Issue |
MATEC Web Conf.
Volume 198, 2018
2018 Asia Conference on Mechanical Engineering and Aerospace Engineering (MEAE 2018)
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Article Number | 06003 | |
Number of page(s) | 4 | |
Section | Satellite Engineering and Space Communication | |
DOI | https://doi.org/10.1051/matecconf/201819806003 | |
Published online | 12 September 2018 |
Research on Shape Remain of Near-Earth Radial Collinear 4-Craft Coulomb Formation
2222 Nanhu Road, Changchun City, Jilin Province, China
This paper investigates the non-linear relative kinetic model of the collinear 4-craft Coulomb formation in geostationary orbit. Considering the fact that the formation remains statically fixed in the radial direction, using the equilibrium conditions to linearize the dynamic model. To keep the radial static stability of the collinear 4-craft Coulomb formation, the LQR controller is designed based on the linear dynamic model, taking the Coulomb force as the only control force. Considering the unmodeled disturbance force and the model error, the improved LQR control law is designed to improve the robustness of the traditional LQR controller. Simulation is executed by Matlab/Simulink, and numerical simulation results demonstrate the effectiveness of the dynamic model and the proposed control strategy.
© The Authors, published by EDP Sciences, 2018
This is an open access article distributed under the terms of the Creative Commons Attribution License 4.0 (http://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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