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
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