DocumentCode :
2251591
Title :
A fractional order sliding mode controller design for spacecraft attitude control system
Author :
Tianyi, Zeng ; Xuemei, Ren ; Yao, Zhang
Author_Institution :
Beijing Institute of Technology, Beijing 100081, China
fYear :
2015
fDate :
28-30 July 2015
Firstpage :
3379
Lastpage :
3382
Abstract :
As fractional order sliding mode controller has its unique advantages, it has been widely studied in recently years. This paper will discuss about the fractional order sliding mode controller and design a controller which is used into the spacecraft attitude system so that it can be with more quickness and strong robustness. A new sliding mode surface is proposed and it is proved that the system can be stable and can convergence in a finite time under this sliding mode surface. Simulation results show that this method can make the spacecraft attitude system has better performance.
Keywords :
Attitude control; Convergence; Fractional calculus; Robustness; Simulation; Sliding mode control; Space vehicles; Fractional order; sliding mode control; spacecraft attitude control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2015 34th Chinese
Conference_Location :
Hangzhou, China
Type :
conf
DOI :
10.1109/ChiCC.2015.7260160
Filename :
7260160
Link To Document :
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