Adaptive Fault Tolerant Control of UAV Attitude Control System

被引：0

作者：

Zhao, Hangzhou ^{[1
]}

Yong, Xu ^{[1
]}

Zhang, Yunqi ^{[1
]}

Ding, Yuhao ^{[1
]}

机构：

[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing, Peoples R China

来源：

PROCEEDINGS OF THE 2017 2ND INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND ARTIFICIAL INTELLIGENCE (CAAI 2017) | 2017年 / 134卷

关键词：

UAV; state feedback; error adjustment; adaptive fault tolerant control;

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, we design a direct feedback adaptive fault-tolerant controller to cope with the uncertainty and non-modeling of the interference of the four-rotor UAV attitude control system. The controller is stuck in the UAV and the external. Under the condition of uncertainty, the attitude of the UAV can effectively track the state output of the reference system by introducing the feedback of the state and its error.

引用

页码：70 / 76

页数：7

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