Title :
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
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;
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
DOI :
10.1109/ChiCC.2014.6895542
