Research on fuzzy PID attitude controller for Multi-rotor UAV

被引：0

作者：

Gao, Shuo ^{[1
]}

Wang, Qi ^{[1
]}

Jiang, Wen ^{[1
]}

Liu, Yan ^{[1
]}

机构：

[1] Nanchang Hangkong Univ, Sch Aircraft Engn, Nanchang 330000, Jiangxi, Peoples R China

来源：

PROCEEDINGS OF THE 2017 5TH INTERNATIONAL CONFERENCE ON FRONTIERS OF MANUFACTURING SCIENCE AND MEASURING TECHNOLOGY (FMSMT 2017) | 2017年 / 130卷

关键词：

Fuzzy PID; Attitude controller; Multi-rotor; UAV;

D O I：

暂无

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

Multi-rotor UAV attitude system has many characteristics such as multi-input multi output, strong coupling, fast time-varying and non-linearity. Thus, for multi rotor UAV attitude control system, the classic PID has some shortcomings. In this paper, the fuzzy PID controller is established by using fuzzy control and classical PID. The on-line self-tuning of PID parameters is realized. The simulation results show that compared with the classical PID, the fuzzy PID controller has the advantages of high control precision, stronger anti-interference ability and stronger robustness, and is more suitable for multi-rotor UAV attitude control system.

引用

页码：726 / 729

页数：4