Adaptive Control for the Twin Rotor Helicopter with Actuator Faults

被引：0

作者：

Zhang, Shijun ^{[1
]}

Chen, Fuyang ^{[1
]}

Tao, Gang ^{[2
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing, Jiangsu, Peoples R China

[2] Univ Virginia, Dept Elect & Comp Engn, Charlottesville, VA 22903 USA

来源：

FRONTIERS OF MANUFACTURING AND DESIGN SCIENCE III, PTS 1 AND 2 | 2013年 / 271-272卷

基金：

中国国家自然科学基金;

关键词：

Actuator Faults; MRAC; Twin Rotor Helicopter;

D O I：

10.4028/www.scientific.net/AMM.271-272.1501

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

For the linear time-invariant model of a twin-rotor helicopter, a new control scheme is proposed in the presence of actuator faults, environmental disturbances and modeling errors. Using the Lyapunov stability theorem, the system with proposed adaptive controller is proved to be stable, and the tracking error tends to zero asymptotically. Simulation results prove the effectiveness of this method.

引用

页码：1501 / +

页数：2

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