DocumentCode
581661
Title
Adaptive block dynamic surface control of BTT missiles
Author
Mingzhe, Hou ; Haoming, Du ; Feng, Tan ; Canghua, Jiang
Author_Institution
Center for Control Theor. & Guidance Technol., Harbin Inst. of Technol., Harbin, China
fYear
2012
fDate
25-27 July 2012
Firstpage
882
Lastpage
886
Abstract
This paper proposes a novel adaptive block dynamic surface control algorithm for BTT missiles. The control system model of BTT missiles is reconstructed into the block strict-feedback form with matched and unmatched uncertainties. Under the assumption that the uncertainties are norm-bounded, an adaptive block dynamic surface control algorithm is proposed for such a time-varying nonlinear systems. It is proved that the attitude angles can be driven to track the desired trajectory with expected precision and all the states are kept bounded simultaneously by choosing proper design parameters. The simulation results show the effectiveness of the proposed method.
Keywords
adaptive control; aircraft control; feedback; missile control; nonlinear control systems; time-varying systems; uncertain systems; BTT missile; adaptive block dynamic surface control; aircraft control; attitude angle; bank-to-turn technique; block strict-feedback form; design parameters; matched uncertainty; norm-bounded uncertainty; time-varying nonlinear system; trajectory tracking; unmatched uncertainty; Adaptive systems; Aerodynamics; Heuristic algorithms; Missiles; Nonlinear dynamical systems; Uncertainty; Vehicle dynamics; Adaptive Control; BTT Missile; Block Dynamic Surface Control; Nonlinear system;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2012 31st Chinese
Conference_Location
Hefei
ISSN
1934-1768
Print_ISBN
978-1-4673-2581-3
Type
conf
Filename
6390049
Link To Document