DocumentCode :
596750
Title :
Fuzzy Sliding Mode Control design for reusable launch vehicles
Author :
Jing Peng ; Xin Qu ; Zhang Ren
Author_Institution :
Sci. & Technol. on Aircraft Control Lab., Beihang Univ. (BUAA), Beijing, China
fYear :
2012
fDate :
18-20 Oct. 2012
Firstpage :
1053
Lastpage :
1056
Abstract :
This paper presents a Fuzzy Sliding Mode Control method for Reusable Launch Vehicles (RLV) in re-entry stage. RLV is a good measure to reduce transportation costs and improve launch vehicle performance effectively. The major contributions of this paper are as follows. Firstly, the non-linear mathematical model of reusable launch vehicle is introduced. And its characteristics are analyzed. Then, an attitude controller is designed by a combination of sliding mode control technology with fuzzy control technology. Finally, the simulations were performed based on the presented mathematical model and the designed controller.
Keywords :
attitude control; control system synthesis; fuzzy control; space vehicles; transportation; variable structure systems; attitude controller design; fuzzy sliding mode control design; launch vehicle performance improvement; nonlinear mathematical model; reentry stage; reusable launch vehicle; transportation cost reduction; Aerodynamics; Aerospace control; Fuzzy logic; Mathematical model; Niobium; Sliding mode control; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Advanced Computational Intelligence (ICACI), 2012 IEEE Fifth International Conference on
Conference_Location :
Nanjing
Print_ISBN :
978-1-4673-1743-6
Type :
conf
DOI :
10.1109/ICACI.2012.6463333
Filename :
6463333
Link To Document :
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