Rotating Lorentz Force Magnetic Bearings’ Dynamics Modeling and Adaptive Controller Design
Author:
Chen Feiyu1, Wang Weijie2, Wang Shengjun2
Affiliation:
1. Graduate School, Space Engineering University, Beijing 101400, China 2. Department of Aerospace Science and Technology, Space Engineering University, Beijing 101400, China
Abstract
To address the issues of our agile satellites’ poor attitude maneuverability, low pointing stability, and pointing inaccuracy, this paper proposes a new type of stabilized platform based on seven-degree-of-freedom Lorentz force magnetic levitation. Furthermore, in this study, we designed an adaptive controller based on the RBF neural network for the rotating magnetic bearing, which can improve the pointing accuracy of satellite loads. To begin, the advanced features of the new platform are described in comparison with the traditional electromechanical platform, and the structural characteristics and working principle of the platform are clarified. The significance of rotating magnetic bearings in improving load pointing accuracy is also clarified, and its rotor dynamics model is established to provide the input and output equations. The adaptive controller based on the RBF neural network is designed for the needs of high accuracy of the load pointing, high stability, and strong robustness of the system, and the current feedback inner loop is added to improve the system stiffness and rapidity. The final simulation results show that, when compared to the PID controller and robust sliding mode controller, the controller’s pointing accuracy and anti-interference ability are greatly improved, and the system robustness is strong, which can effectively improve the pointing accuracy and pointing stability of the satellite/payload, as well as provide a powerful means of solving related problems in the fields of laser communication, high score detection, and so on.
Funder
National Natural Science Foundation of China
Subject
Electrical and Electronic Engineering,Biochemistry,Instrumentation,Atomic and Molecular Physics, and Optics,Analytical Chemistry
Reference22 articles.
1. Tan, Z., Luo, R., Li, J., Ling, Q., and Liang, J. (2018, January 14–16). Process Analysis and Visual Interpretation Platform Design for Agile Satellite Dynamic Imaging. Proceedings of the 2018 IEEE 4th Information Technology and Mechatronics Engineering Conference (ITOEC), Chongqing, China. 2. Qu, Z., Jia, H., Xu, K., He, X., Yang, F., Li, F., and Liu, M. (2020, January 1–3). Reconfigurability Analysis of Distributed Control Moment Gyro for Jilin-1 Super Agile Satellite. Proceedings of the 2020 3rd International Conference on Electron Device and Mechanical Engineering (ICEDME), Suzhou, China. 3. Wen, W. (2016). Research on Attitude Maneuvering Planning Method of Agile Satellite. [Ph.D. Thesis, Harbin Engineering University]. 4. Li, Y. (2016). Study on Key Technology of Image Motion Compensation of Agile Satellite Camera. [Ph.D. Thesis, University of Chinese Academy of Sciences]. 5. Qu, Z. (2021). Research on Attitude Maneuver and Stability Control Algorithm of Hyper-Agile Satellite, Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences.
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