Improved Three-point Correction Model for Inertial Navigation System Based on Measurement Error and Dynamic Detuning Angle

Author:

Wei-xing Xia1,Yu-hao Shan1

Affiliation:

1. Naval Submarine Academy, Nostate, Qingdao

Publisher

ACM Press

Reference7 articles.

1. <Inertial Navigation System> authoring team. Inertial Navigation System[M].Beijing: National Defense Industry Press, 1983.

2. Gao Wei, Shi Hong-yang, Zhang Xin, et a1. Comprehensive correction technology of strapdown inertial navigation system based on position information [J]. Journal of Huazhong Universny of science and Technology (Nature Science Edition), 2014(6): 10l--106.

3. Wang Dong-sheng, Liu Kang, Zhang Hai-feng, et al. one-point comprehensive calibration in gimbaled inertial navigation system based on azimuth rotating modulation technique[J]. Journal of Chinese Inertial Technology, 2017, 25(1): 43--46.

4. Britting K R. Inertial navigation system analysis[M]. New York: John Wiley& Sons Inc, 1971: 132.

5. Xia Wei-xing, Yang Xiao-dong. Shi Wen-ming, et a1. "Loosely Navigating State" Algorithm of INS Two-point Calibration in Horizontal Damping Mode[J]. Journal of Traffic and Transportation Engineering, 2013, 13(2):99--105.

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