%0 Journal Article
%T THE DYNAMIC SIMULATION OF SECONDARY SEPARATION OF SMALL SATELLITE<br>小卫星二次分离的动力学仿真
%A 王秋梅
%A 孟宪红
%J 力学与实践
%D 2009
%I 
%X At present, the piggyback is often applied to small satellites launching, while the research of launching sub-satellites from secondary payload adapter of primary satellite is undeveloped. In this article, Adams simulation was made about the separation process of secondary separation structures. Firstly, the rational parameters were selected on the basis of the simplified model. After that, the simulation analysis and dynamic calculating were carried out and the velocity and angle velocity of one sub-satellite' separation were obtained. Finally, it could be concluded that the Adams model was correct comparing results. The conclusion of this article is of great importance on the design and the research of new small satellites.
%K Secondary separation
%K Adams
%K Dynamics simulation
%K Separation attitude<br>二次分离
%K Adams
%K 动力学仿真
%K 分离姿态
%U http://www.alljournals.cn/get_abstract_url.aspx?pcid=6E709DC38FA1D09A4B578DD0906875B5B44D4D294832BB8E&cid=5D344E2AD54D14F8&jid=0BF5C9FB031A532ED0A6D99DC4F6181A&aid=239597BAAC3DF0ADF7DEF4E27E4DF5B5&yid=DE12191FBD62783C&vid=4AD960B5AD2D111A&iid=38B194292C032A66&sid=EA389574707BDED3&eid=96C778EE049EE47D&journal_id=1000-0879&journal_name=力学与实践&referenced_num=0&reference_num=6