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Full Length Article | Open Access

Startup drift compensation of RLG based on monotone constrained RBF neural network

Songlai HANa, Mingcun ZHAOa, Xuesong LIUa, Xuecong LIUb( )
Research Institute of Aerospace Technology, Central South University, Changsha 410083, China
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China

Peer review under responsibility of Editorial Committee of CJA

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Abstract

Serious startup drift of the Ring Laser Gyroscope (RLG) is observed during cold startup process, which will dramatically degrade the performances of the corresponding Inertial Navigation System (INS). In this paper, correlation analysis method, which analyzes the relationship between the startup drift of the RLG and the temperature change, is used to determine the significant temperature-related terms during gyroscope startup. Based on the significant temperature-related terms and the startup time length, a startup drift compensation model for RLG based on monotonicity-constrained Radial Basis Function (RBF) neural network is proposed and validated. Compared with the raw RLG data without compensation, the standard deviation of the RLG output with the proposed constrained RBF network model is decreased by more than 46%, and the peak-to-peak value is decreased by more than 35%. Compared with the traditional multiple regression model, the standard deviation and peak-to-peak value of the RLG output are decreased by more than 10% and 6%, respectively. Compared with the common RBF network model, the standard deviation and peak-to-peak value of the RLG output are decreased by more than 8% and 3%, respectively. Navigation experiments also validate the effectiveness of the compensation model.

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Chinese Journal of Aeronautics
Pages 355-365

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Cite this article:
HAN S, ZHAO M, LIU X, et al. Startup drift compensation of RLG based on monotone constrained RBF neural network. Chinese Journal of Aeronautics, 2024, 37(11): 355-365. https://doi.org/10.1016/j.cja.2024.08.022

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Received: 24 September 2023
Revised: 04 January 2024
Accepted: 04 July 2024
Published: 22 August 2024
© 2024 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).