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