首页|Controlled flight of a self-powered micro blimp driven by insect-sized flapping-wing thrusters

Controlled flight of a self-powered micro blimp driven by insect-sized flapping-wing thrusters

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Micro aerial platforms face significant challenges in achieving long controlled endurance as most of the energy is consumed to overcome the weight of the body.In this study,we present a controllable micro blimp that addresses this issue through the use of a helium-filled balloon.The micro blimp has a long axis of 23 cm and is propelled by four insect-sized flapping-wing thrusters,each weighing 80 mg and with a wingspan of 3.5 cm.These distributed thrusters enable controlled motions and provide the micro blimp with an advantage in flight endurance compared to multi-rotors or flapping-wing micro aerial vehicles at the same size scale.To enhance the performance of the controlled flight,we propose a wireless control module that enables manipulation from a dis-tance of up to 100 m.Additionally,a smartphone application is developed to send instructions to the circuit board,allowing the blimp to turn left and right,ascend and descend,and achieve a com-bination of these movements separately.Our findings demonstrate that this micro blimp is one of the smallest controlled self-powered micro blimps to date.

Micro air vehicleAircraft controlSelf-powered micro blimpFlapping-wing thrusterWireless flight

Xian YU、Zhiwei LIU、Jiaming LENG、Mingjing QI、Xiaojun YAN

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School of Energy and Power Engineering,Beihang University,Beijing 100191,China

Collaborative Innovation Center of Advanced Aero-Engine,Beijing 100191,China

National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,Beihang University,Beijng 100191,China

Beijing Key Laboratory of Aero-Engine Structure and Strength,Beihang University,Beijing 100191,China

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Beijing Natural Science Foundation,ChinaNational Natural Science Foundation of ChinaMinistry of Education of the People's Republic of China 111 Project

323201012002017B08009

2024

中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
年,卷(期):2024.37(6)
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