DocumentCode
3116147
Title
Study on the landing mechanism employed in asteroid exploration
Author
Zhao, Zhijun ; Zhao, Jingdong ; Liu, Hong
Author_Institution
State Key Lab. of Robot. & Syst., Harbin Inst. of Technol., Harbin, China
fYear
2012
fDate
5-8 Aug. 2012
Firstpage
1032
Lastpage
1037
Abstract
Different landing exploration modes of small bodies are discussed. A landing mechanism employed in the asteroid landing exploration is designed. It contains landing foot, landing gear, cardan, buffer mechanism, equipment base, anchor system, and so on. The landing mechanism could fold up to reduce space occupation in the spacecraft. It could fix itself on the landing slope under microgravity via the anchor system. The anchor system´s penetrating and anchoring capability is examined in the frozen earth. The landing performance under microgravity is tested on the air-floating platform. Experiments show that the landing mechanism could perform landing under microgravity and anchoring itself firmly on the landing slope.
Keywords
aerospace components; anchors; asteroids; gears; space vehicles; air floating platform; anchor system; asteroid landing exploration; buffer mechanism; cardan; frozen earth; landing foot; landing gear; landing mechanism; microgravity landing performance; Acceleration; Damping; Earth; Foot; Force; Gears; Space vehicles; Anchoring. Microgravity; Asteroid exploration; Landing mechanism;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation (ICMA), 2012 International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4673-1275-2
Type
conf
DOI
10.1109/ICMA.2012.6283392
Filename
6283392
Link To Document