Tracking Control of a Small Fixed-Wing UAV based on Additive-State-Decomposition-Based Dynamic Inversion Method

被引：0
|
作者：
Deng Siyang [1 ,2 ]
Du Guang-Xun [1 ]
Quan Quan [1 ]
Cai Kai-Yuan [1 ]
机构：
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[2] Beihang Univ, Beihang Sino French Engn Sch, Beijing 100191, Peoples R China
来源：
2014 33RD CHINESE CONTROL CONFERENCE (CCC) | 2014年
关键词：
Small fixed-wing; LJAV; Additive State Decomposition;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
In this paper, an Additive-State-Decomposition-Based (ASDB) dynamic inversion tracking controller is designed for a small fixed-wing UAN"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.
引用
收藏
页码：3625 / 3631
页数：7
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