Cooperation attitude control of multiple spacecraft using sliding mode variable structure

机译：基于滑模变结构的多航天器协同姿态控制

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This paper focuses on the attitude control for multiple spacecraft. Two decentralized finite-time control laws are proposed when the communication topologies are directed and undirected, respectively. The proposed control schemes rely on the information of angular velocity errors and error quaternions of the neighboring spacecraft which determines the orientation of the torques and reduce the relative errors. Finite-time stabilization of the system is proved by using Lyapunov function and graph theory. Finally, simulation examples are illustrated to validate the approach by different case studies.

机译：本文着重于多飞船的姿态控制。当通信拓扑分别是有向的和无向的时，提出了两个分散的有限时间控制律。所提出的控制方案依赖于角速度误差和相邻航天器的误差四元数的信息，该信息确定了转矩的方向并减小了相对误差。利用李雅普诺夫函数和图论证明了系统的有限时间稳定。最后，通过不同的案例研究说明了仿真示例，以验证该方法。

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来源
《2014 International Conference on Mechatronics and Control》|2014年|1828-1833|共6页
会议地点 Jinzhou(CN)
作者
Jie Huang; Qingkai Yang; Xuehui Gao;
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Sch. of Autom., Beijing Inst. of Technol., Beijing, China;

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正文语种 eng
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专利

1. Finite-time cooperative attitude control of multiple spacecraft using terminal sliding mode control technique [J] . Haibo Du, Shihua Li International Journal of Modelling, Identification and Control . 2012,第4期

机译：利用终端滑模控制技术的多航天器有限时间协同姿态控制
2. Characteristic model-based discrete-time sliding mode control for spacecraft with variable tilt of flexible structures [J] . Chen Lei, Yan Yan, Mu Chaoxu, Automatica Sinica, IEEE/CAA Journal of . 2016,第1期

机译：基于特征模型的挠性结构可变倾角航天器离散时间滑模控制
3. Characteristic Model-based Discrete-time Sliding Mode Control for Spacecraft with Variable Tilt of Flexible Structures [J] . Lei Chen, Yan Yan, Chaoxu Mu, 自动化学报：英文版 . 2016,第001期

机译：柔性结构可变倾角航天器基于特征模型的离散滑模控制
4. Cooperation attitude control of multiple spacecraft using sliding mode variable structure [C] . Jie Huang, Qingkai Yang, Xuehui Gao International Conference on Mechatronics and Control . 2014

机译：使用滑模变量结构的多个航天器的合作态度控制
5. Variable structure surface design and sliding mode control of modern power electronics. [D] . Khasawneh, Bashar Yusuf. 2014

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7. Attitude-Orbit Cooperative Control for Small-Scale Spacecraft with Chemical Propulsion: Adaptive Sliding Mode Control Based on Neural Network [O] . Guogang Wang, Keping Liu, Zhongbo Sun, 2020

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8. Variable Structure Attitude Control and Elastic Mode Stabilization of Flexible Spacecraft. [R] . Iyer, A., Singh, S. 1989

机译：柔性航天器的变结构姿态控制与弹性模态稳定。

Cooperation attitude control of multiple spacecraft using sliding mode variable structure

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