DocumentCode
724166
Title
Robust velocity and height control for uncertain hypersonic vehicles
Author
Yu Lingyi ; Li Zhaoying ; Liu Hao ; Yu Yao
Author_Institution
Sch. of Astronaut., Beihang Univ., Beijing, China
fYear
2015
fDate
23-25 May 2015
Firstpage
2297
Lastpage
2302
Abstract
This paper presents a robust controller design approach for the longitudinal dynamics of hypersonic vehicles. The proposed linear and time-invariant controller includes a state feedback H∞ controller and a robust compensator. The robust compensator is introduced to restrain the effects of nonlinear dynamics and unstructured uncertainties in the whole frequency range. It is proven that the velocity and height tracking errors can be guaranteed to converge to the neighborhood of the origin in a finite time. Simulation results are given to show the advantages of the proposed control method.
Keywords
H∞ control; aircraft control; compensation; control system synthesis; linear systems; nonlinear dynamical systems; robust control; state feedback; uncertain systems; velocity control; height control; height tracking errors; linear controller; longitudinal dynamics; nonlinear dynamics; robust compensator; robust controller design; robust velocity control; state feedback H∞ controller; time-invariant controller; uncertain hypersonic vehicles; unstructured uncertainties; velocity errors; Robust control; Robustness; State feedback; Uncertainty; Vehicle dynamics; Vehicles; H∞ control; Hypersonic vehicle; nonlinear system; robust control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2015 27th Chinese
Conference_Location
Qingdao
Print_ISBN
978-1-4799-7016-2
Type
conf
DOI
10.1109/CCDC.2015.7162304
Filename
7162304
Link To Document