Micro-Thrust, Low-Fuel Consumption, and High-Precision East/West Station Keeping Control for GEO Satellites Based on Synovial Variable Structure Control
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Published:2023-01-30
Issue:3
Volume:11
Page:705
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ISSN:2227-7390
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Container-title:Mathematics
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language:en
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Short-container-title:Mathematics
Author:
Liu Fucheng1, Ye Lijun234, Liu Chunyang34ORCID, Wang Jingji34, Yin Haining34
Affiliation:
1. Shanghai Academy of Spaceflight Technology, Shanghai 201109, China 2. School of Aerospace Engineering, Tsinghua University, Beijing 100084, China 3. Shanghai Key Laboratory of Aerospace Intelligent Control Technology, Shanghai 201109, China 4. Shanghai Aerospace Control Technology Institute, Shanghai 201109, China
Abstract
Aiming at the shortcomings of non-optimal fuel consumption and low accuracy of Geosynchronous orbit (GEO) satellites in the east/west station keeping (EWSK) at the current stage, a micro-thrust EWSK algorithm for GEO satellites based on a single-synovial surface is proposed. This algorithm has the characteristics of low fuel consumption and high control precision. However, when this algorithm performs GEO station switching under the condition of limited velocity increment, the mean longitude capture path may not be optimal, the capture time of the mean longitude is too long, and the engineering applicability is not good. In view of the above problems, a micro-thrust EWSK for GEO satellites based on dual synovial surfaces is proposed. Through the advance planning of the mean longitude, the control lag caused by the limited velocity increment is eliminated, the optimal path-planning problem of the mean longitude is solved, and the capture time of the mean longitude is greatly shortened. The two EWSK algorithms proposed in this paper have the advantages of small calculation amount, optimal fuel consumption, high precision and strong stability, which have good engineering application value.
Funder
National Nature Science Foundation of China
Subject
General Mathematics,Engineering (miscellaneous),Computer Science (miscellaneous)
Reference20 articles.
1. Chao, C.C. (2005). Applied Orbit Perturbation and Maintenance, The Aerospace Press. 2. Wang, Z.C., Xing, G.H., and Zhang, H.W. (1999). Handbook of Geostationary Orbits, National Defense Industry Press. 3. Ye, L., Liu, C., Zhu, W., Yin, H., Liu, F., and Baoyin, H. (2022). North/south Station Keeping of the GEO Satellites in Asymmetric Configuration by Electric Propulsion with Manipulator. Mathematics, 10. 4. Possner, M.P., Almendra, M., and Garcia, G. (2008, January 9–11). A New Flight Dynamics Solution for Operations of the Boeing 702 Satellite. Proceedings of the AIAA Space 2008 Conference & Exposition, San Diego, CA, USA. 5. Feuerborn, S.A., Neary, D.A., and Perkins, J.M. (2013, January 14–17). Finding a way: Boeing’s All Elecric Propulsion Satellite. Proceedings of the 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, USA.
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