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 :
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