H Infinity State Feedback Control for the Stabilization of the Three Euler Angles of Helicopter Based on LMI

Author

Xie, Rong ; Wang, Xinmin ; Li, Yan

Author_Institution

Sch. of Autom., Northwestern Polytech. Univ., Xian

Volume

1

fYear

2008

fDate

20-22 Oct. 2008

Firstpage

375

Lastpage

379

Abstract

The H_infin state feedback control for the stabilization of the three Euler angles of helicopter is studied. The little perturbation model of helicopter is introduced. The proper generalized control variables are chosen and the generalized control object is established. The H_infin state feedback algorithm is developed based on the Iterative Linear Matrix Inequality (LMI) approach and the digital simulation is finished. The simulation results demonstrate the effectiveness of the H_infin state feedback controller.

Keywords

H^infin control; aircraft control; helicopters; linear matrix inequalities; perturbation techniques; stability; state feedback; Euler angles; H_infin infinity state feedback control; LMI; generalized control; helicopter; iterative linear matrix inequality; perturbation model; stabilization; Aerodynamics; Automatic control; Automation; Control theory; Differential equations; H infinity control; Helicopters; Iterative algorithms; Robust control; State feedback; H8 Control; Helicopter; LMI; State Feedback;

fLanguage

English

Publisher

ieee

Conference_Titel

Intelligent Computation Technology and Automation (ICICTA), 2008 International Conference on

Conference_Location

Hunan

Print_ISBN

978-0-7695-3357-5

Type

conf

DOI

10.1109/ICICTA.2008.332

Filename

4659509