首页 | 本学科首页   官方微博 | 高级检索  
     检索      

多星与上面级非对称分离技术研究
引用本文:曾文花,吴琳娜.多星与上面级非对称分离技术研究[J].上海航天,2014,31(2):30-36.
作者姓名:曾文花  吴琳娜
作者单位:[1]上海宇航系统工程研究所,上海201109 [2]上海市空间飞行器机构重点实验室,上海201109
摘    要:对多星与上面级非对称分离技术进行了研究。针对上面级多星非对称分离存在较大偏心的特点,通过优化调整,使用不同大小弹簧力的匹配抵消上面级转动的影响,减小了因卫星相对上面级偏心布置导致的分离力对卫星和上面级姿态的干扰。根据总体偏差量的概率模型,用蒙特卡洛仿真法统计出卫星姿态角和角速度的概率分布规律。

关 键 词:卫星  上面级  非对称  分离  概率模型

Research on Dissymmetry Separation Technology Between Multi-Satellite and Upstage
ZENG Wen-hua,WU Lin-na.Research on Dissymmetry Separation Technology Between Multi-Satellite and Upstage[J].Aerospace Shanghai,2014,31(2):30-36.
Authors:ZENG Wen-hua  WU Lin-na
Institution:1. Aerospace System Engineering Shanghai, Shanghai 201109, China;2. Shanghai Key Laboratory of Spacecraft Mechanism, Shanghai 201109, China)
Abstract:The dissymmetry separation technology between multi-satellite and upstage was studied in this paper. According to the characteristic of the large eccentricity exited in dissymmetry separation between muhi-satellite and upstage, the different appropriate spring forces were adopted to the effect of the upstage rotation by optimizing the parameters, which could decrease the attitude disturbance of the upstage caused by the separation of the satellites which were deployed eccentricity relative the upstage. Based on the probability model of general deviation, the probability law of the attitude angle and the angular velocity of the satellites was statisitied by using the Monte-Carlo simulation method.
Keywords:Satellite  Upstage  Dissymmetry  Separate simulation  Probability model
本文献已被 CNKI 维普 等数据库收录!
点击此处可从《上海航天》浏览原始摘要信息
点击此处可从《上海航天》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号