四旋翼无人直升机飞行控制技术综述  

Survey of flight control technology for quad-rotor unmanned helicopter

作　　者：甄红涛[1] 齐晓慧[1] 夏明旗 赵红瑞 

机构地区：[1]军械工程学院光学与电子工程系,河北石家庄050003 [2]总装备部驻447厂军事代表室,内蒙古包头014033 [3]内蒙古北方重工业集团有限公司办公室,内蒙古包头014033

出　　处：《飞行力学》2012年第4期295-299,共5页Flight Dynamics

基　　金："十一五"装备预研基金资助(9140A25070509JB3405)

摘　　要：四旋翼无人直升机因具有良好的性能而成为近十几年来的研究热点,针对四旋翼直升机的飞行控制技术进行了简要综述。首先,通过分析四旋翼无人直升机的飞行控制特性,指出了飞行控制系统设计的要求和难点;然后,总结了四旋翼直升机飞行控制的研究现状,对几种常用控制算法的特点进行了分析;最后,在分析四旋翼无人直升机关键技术的基础上,讨论了四旋翼飞行控制的发展趋势。Quad-rotor unmanned helicopter has been a hot research focus in recent years because of its good performance.This paper gives a brief introduction to the flight control technologies of quad-rotor helicopter.First of all,the characteristics of the flight control system of quad-rotor are analyzed,and the difficulties and requirements for the flight control system are pointed out.Then,the present research development for the quad-rotor flight control is summarized,and the characteristics of some common control algorithm are analyzed.Finally,the future research direction of quad-rotor flight control is discussed on the basis of analyzing the key technologies of quad-rotor unmanned helicopter.

关 键 词：四旋翼无人直升机 微小型飞行器 控制技术 自主飞行 

分 类 号：V279[航空宇航科学与技术—飞行器设计]