 1992), 92-97.
3. Bar-Itzhack, I. Y, and Berman, N. (1988) Control theoretic approach to inertial navigation systems. Journal of Guidance and Control, 11, 3 (May-June 1988), 237-245.
4. Meskin, D. G., and Bar-Itzhack, I. Y. (1992) Observability analysis of piece-wise constant systems-Part II: Application to inertial navigation in-flight alignment. IEEE Transactions on Aerospace and Electronic Systems, 28, 4 (Oct. 1992), 1068-1075.
5. Yuan, X., Yu, J. X., and Chen, Z. (1993) Navigation Systems. Beijing: Aeronautic Industry Press, 1993.
6. Siouris, G. M. (1993) Aerospace Avionics Systems: A Modern Synthesis. New York: Academic Press, 1993.