Title :
Observer-based H-infinity tracking control design for a linearized hypersonic vehicle model with external disturbance
Author :
Zhifeng Gao ; Teng Cao ; Jinxing Lin ; Moshu Qian
Author_Institution :
Coll. of Autom., Nanjing Univ. of Posts & Telecommun., Nanjing, China
Abstract :
In this study, the H-infinity tracking control problem of a linearized hypersonic vehicle model with the bounded external disturbance is investigated. Firstly, the nonlinear longitudinal dynamics of hypersonic vehicle is linearized as a linear time-invariant system with the bounded external disturbance, a reference model is introduced for the aim of tracking control. And then an observer-based output feedback tracking controller design approach is proposed by using the linear matrix inequalities (LMIs) technique. The asymptotical stability of the closed-loop system is analyzed in the framework of Lyapunov method. Finally, the simulation results are given to illustrate the applicability of the developed control approach.
Keywords :
H∞ control; Lyapunov methods; aircraft control; asymptotic stability; closed loop systems; control system synthesis; feedback; linear matrix inequalities; linear systems; nonlinear control systems; observers; LMI technique; Lyapunov method; asymptotical stability analysis; bounded external disturbance; closed-loop system; controller design approach; linear matrix inequalities; linear time-invariant system; linearized hypersonic vehicle model; nonlinear longitudinal dynamics; observer-based H-infinity tracking control design; observer-based output feedback tracking controller; tracking control; Aerodynamics; Linear matrix inequalities; Mathematical model; Output feedback; Vehicle dynamics; Vehicles;
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
DOI :
10.1109/CGNCC.2014.7007436