DocumentCode :
2671812
Title :
Application of sliding mode control based on dmc in guidance control system
Author :
Jia, Lei ; Xiuyun, Meng
Author_Institution :
Sch. of Aerosp. Eng., Beijing Inst. of Technol., Beijing, China
Volume :
2
fYear :
2010
fDate :
27-29 March 2010
Firstpage :
556
Lastpage :
559
Abstract :
In this paper, a new control strategy is applied in guidance control system. It obtains the control law with predicting the sliding surface which designed in sliding mode control. This technique is called predictive sliding mode control. It acquires the robustness feature of sliding mode control and the good performance of predictive control. Finally, simulation results are provided to show the effectiveness of the proposed method.
Keywords :
aircraft control; control system synthesis; predictive control; variable structure systems; dynamic matrix control; guidance control system; predictive control; sliding mode control; sliding surface; Aerospace engineering; Control system synthesis; Control systems; Optimal control; Predictive control; Predictive models; Robust control; Sliding mode control; Switches; Uncertainty; DMC; guidance control system; predictive control; sliding mode control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Advanced Computer Control (ICACC), 2010 2nd International Conference on
Conference_Location :
Shenyang
Print_ISBN :
978-1-4244-5845-5
Type :
conf
DOI :
10.1109/ICACC.2010.5486705
Filename :
5486705
Link To Document :
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