Review for the Design and Experimental Study of a Coaxial Twin-rotor Mars Unmanned Aerial VehicleOA
The thin atmosphere of Mars presents a necessary yet challenging flight environment for low-altitude flying vehicles or unmanned aerial vehicles.As a key technology,Martian unmanned aerial vehicles hold marked value and importance for scientific research and future interplanetary exploration.This review systematically explores the advantages and challenges of coaxial dual-rotor Martian drones under low-Reynolds-number conditions,focusing on the optimization of blade design methods and experimental research progress under these conditions.It also details the development of a multi-degree-of-freedom coaxial dual-rotor Martian drone prototype and its flight control algorithm strategy.In addition,the review describes the process of establishing a blade testing platform in a vacuum chamber to simulate the Martian environment.The review offers a comprehensive analysis of the different impacts that the environments of Earth and Mars have on the design of coaxial dual-rotor drones and looks forward to potential design methods and experimental research directions for future Martian drone development.Through takeoff experiments conducted in an Earth-based simulated Martian environment,the feasibility of flight testing for Martian drones is verified.The review compares the differences and characteristics of developing coaxial dual-rotor drones under terrestrial and Martian conditions,providing valuable examples and a solid foundation for the research and development of Martian drones.
Zhifang Ke;Yu Hu;Qingkai Meng;Yongjie Shu;Jinghan Tu;Molei Zhao;Shiyi Wei;Haitao Zhang;Bin Xu;Zhaopu Yao;Wei Wei
School of Mechanical Engineering,Beijing Institute of Technology,Beijing 100081,China Institute of Advanced Technology,Beijing Institute of Technology,Jinan 250300,ChinaBeijing Institute of Control Engineering,Beijing 100094,ChinaSchool of Mechanical Engineering,Beijing Institute of Technology,Beijing 100081,China Institute of Advanced Technology,Beijing Institute of Technology,Jinan 250300,ChinaSchool of Mechanical Engineering,Beijing Institute of Technology,Beijing 100081,ChinaSchool of Mechanical Engineering,Beijing Institute of Technology,Beijing 100081,China Chongqing Innovation Center,Beijing Institute of Technology,Chongqing 401122,ChinaSchool of Mechanical Engineering,Beijing Institute of Technology,Beijing 100081,ChinaSchool of Mechanical Engineering,Beijing Institute of Technology,Beijing 100081,ChinaShenSi Lab,Shenzhen Institute for Advanced Study,University of Electronic Science and Technology of China,Shenzhen 518110,ChinaSchool of Mechanical Engineering,Beijing Institute of Technology,Beijing 100081,China Chongqing Innovation Center,Beijing Institute of Technology,Chongqing 401122,ChinaBeijing Institute of Control Engineering,Beijing 100094,ChinaSchool of Mechanical Engineering,Beijing Institute of Technology,Beijing 100081,China Chongqing Innovation Center,Beijing Institute of Technology,Chongqing 401122,China
航空航天
optimization blade design methodsunmanned aerial vehiclesexperimental research prunmanned aerial vehiclesaslow Reynolds number conditionsmartian dronescoaxial twin rotorMars unmanned aerial vehicle
《Space(Science & Technology)》 2025 (1)
P.689-721,33
funded by Beijing Natural Science Foundation(grant number 3244036)the National Key Research and Development Program(grant number 2020YFC1512500)the Shandong Postdoctora1 Science Foundation(grant number SDCX-ZG-202303052)Natural Science Foundation of Chongqing,China(grant number CSTB2022NSCQ-MSX1101).
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