Helicopter Hovering Control Design based on Model Reference Adaptive Method

被引：0

作者：

Sun, Li ^{[1
]}

机构：

[1] Shan Dong Xiehe Coll, Coll Mech & Elect Engn, Jinan, Shandong, Peoples R China

来源：

PROCEEDINGS OF 2019 IEEE 3RD INFORMATION TECHNOLOGY, NETWORKING, ELECTRONIC AND AUTOMATION CONTROL CONFERENCE (ITNEC 2019) | 2019年

关键词：

3-DOF helicopter system; model-reference adaptive control; hovering control; multi-input multi-output system;

D O I：

10.1109/itnec.2019.8729298

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

To study the dynamic characteristics of 3-DOF experimental teaching helicopter model , the mathematical model of small-sized 3-DOF helicopter system is set up. The movement of helicopter includes three parts of elevation ax-is, pitch axis and travel axis, and their dynamic functions are set up. To solve the hovering control problem, a model-reference adaptive control system is designed based on Lyapunov stability theory. Simulation results show the designed control system can satisfy the dynamic and steady properties , and provide a reference for designing other control systems.

引用

页码：1621 / 1624

页数：4

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