Citation: | ZUO Kai, ZHONG Mai-ying, LIU Bai-qi, GONG Xiao-lin. Adaptive SINS/GPS Outlier Detection and Accommodation Using Innovation Orthogonal[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2010, 19(4): 427-431. |
[1] |
Qin Yongyuan. Inertia navigation[M]. Beijing: Science Press, 2005. (in Chinese)
|
[2] |
Fang J, Ning X. Celestial navigation and its application[M]. Beijing: Beihang University Press, 2006. (in Chinese)
|
[3] |
Fu M, Deng Z. Kalman filtering theory and application in satellite navigation system[M]. Beijing: Science Press, 2003. (in Chinese)
|
[4] |
Liu B. Study on SINS/GPS for motion compensation of high resolution real-time airborne SAR . Beijing: Beihang University, 2008. (in Chinese)
|
[5] |
Kim K H, Lee J G, Park C G. Adaptive two-stage extended Kalman filter for a fault-tolerant INS-GPS loosely coupled system[J]. IEEE Trans on Aerospace and Electronic Systems, 2009,45(1):125-137.
|
[6] |
Liu H, Yao Y, Lu D, et al. Study for outliers based on Kalman filtering[J]. Electric Mattress and Control, 2003,7(1):40-42.
|
[7] |
Gong X. Research on the filtering methods and experiments of SINS/GPS for imaging of airborne earth observation . Beijing: Beihang University, 2009. (in Chinese)
|
[8] |
Zhu Z, Qiu H, Li J, et al. Identification and elimination of outliers in dynamic measurement data[J]. Systems Engineering and Electronics, 2004,26(2):147-149.
|
[9] |
Wang G, Zhang S, Yang R. An adaptive outlier algorithm based on Kalman filtering for Beidou satellite passive combination[J]. J Electronics and Information Technology, 2008,30(8):1981-1984.
|