Tracking control of a small fixed-wing UAV based on Additive-State-Decomposition-Based dynamic inversion method

Author

Deng Siyang ; Du Guang-Xun ; Quan Quan ; Cai Kai-Yuan

Author_Institution

Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China

fYear

2014

fDate

28-30 July 2014

Firstpage

3625

Lastpage

3631

Abstract

In this paper, an Additive-State-Decomposition-Based (ASDB) dynamic inversion tracking controller is designed for a small fixed-wing UAV´s uncertain short-period longitudinal and lateral dynamics. Concretely, we first solve desired attitude and then design attitude controllers by adopting the ASDB dynamic inversion method. Finally, we carry out tracking simulation for both short-period longitudinal and lateral dynamics of a small fixed-wing UAV. The results show the effectiveness of the proposed method.

Keywords

aerospace components; attitude control; autonomous aerial vehicles; robot dynamics; vehicle dynamics; ASDB dynamic inversion tracking controller; additive-state-decomposition-based dynamic inversion method; attitude controller design; small fixed-wing UAV uncertain short-period lateral dynamics; small fixed-wing UAV uncertain short-period longitudinal dynamics; tracking simulation; Abstracts; Attitude control; Automation; Computer aided instruction; Educational institutions; Electrical engineering; Electronic mail; Additive State Decomposition; Small fixed-wing; UAV;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference (CCC), 2014 33rd Chinese

Conference_Location

Nanjing

Type

conf

DOI

10.1109/ChiCC.2014.6895542

Filename

6895542