A robust dynamic inversion technique for asymptotic tracking control of an aircraft

Author

Tanyer, I. ; Tatlicioglu, Enver ; Zergeroglu, Erkan

Author_Institution

Dept. of Electr. & Electron. Eng., Izmir Inst. of Technol., Izmir, Turkey

fYear

2013

fDate

23-26 June 2013

Firstpage

1

Lastpage

6

Abstract

In this paper, a tracking controller is developed for an aircraft model subject to uncertainties in the dynamics and additive state-dependent nonlinear disturbance-like terms. In the design of the controller, dynamic inversion technique is utilized in conjunction with a robust term. Only the output of aircraft dynamics is utilized in the controller design and acceleration measurements are not required. Lyapunov based stability analysis is used to prove global asymptotic tracking.

Keywords

Lyapunov methods; aircraft control; asymptotic stability; control system synthesis; nonlinear control systems; vehicle dynamics; Lyapunov based stability analysis; additive state-dependent nonlinear disturbance-like terms; aircraft dynamics; aircraft tracking control; asymptotic tracking control; controller design; dynamic inversion technique; global asymptotic tracking; robust dynamic inversion technique; Aerodynamics; Aerospace control; Aircraft; Atmospheric modeling; Control design; Robustness; Uncertainty;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference (ASCC), 2013 9th Asian

Conference_Location

Istanbul

Print_ISBN

978-1-4673-5767-8

Type

conf

DOI

10.1109/ASCC.2013.6606263

Filename

6606263