Stable Spinning Deployment Control of a Triangle Tethered Formation System

被引:17
作者
Zhang, Fan [1 ]
Zhou, He [1 ]
Huang, Panfeng [1 ]
Guo, Jian [2 ]
机构
[1] Northwestern Polytech Univ, Sch Astronaut, Natl Key Lab Aerosp Flight Dynam, Res Ctr Intelligent Robot, Xian 710072, Peoples R China
[2] Delft Univ Technol, Fac Aerosp Engn, NL-2600 AA Delft, Netherlands
基金
中国国家自然科学基金;
关键词
Spinning; Space vehicles; Orbits; Mathematical model; Space missions; Space stations; Sliding mode control; Stable and spinning deployment; tethered satellites system; triangle formation; SLIDING-MODE CONTROL;
D O I
10.1109/TCYB.2021.3074981
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The tethered formation system has been widely studied due to its extensive use in aerospace engineering, such as Earth observation, orbital location, and deep space exploration. The deployment of such a multitethered system is a problem because of the oscillations and complex formation maintenance caused by the space tether's elasticity and flexibility. In this article, a triangle tethered formation system is modeled, and an exact stable condition for the system's maintaining is carefully analyzed, which is given as the desired trajectories; then, a new control scheme is designed for its spinning deployment and stable maintenance. In the proposed scheme, a novel second-order sliding mode controller is given with a designed nonsingular sliding-variable. Based on the theoretical proof, the addressed sliding variable from the arbitrary initial condition can converge to the manifold in finite time, and then sliding to the equilibrium in finite time as well. The simulation results show that compared with classic second sliding-mode control, the proposed scheme can speed up the convergence of the states and sliding variables.
引用
收藏
页码:11442 / 11452
页数:11
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