Comments and further results on "observability of an integrated GPS/INS during maneuvers"

IEEE Transactions on Aerospace and Electronic Systems

Volumn 46, Issue 3, 2010, Pages 1566-1568

  Wu, Yuanxin ^a   Tang, Yonggang ^b   Zhang, Hongliang ^a  

^a NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY   (China)

^b Guilin Air Force Academy   (China)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 77955605688     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2010.5545211     Document Type: Note

References (5)

1. Rhee, I., Abdel-Hafez, M. F., and Speyer, J. L. Observability of an integrated GPS/INS during maneuvers. IEEE Transactions on Aerospace and Electronic Systems, 40 (2004), 526-535.
2. Rhee, I., Abdel-Hafez, M. F., and Speyer, J. L. Errata: Observability of an integrated GPS/INS during maneuvers. IEEE Transactions on Aerospace and Electronic Systems, 40 (2004), 1421.
3. Rogers, R. M. Applied Mathematics in Integrated Navigation Systems (3rd ed.). AIAA, Reston, VA, 2007.
4. Lee, J. G., Park, C. G., and Park, G.W. Multiposition alignment of strapdown inertial navigation system. IEEE Transactions on Aerospace and Electronic Systems, 29 (1993), 1323-1328.
5. Widnall, W. S. and Grundy, P. A. Inertial navigation system tests having improved observability of error sources. Journal of Aircraft, 13 (1976), 12-21.