@inproceedings{1bc126796779446d9ce53ae3c056b0e5,
title = "Dynamic Sliding Mode Attitude Tracking Control for Flexible Spacecraft",
abstract = "In this paper, the dynamic sliding mode control approach is adopted to design attitude tracking control law for flexible spacecraft. First, the mathematical model of the flexible spacecraft based on attitude errors is constructed. The kinematic equation of the flexible spacecraft is described by error quaternions. Then, by introducing a dynamic switching function, an dynamical sliding mode control law is proposed for the flexible spacecraft to tackle attitude tracking issue. The proposed dynamic sliding mode control law can suppress the chattering raised by the sign function of the traditional sliding mode control law. Finally, a numerical example is employed to verify the effectiveness of the presented control law.",
keywords = "attitude tracking, dynamic sliding mode control, flexible spacecraft",
author = "Dong, \{Rui Qi\} and Xi Dong and Wu, \{Ai Guo\} and Ying Zhang",
note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 28th IEEE International Symposium on Industrial Electronics, ISIE 2019 ; Conference date: 12-06-2019 Through 14-06-2019",
year = "2019",
month = jun,
doi = "10.1109/ISIE.2019.8781505",
language = "英语",
series = "IEEE International Symposium on Industrial Electronics",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "509--514",
booktitle = "Proceedings - 2019 IEEE 28th International Symposium on Industrial Electronics, ISIE 2019",
address = "美国",
}