| Design,modeling, and control of morphing aircraft:A review |
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| 作者姓名： | Lingling CHU Qi LI Feng GU Xintian DU Yuqing HE Yangchen DENG |
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| 作者单位： | 1. State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences;3. University of Chinese Academy of Sciences;4. Shenyang Aircraft Design & Research Institute |
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| 基金项目： | supported by the National Key R&D Program of China (No. 2018YFC0810102)；;the National Natural Science Foundation of China (Nos. 91848203 and 91948202)；;Natural Science Foundation of Liao Ning Province of China (20180520014)； |
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| 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...
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| 收稿时间： | 19 January 2021 |
Design,modeling, and control of morphing aircraft: A review |
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| Lingling CHU,Qi LI,Feng GU,Xintian DU,Yuqing HE,Yangchen DENG.Design,modeling, and control of morphing aircraft:A review[J].Chinese Journal of Aeronautics,2022,35(5):220-246. |
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| Institution: | 1. State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang 110016, China;2. Institutes for Robotics and Intelligent Manufacturing, Chinese Academy of Sciences, Shenyang 110169, China;3. University of Chinese Academy of Sciences, Beijing 100049, China;4. Shenyang Aircraft Design & Research Institute, Shenyang 110034, China |
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| Abstract: | 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. |
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| Keywords: | Aircraft design Dynamic modeling Fault tolerance Flight control Intelligent material Morphing aircraft Unmanned Aerial Vehicles (UAV) |
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