The Error Analysis Caused by Accelerometer Drifs to the Rate Azimuth Platform Inertial System

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Abstract:

To know the influence of deterministic system error to navigation system well, so the precision index of gyroscopes and accelerometers, which are the main components of rate azimuth platform inertial navigation system, and initial calibration precision, can be put forward. Based on the error equations, the characteristic equation of rate azimuth platform inertial system is established, and the solutions of the error equation under static state are obtained with analytical method, and the system error characteristics caused by the accelerometer drifts are analyzed.

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595-600

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December 2011

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© 2012 Trans Tech Publications Ltd. All Rights Reserved

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[1] CaiTijing, G. I. Emeliantsev, Study on rate azimuth platform inertial navigation system[J], Journal of Southeast University (English Edition), 2005, 121(1): 29-32.

Google Scholar

[2] ZHANG Tao, XU Xiao-su, Azimuth strapdown inertial navigation Platform system and error analysis[J], Journal of Chinese Inertial Technology, 2006, 14(5): 5-8(in Chinese).

Google Scholar

[3] WANG Feng-lin, CAI Ti-jing, LUO Bin, Rate Azimuth Inertial Platform/GPS/Log Integrated Navigation System[J], Journal of Chinese Inertial Technology, 2005, 13(2): 35-40(in Chinese).

Google Scholar

[4] Yuan Xing, Yu Ji-xian, Chen Zhe, Navigation System[M], Aviation industry press, 1992: 50-52. (in Chinese).

Google Scholar