Control Method Research of Three-DOF Helicopter Based on Active Disturbances Rejection Controller

被引：0
|
作者：
Zhou, You [1 ]
Wang, Qinglin [1 ]
Qiu, Dehui [2 ]
机构：
[1] Beijing Inst Technol, Sch Automat, Beijing 100081, Peoples R China
[2] Capital Normal Univ, Beijing Inst Technol, Sch Information Engn, Sch Automat, Beijing, Peoples R China
来源：
PROCEEDINGS OF THE 2011 INTERNATIONAL CONFERENCE ON INFORMATICS, CYBERNETICS, AND COMPUTER ENGINEERING (ICCE2011), VOL 1: INTELLIGENT CONTROL AND NETWORK COMMUNICATION | 2011年 / 110卷 / 01期
关键词：
active disturbances rejection controller; three-DOF helicopter; tracking;
D O I：
暂无
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
The flight control system of helicopter is difficult to control for their performance of high-order, multi-inputs multi-outputs and strong non-linear. This paper proposed a stability control algorithm of three-DOF laboratory helicopter based on active disturbances rejection controller (ADRC). Controlling the motion of axis guaranteed the tracking control in degrees of helicopter respectively. The stability analysis is carried through Lyapunov method. The results show that the algorithm compensate the disturbance and improve the system performance effectively.
引用
收藏
页码：501 / +
页数：3
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