SLIDING MODE VARIABLE STRUCTURE CONTROL FOR UAV LONGITUDINAL LOOP

被引：0

作者：

Hu Haiyan ^{[1
]}

Xu Min ^{[1
]}

机构：

[1] NW Polytech Univ, Sch Astronaut, Xian 710072, Peoples R China

来源：

2011 INTERNATIONAL CONFERENCE ON INSTRUMENTATION, MEASUREMENT, CIRCUITS AND SYSTEMS ( ICIMCS 2011), VOL 1: INSTRUMENTATION, MEASUREMENT, CIRCUITS AND SYSTEMS | 2011年

关键词：

flight control; variable structure control; sliding mode variable structure; switching function; chattering;

D O I：

暂无

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

This paper introduces the Sliding Mode Variable Structure Control to UAV flight control system. The principle of the Sliding Mode Control Design is presented. The existence condition and the hitting condition of the error adaptive sliding regime are discussed. By studying the longitudinal attitude stabilization loop, a switching function is proposed to realize an error adaptive variable structure. In order to eliminate the chattering of the sliding regime, a dead zone is utilized to realize the variable structure control of the attitude stabilization. Simulation results show that this technology has the following benefits: high disturbance immunity, high control quality, high accuracy and simple algorithm.

引用

页码：313 / 316

页数：4