Attitude tracking control based on nonlinear dynamic inversion

Author

Liu, Zhiping ; Yan, Qianshi

Author_Institution

Sch. of Comput. Sci. & Eng., Xi´´an Technol. Univ., Xi´´an, China

Volume

3

fYear

2010

fDate

25-27 June 2010

Abstract

In this paper, a nonlinear dynamic inversion control law is presented for unpowered flying vehicle firstly, meanwhile inertia uncertainty and aerodynamic moment uncertainty are taken into consideration. The vehicle model is a nonlinear and time-varying system, the illustration of the global stability analysis is given secondly, finally the validity of the proposed control law is demonstrated by six-degree-of-freedom simulation.

Keywords

aerodynamics; attitude control; nonlinear control systems; position control; stability; time-varying systems; vehicle dynamics; aerodynamic moment uncertainty; attitude tracking control; global stability analysis; inertia uncertainty; nonlinear dynamic inversion; nonlinear system; six-degree-of-freedom simulation; time-varying system; unpowered flying vehicle; Aerodynamics; Analytical models; Attitude control; Nonlinear control systems; Nonlinear dynamical systems; Stability analysis; Time varying systems; Uncertainty; Vehicle dynamics; Vehicles; Dynamic inversion; Nonlinear system; Robust control; Unpowered flying vehicle;

fLanguage

English

Publisher

ieee

Conference_Titel

Computer Design and Applications (ICCDA), 2010 International Conference on

Conference_Location

Qinhuangdao

Print_ISBN

978-1-4244-7164-5

Electronic_ISBN

978-1-4244-7164-5

Type

conf

DOI

10.1109/ICCDA.2010.5541321

Filename

5541321