Review of Key Technologies of Rotary-Wing Mars UAVs for Mars Exploration

被引：1
|
作者：
Zhao, Pengyue [1 ,2 ,3 ]
Li, Ruihan [4 ]
Wu, Peng [2 ,3 ]
Liu, Huan [2 ,3 ]
Gao, Xifeng [2 ,3 ]
Deng, Zongquan [1 ]
机构：
[1] Harbin Inst Technol, State Key Lab Robot & Syst, Harbin 150001, Peoples R China
[2] Harbin Inst Technol, Ctr Ultraprecis Optoelect Instrumentat Engn, Harbin 150001, Peoples R China
[3] Minist Ind Informat Technol, Key Lab Ultraprecis Intelligent Instrumentat, Harbin 150080, Peoples R China
[4] Harbin Engn Univ, Coll Mech & Elect Engn, Harbin 150001, Peoples R China
来源：
INVENTIONS | 2023年 / 8卷 / 06期
基金：
中国国家自然科学基金;
关键词：
Mars UAV; rotary wing; key technologies; aerodynamic characteristics; control methods; experiments; LOW-REYNOLDS-NUMBER; SCALE HELICOPTER ROTOR; HOVER PERFORMANCE; MARTIAN ATMOSPHERE; DESIGN; AIRFOIL; SYSTEM; MODEL; FLOW; SEPARATION;
D O I：
10.3390/inventions8060151
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
The sparse atmosphere on the surface of Mars provides the necessary flight conditions for Mars unmanned aerial vehicles (UAVs) to perform low-altitude flights. This work presents a comprehensive overview of key technologies in the development of Mars UAVs, with a specific focus on rotary-wing Mars UAVs. It summarizes prototypes of rotary-wing Mars UAVs developed by various global research institutions. It reviews essential technologies in rotary-wing Mars UAV research, including the Mars near-surface atmospheric environment, aerodynamic characteristics, and principles of low-pressure flight control. This work also summarizes various experimental setups and ground test results for rotary-wing Mars UAVs. Furthermore, it discusses the future development trends of rotary-wing Mars UAVs.
引用
收藏
页数：25
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