Design, modeling, and control of morphing aircraft:A review

被引：0

作者：

Lingling CHU ^{[1
,2
,3
]}

Qi LI ^{[1
,2
]}

Feng GU ^{[1
,2
]}

Xintian DU ^{[1
,2
]}

Yuqing HE ^{[1
,2
]}

Yangchen DENG ^{[4
]}

机构：

[1] State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences

[2] Institutes for Robotics and Intelligent Manufacturing, Chinese Academy of Sciences

[3] University of Chinese Academy of Sciences

[4] Shenyang Aircraft Design & Research Institute

来源：

Chinese Journal of Aeronautics | 2022年 / 35卷 / 05期

基金：

中国国家自然科学基金; 国家重点研发计划;

关键词：

D O I：

暂无

中图分类号：

V279 [无人驾驶飞机]; V249.1 [飞行控制];

学科分类号：

081105 ; 1111 ;

摘要：

A morphing aircraft can adapt its configuration to suit different types of tasks, which is also an important requirement of Unmanned Aerial Vehicles(UAV). The successful development of an unmanned morphing aircraft involves three steps that determine its ability and intelligent: configuration design, dynamic modeling and flight control. This study conducts a comprehensive survey of morphing aircraft. First, the methods to design the configuration of a morphing aircraft are presented and analyzed. Then, the nonlinear dynamic characteristics and aerodynamic interference caused by a morphing wing are described. Subsequently, the dynamic modeling and flight control methods for solving the flight control problems are summarized with respect to these features.Finally, the general as well as special challenges ahead of the development of intelligent morphing aircraft are discussed. The findings can provide a theoretical and technical reference for designing future morphing aircraft or morphing-wing UAVs.

引用

页码：220 / 246

页数：27

共 80 条

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