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
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;
Conference_Titel :
Control and Decision Conference (CCDC), 2015 27th Chinese
Conference_Location :
Qingdao
Print_ISBN :
978-1-4799-7016-2
DOI :
10.1109/CCDC.2015.7162304