Decoupling control of a hypersonic gliding vehicle based on NESO

Author

Bai Chen ; Ren Zhang ; Shao Xingyue

Author_Institution

Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China

fYear

2014

fDate

28-30 July 2014

Firstpage

2311

Lastpage

2315

Abstract

According to attitude control of a hypersonic gliding vehicle, a decoupling control approach based on NESO is proposed. Decoupling control is realized through the decentralized control theory. The system coupling terms and uncertainties are estimated by NESO and added into the control law for compensation. Theoretical analysis proves that the tracking errors of the closed-loop system are consistently bounded. Simulations are carried on through the hypersonic gliding vehicle model comparing the proposed method and the traditional sub-channel control method. The results show that the tracking effectiveness of the proposed method is better and impact caused by coupling and uncertainties is eliminated.

Keywords

aircraft control; attitude control; closed loop systems; compensation; decentralised control; nonlinear control systems; observers; uncertain systems; NESO; attitude control; closed-loop system; compensation control law; consistently bounded tracking errors; decentralized control theory; decoupling control approach; hypersonic gliding vehicle; nonlinear extended state observer; system coupling term estimation; system uncertainty estimation; Control systems; Couplings; MIMO; Robustness; Uncertainty; Vehicle dynamics; Vehicles; Decoupling control; Hypersonic gliding vehicle; NESO; Uncertainties;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference (CCC), 2014 33rd Chinese

Conference_Location

Nanjing

Type

conf

DOI

10.1109/ChiCC.2014.6896993

Filename

6896993