DocumentCode :
3660327
Title :
Landing performance simulation of an asteroid landing mechanism
Author :
Zhijun Zhao;Delun Li;Baofeng Yuan;Sheng Gao;Jingdong Zhao
Author_Institution :
Beijing Key Laboratory of Intelligent Space Robotic Systems, Technology and Applications, Beijing Institute of Spacecraft System Engineering, 100092, China
fYear :
2015
Firstpage :
1914
Lastpage :
1919
Abstract :
Asteroid landing is a new research field in deep space exploration, which has important scientific and economic values in learning the origin of the solar system and exploring the asteroid. It is microgravity and little media properties are obtained on the asteroid surface, thus good landing performance is demanded to realize safe landing of the landing mechanism. Landing mechanism in the paper has three legs, and the damping device is located between the landing gear and the equipment base. Simulation method is introduced to analyze the landing performance of the landing mechanism. Landing performance of the landing mechanism on 30° landing slope with the largest landing velocity is simulated in three typical landing modes, and the landing performance is reflected by stability time of the landing gear and overloading acceleration of the equipment base. Landing simulation has important significance in learning landing performance and guiding the landing of the landing mechanism.
Keywords :
"Force","Damping","Acceleration","Gears","Loading","Stability analysis","Mathematical model"
Publisher :
ieee
Conference_Titel :
Information and Automation, 2015 IEEE International Conference on
Type :
conf
DOI :
10.1109/ICInfA.2015.7279601
Filename :
7279601
Link To Document :
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