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http://dx.doi.org/10.5139/JKSAS.2018.46.11.921

A Study on Error Analysis of Dual-Axis Rotational Inertial Navigation System Based on Ring Laser Gyroscope  

Kim, Cheon-Joong (Agency for Defence Development)
Yu, Hae-Sung (Agency for Defence Development)
Lee, In-Seop (Agency for Defence Development)
Oh, Ju-Hyun (Agency for Defence Development)
Lee, Sang-Jeong (Chungnam National University)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.46, no.11, 2018 , pp. 921-933 More about this Journal
Abstract
There is a method to enhance the pure navigation performance of INS(Inertial Navigation System) through the rotation of inertial measurement unit to compensate error sources of inertial sensors each other and that INS using this principle of operation is called rotational INS. In this paper, the exact error analysis of rotational INS based on ring laser gyro considering the coupling effect with gravity and earth rate is performed to evaluate the navigation performance by inertial sensor error sources. And error analysis and performance evaluation result confirmed by modelling and simulation is also proposed in this paper.
Keywords
Rotational Inertial Navigation System; Error Analysis; Performance Analysis; Ring Laser Gyro;
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