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


Simulation of a flexible spacecraft motion to evaluate microaccelerations
Authors:A V Sedel’nikov  A A Serpukhova
Institution:1.Samara State Aerospace University,Samara,Russia
Abstract:A method for simulating a flexible spacecraft motion using Lagrange’s quasivelocity formulation is considered. An algorithm of quasivelocity formation by Walsh’s means is proposed. This method can be used to evaluate a quasistatic microacceleration field component in the spacecraft internal environment.
Keywords:
本文献已被 SpringerLink 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