Development of an Anchoring System for the Soft Asteroid Landing Exploration

被引:9
|
作者
Zhao, Zhijun [1 ]
Wang, Shuang [2 ,3 ]
Li, Delun [1 ]
Wang, Hongtao [1 ]
Wang, Yongbing [4 ]
Zhao, Jingdong [5 ]
机构
[1] Beijing Inst Spacecraft Syst Engn, Beijing Key Lab Intelligent Space Robot Syst Tech, Beijing 100092, Peoples R China
[2] Harbin Inst Technol, Res Ctr Satellite Technol, Harbin 150080, Heilongjiang, Peoples R China
[3] Space Star Technol Co LTD, Beijing 100086, Peoples R China
[4] Beijing Inst Mech & Elect, Beijing 100092, Peoples R China
[5] Harbin Inst Technol, State Key Lab Robot & Syst, Harbin 150080, Heilongjiang, Peoples R China
基金
国家高技术研究发展计划(863计划); 中国国家自然科学基金;
关键词
ROSETTA LANDER; PHILAE;
D O I
10.1155/2019/1257038
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The landing mechanism is easy to flow away from the surface of the asteroid, as there is nearly no gravity on the asteroid. One of the most problems for the asteroid landing exploration is to anchor the landing mechanism on the asteroid surface. In the paper, an anchoring system employed on the soft asteroid anchoring is designed. It is mainly composed of penetrating unit, advancing unit, winding unit, damping unit, and so on. On the basis of the mechanical design, the resistance characteristic of the anchor body in penetrating process is analyzed, and the shape of the anchor tip is designed with the least resistance as the constraint. Then, the validity of the anchor tip design is tested by comparing penetrating ability of different anchor tips. Finally, the penetrating and the anchoring performances of the anchoring system are tested in a variety of media.
引用
收藏
页数:13
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