Development of a Bird-like Flapping-wing Aerial Vehicle with Autonomous Take-off and Landing Capabilities
作者机构：School of AeronauticsNorthwestern Polytechnical UniversityXi’an710072China Yangtze River Delta Research Institute of Northwestern Polytechnical UniversityTaicang215400China Research&Development Institute of Northwestern Polytechnical University in ShenzhenShenzhen518057China
出 版 物：《Journal of Bionic Engineering》 (仿生工程学报（英文版）)
年 卷 期：2021年第18卷第6期
页 面：1291-1303页
核心收录：
学科分类：0711[理学-系统科学] 08[工学] 082503[工学-航空宇航制造工程] 0825[工学-航空宇航科学与技术]
基 金：supported in part by the National Key Research and Development Program of China(No.2017YFB1300102) the Key R&D Program in Shaanxi Province of China(No.2020ZDLGY06-05,No 2021ZDLGY09-10) the National Natural Science Foundation of China(No.11902103,No.11872314)
主 题：Bird-like flapping-wing aerial vehicle(BFAV) Autonomous take-off and landing Take-off mechanism Hybrid layout
摘 要：The lack of autonomous take-off and landing capabilities of bird-like flapping-wing aerial vehicles(BFAVs)seriously restricts their further development and ***,combined with the current research results on the autonomous take-off and landing technology of unmanned aerial vehicles,four types of technologies are studied,including jumping take-off and landing technology,taxiing take-off and landing technology,gliding take-off and landing technology,and vertical take-off and landing(VTOL)*** on the analytic hierarchy process(AHP)-comprehensive evaluation method,a fuzzy comprehensive evaluation model for the autonomous take-off and landing scheme of a BFAV is established,and four schemes are evaluated *** results show that under the existing technical conditions,the hybrid layout VTOL scheme is the ***,the detailed design and development of the prototype of a BFAV with a four-rotor hybrid layout are carried out,and the vehicle performance is *** results prove that through the four-rotor hybrid layout design,the BFAV has good autonomous take-off and landing *** power consumption analysis shows that for a fixed-point reconnaissance mission,when the mission radius is less than 3.38 km,the VTOL type exhibits longer mission duration than the hand-launched type.
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