@inproceedings{a02dafdeca2e4b82b360f2ff886d4826,
title = "Nonsingular terminal sliding mode control for approach to non-cooperative satellite",
abstract = "The problem of final approach to a non-cooperative tumbling target is researched in this paper. The accurate orbit and attitude dynamics model of two relative motion spacecrafts with arbitrary eccentrics is established. The traditional linear synchronization rotating approach strategy is improved by designing exponential decay reference trajectory to insure the safety of final approach. The nonsingular terminal sliding mode control law is designed. The stability of the control law is demonstrated via a Lyapunov analysis and effectiveness of controller is verified by the numerical simulation.",
keywords = "Attitude Control, Non-cooperative Target, Relative Motion, Space Rendezvous, Terminal Sliding Mode Control",
author = "Hailong Liu and Xiaoping Shi and Long Li and Jing Yang",
note = "Publisher Copyright: {\textcopyright} 2015 IEEE.; 27th Chinese Control and Decision Conference, CCDC 2015 ; Conference date: 23-05-2015 Through 25-05-2015",
year = "2015",
month = jul,
day = "17",
doi = "10.1109/CCDC.2015.7162161",
language = "英语",
series = "Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1524--1529",
booktitle = "Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015",
address = "美国",
}