@inproceedings{823f7e5b78e84c9999236831e1944717,
title = "Coupled Attitude And Orbit Control For Spacecraft Based On Fast Nonsingular Terminal Sliding Mode Without Dual Velocity Information",
abstract = "In order to solve the coupled attitude and orbit control problem of spacecraft, a novel terminal sliding mode controller is proposed in this paper. The relative dynamic model coupling the translational and rotational motion is established by using dual quaternion. To deal with the problem of unmeasurable dual velocity information, a dual velocity observer is designed based on the extended state observer. The finite-time stability of the controller and observer is proven by the Lyapunov stability theory. The simulation result shows that the proposed method is effective.",
keywords = "Coupled attitude and orbit, dual quaternion, dual velocity observer, fast nonsingular terminal sliding mode",
author = "Junyu Li and Ying Zhang and Rui Zhang",
note = "Publisher Copyright: {\textcopyright} 2022 Technical Committee on Control Theory, Chinese Association of Automation.; 41st Chinese Control Conference, CCC 2022 ; Conference date: 25-07-2022 Through 27-07-2022",
year = "2022",
doi = "10.23919/CCC55666.2022.9901524",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "558--563",
editor = "Zhijun Li and Jian Sun",
booktitle = "Proceedings of the 41st Chinese Control Conference, CCC 2022",
address = "美国",
}