Electronics Optics & Control, Volume. 23, Issue 6, 40(2016)
A Complete Integrated Attitude Measuring System of Multi-antenna GPS/SINS and Its Observability Analysis
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[2] [2] GOSHEN-MESKIN D,BAR-ITZHACK I Y. Observability analysis of piece-wise constant systems(partⅡ):application to inertial navigation in-flight alignment [J]. IEEE Transactions on Aerospace and Electronic Systems,1992,28(4):1068-1075.
[6] [6] HU X M, LIU F, WENG H N. Observability analysis of MSINS/SINS complete integrated system[J]. Journal of Chinese Inertial Technology, 2011, 19(1): 38-45.
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HE Hao, YANG Dong-fang, ZHENG Yu-hang, ZHANG Jin-sheng, WANG Shi-cheng. A Complete Integrated Attitude Measuring System of Multi-antenna GPS/SINS and Its Observability Analysis[J]. Electronics Optics & Control, 2016, 23(6): 40
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Received: Jun. 10, 2015
Accepted: --
Published Online: Jan. 28, 2021
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