A Suppression Method for Random Errors of IFOG Based on the Decoupling of Colored Noise-Spectrum Information

Uloženo v:
Podrobná bibliografie
Vydáno v:Micromachines vol. 16, no. 8 (2025), p. 963-984
Hlavní autor: Liang Zhe
Další autoři: Zhang, Zhili, Zhou Zhaofa, Li, Hongcai, Zhao Junyang, Tian Longjie, Duan, Hui
Vydáno:
MDPI AG
Témata:
On-line přístup:Citation/Abstract
Full Text + Graphics
Full Text - PDF
Tagy: Přidat tag
Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!

MARC

LEADER 00000nab a2200000uu 4500
001 3244047979
003 UK-CbPIL
022 |a 2072-666X 
024 7 |a 10.3390/mi16080963  |2 doi 
035 |a 3244047979 
045 2 |b d20250101  |b d20251231 
084 |a 231537  |2 nlm 
100 1 |a Liang Zhe  |u Intelligent Control Laboratory, PLA Rocket Force University of Engineering, Xi’an 710025, China 
245 1 |a A Suppression Method for Random Errors of IFOG Based on the Decoupling of Colored Noise-Spectrum Information 
260 |b MDPI AG  |c 2025 
513 |a Journal Article 
520 3 |a In high-precision inertial navigation systems, suppressing the random errors of a fiber-optic gyroscope is of great importance. However, the traditional rule-based autoregressive moving average modeling method, when applied in Kalman filtering considering colored noise, presents inherent disadvantages in principle, including inaccurate state equations and difficulties in state dimension expansion. To this end, the noise characteristics in the fiber-optic gyroscope signal are first deeply analyzed, a random error model form is clarified, and a new model-order determination criterion is proposed to achieve the high-precision modeling of random errors. Then, based on the effective suppression of the angle random walk error of the fiber-optic gyroscope, and combined with the linear system equation of its colored noise, an adaptive Kalman filter based on noise-spectrum information decoupling is designed. This breaks through the principled limitations of traditional methods in suppressing colored noise and provides a scheme for modeling and suppressing fiber-optic gyroscope random errors under static conditions. Experimental results show that, compared with existing methods, the initial alignment accuracy of the proposed method based on 5 min data of fiber-strapdown inertial navigation is improved by an average of 48%. 
653 |a Navigation systems 
653 |a Random errors 
653 |a Fiber optic gyroscopes 
653 |a Strapdown inertial navigation 
653 |a Model forms 
653 |a Wavelet transforms 
653 |a Fog 
653 |a Equations of state 
653 |a Modelling 
653 |a Decoupling 
653 |a Random walk 
653 |a Linear systems 
653 |a Noise 
653 |a Autoregressive moving average 
653 |a Methods 
653 |a Algorithms 
653 |a Kalman filters 
653 |a Time series 
653 |a Optics 
653 |a Markov analysis 
653 |a Inertial navigation 
700 1 |a Zhang, Zhili  |u Intelligent Control Laboratory, PLA Rocket Force University of Engineering, Xi’an 710025, China 
700 1 |a Zhou Zhaofa  |u Intelligent Control Laboratory, PLA Rocket Force University of Engineering, Xi’an 710025, China 
700 1 |a Li, Hongcai  |u Intelligent Control Laboratory, PLA Rocket Force University of Engineering, Xi’an 710025, China 
700 1 |a Zhao Junyang  |u Intelligent Control Laboratory, PLA Rocket Force University of Engineering, Xi’an 710025, China 
700 1 |a Tian Longjie  |u Institute of Optics and Electronics, School of Instrumentation Science and Optoelectronics, Engineering, Beihang University, Beijing 100191, China 
700 1 |a Duan, Hui  |u Intelligent Control Laboratory, PLA Rocket Force University of Engineering, Xi’an 710025, China 
773 0 |t Micromachines  |g vol. 16, no. 8 (2025), p. 963-984 
786 0 |d ProQuest  |t Engineering Database 
856 4 1 |3 Citation/Abstract  |u https://www.proquest.com/docview/3244047979/abstract/embedded/7BTGNMKEMPT1V9Z2?source=fedsrch 
856 4 0 |3 Full Text + Graphics  |u https://www.proquest.com/docview/3244047979/fulltextwithgraphics/embedded/7BTGNMKEMPT1V9Z2?source=fedsrch 
856 4 0 |3 Full Text - PDF  |u https://www.proquest.com/docview/3244047979/fulltextPDF/embedded/7BTGNMKEMPT1V9Z2?source=fedsrch