Error Characteristic Analysis of Tri-axis Rotating Optical Gyro Inertial Navigation System Based on Inertial Frame

Author:

Fan Huiying,Tian Kaiwen,Cheng Guangxin,Dong Zhuangzhuang,Yu Xudong

Publisher

Springer Nature Singapore

Reference10 articles.

1. B. Yuan, G. Rao, On the theory of optical gyro rotating inertial navigation system. J. Natl. Univ. Def. Technol. 28(6), 76–80 (2006)

2. X. Yu, Y. Wang, P. Zhang et al., Influence of single-axial rotation on INS error characteristics. J. Chin. Inertial Technol. 16(6), 643–648 (2008)

3. Y. Yang, L. Miao, Fiber-optic strapdown inertial system with sensing cluster continuous rotation. IEEE Trans. Aerosp. Electron. Syst 40(4), 1173–1178 (2004)

4. E. Levinson, R. Majure, Accuracy enhancement techniques applied to the marine ring laser inertial navigator (MARLIN). Navigation 34(1), 64–86 (1987)

5. H. Lei, X. Wang, F. Liu, Analysis on error characteristics and key technology of airborne double-axis rotation-modulating RLG INS. Navig. Position. Timing 3(4), 13–18 (2016)

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