首页 | 本学科首页   官方微博 | 高级检索  
     

多星分离的ADAMS仿真
引用本文:张兵,岑拯. 多星分离的ADAMS仿真[J]. 导弹与航天运载技术, 2004, 0(2): 1-6
作者姓名:张兵  岑拯
作者单位:北京宇航系统工程设计部,北京,100076;北京宇航系统工程设计部,北京,100076
摘    要:以长征火箭发射伽利略星为应用背景,运用ADAMS软件对三星分离的近场情况进行了仿真分析.详细介绍了分离分析中建立星箭模型的ADAMS描述、仿真过程控制以及各偏差因素对分离过程影响的分析方法.同时,运用ADAMS仿真可以方便地对多星分离的故障模式进行分析,对数值仿真难以实现的碰撞问题进行直观的检测.

关 键 词:伽利略星  多星分离  ADAMS仿真
文章编号:1004-7182(2004)02-0001-06
修稿时间:2003-07-16

The ADAMS Simulation of Multi-satellite Separation System
Zhang Bing Cen Zheng. The ADAMS Simulation of Multi-satellite Separation System[J]. Missiles and Space Vehicles, 2004, 0(2): 1-6
Authors:Zhang Bing Cen Zheng
Abstract:In this paper, ADAMS simulation is applied to the separating motion of the several-satellite system in the background of Galileo satellite launched by Long March launch vehicle, in which, the detailed separating model of both satellites and launch vehicle and the procedure control of simulation are described, and the method of affect analysis about all kinds of elements is introduced. At the same time, malfunction mode analysis and collision detection that is difficult to perform by digital simulation can be accomplished by ADAMS simulation conveniently.
Keywords:Galileo satellite  Multi satellite separation  ADAMS simulation  
本文献已被 CNKI 维普 万方数据 等数据库收录!
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