@inproceedings{d300c67cfc794099bddbc20dc34ad10d,
title = "Finite-time Output Feedback Attitude Control for Double Tethered Satellite System in Deep Space",
abstract = "This paper addresses the problem of finite-time output feedback decentralized control of double tethered satellite system (2-TSS) attitude tracking in the presence of external disturbances in deep space. More specifically, the finite-time attitude tracking control law with the reconstructed information achieving from the pseudo-angular velocity filter is proposed in this paper. The significant feature of proposed strategy is that the whole closed-loop control system can be guaranteed theoretically to be finite-time stable by the development of adding a power integrator method, which indicates that the tracking errors for 2-TSS are confronted into a small residual region around origin within finite time. Finally, numerical simulation analysis is presented to validate the effectiveness and feasibility of proposed scheme.",
keywords = "2-TSS, adding a power integrator method, attitude control, finite time, output feedback",
author = "Mingmin Liu and Junyu Yao and Qinglei Hu",
note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 31st Chinese Control and Decision Conference, CCDC 2019 ; Conference date: 03-06-2019 Through 05-06-2019",
year = "2019",
month = jun,
doi = "10.1109/CCDC.2019.8833210",
language = "英语",
series = "Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1938--1942",
booktitle = "Proceedings of the 31st Chinese Control and Decision Conference, CCDC 2019",
address = "美国",
}