Control techniques of tilt rotor unmanned aerial vehicle systems: A review

被引：116

作者：

Liu Zhong ^{[1
,2
]}

He Yuqing ^{[1
]}

Yang Liying ^{[1
]}

Han Jianda ^{[1
]}

机构：

[1] Chinese Acad Sci, Shenyang Inst Automat, State Key Lab Robot, Shenyang 110016, Peoples R China

[2] Univ Chinese Acad Sci, Beijing 100049, Peoples R China

来源：

CHINESE JOURNAL OF AERONAUTICS | 2017年 / 30卷 / 01期

基金：

中国国家自然科学基金;

关键词：

Aircraft structures; Dynamics modeling; Flight control; Tilt rotors; Unmanned aerial vehicle (UAV); FLIGHT CONTROL-SYSTEM; DESIGN OPTIMIZATION; AIRCRAFT; MODE;

D O I：

10.1016/j.cja.2016.11.001

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The tilt rotor unmanned aerial vehicle (TRUAV) exhibits special application value due to its unique rotor structure. However, varying dynamics and aerodynamic interference caused by tiltable rotors are great technical challenges and key issues for TRUAV's high-powered flight controls, which have attracted the attention of many researchers. This paper outlines the concept of TRUAV and some typical TRUAV platforms while focusing on control techniques. TRUAV structural features, dynamics modeling, and flight control methods are discussed, and major challenges and corresponding developmental tendencies associated with TRUAV flight control are summarized. (C) 2016 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license.

引用

页码：135 / 148

页数：14