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Random Noise Suppression Method for Inertial Sensors Based on Complexing an AR Model and Adaptive SRUKF Kalman Filter under the PINS Alignment on a Stationary Platform

https://doi.org/10.32603/1993-8985-2023-26-2-101-119

Abstract

Introduction. In the gyrocompassing mode, the initial heading angle of a platformless inertial navigation system (PINS) is determined based on the data obtained from accelerometers and gyroscopes that measure the projections of the gravitational acceleration vector and the Earth’s angular velocity vector on the axes of the body coordinates system in the PINS initial stationary mode. Due to unavoidable circumstances, such as bias instability and random noise in the accelerometer and gyroscope signals, much time is required to obtain the sufficient amount of sensor data for achieving the necessary accuracy of useful measurement values by the averaging method. In this context, in order to reduce the time of the gyrocompassing mode, data processing methods should be used to eliminate the bias instability and random noise in the signals received from PINS inertial sensors.
Aim. To develop a method for suppressing random noise and reducing bias instability in the signals of inertial sensors, thereby reducing the time of the gyrocompassing mode of PINS and providing for the required accuracy of its initial heading angle determination.
Materials and methods. An autoregressive (AR) model was used to simulate random noise in the measured sensor signals followed by its filtering using a Sage-window square-root unscented Kalman filter (SW-SRUKF).
Results. A mathematical model describing random noise in the PINS inertial sensors in the stationary mode was derived. A methodology for suppressing random noise was proposed. The effectiveness of the proposed method was tested on actual data, with the results presented in the form of figures and tables.
Conclusion. A method for eliminating the bias instability and random noise of PINS accelerometers and gyroscopes was proposed based on AR model and SW-SRUKF. The accuracy and effectiveness of the proposed method was confirmed by processing actual inertial sensor data. The results obtained are significant for reducing the initial alignment time of a PINS in the gyrocompassing mode.

About the Authors

Trong Yen Nguyen
Le Quy Don Technical University
Viet Nam

Nguyen Trong Yen, Master in Instrumentation Engineering and Navigation, Stabilization and Orientation Systems (2014), Postgraduate student. The author of 10 scientific publications. Area of expertise: inertial navigation and orientation systems.

Ha Noi, Bac Tu Liem, Co Nhue, 236



Quoc Khanh Nguyen
Le Quy Don Technical University
Viet Nam

Nguyen Quoc Khanh, Engineer in Instrumentation Engineering (2020), Postgraduate student. The author of 3 scientific publications. Area of expertise: inertial navigation and orientation systems. 

Ha Noi, Bac Tu Liem, Co Nhue, 236



Van Khoi Nguyen
Academy of Science and Technology
Viet Nam

Nguyen Van Khoi, PhD (Eng.) (2014), Employee of the Department of Airborne Management System. The author of 9 scientific publications. Area of expertise: control systems of technical processes and productions.

Ha Noi, Cau Giay, Hoang Sam, 17



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For citations:


Nguyen T., Nguyen Q., Nguyen V. Random Noise Suppression Method for Inertial Sensors Based on Complexing an AR Model and Adaptive SRUKF Kalman Filter under the PINS Alignment on a Stationary Platform. Journal of the Russian Universities. Radioelectronics. 2023;26(2):101-119. (In Russ.) https://doi.org/10.32603/1993-8985-2023-26-2-101-119

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ISSN 1993-8985 (Print)
ISSN 2658-4794 (Online)