Show simple item record

contributor authorXiuchang Huang
contributor authorJingya Sun
contributor authorHongxing Hua
contributor authorZhiyi Zhang
date accessioned2017-05-08T22:20:57Z
date available2017-05-08T22:20:57Z
date copyrightMay 2015
date issued2015
identifier other42744238.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/78352
description abstractThis paper addresses dynamic modeling and performs optimization of a passive multistrut vibration isolation platform (VIP) in vibration isolation for an assembly of control moment gyroscopes (CMGs). Each strut of the VIP is composed of a metal rod and a three-parameter isolator in series. First, the frequency response function (FRF)–based substructuring method was developed to establish the dynamic model of a whole satellite system. This method can take into account the influence of the flexibility of the satellite bus and the CMG assembly as well as the gyroscopic effects of CMGs. Then, an optimization model was developed, and the FRF-based sensitivity analysis was employed to optimize the characteristic parameters of a strut under two objective functions. Finally, a numerical model was developed to verify the validity and effectiveness of the proposed method. The dynamic characteristics of an octostrut VIP were analyzed. The isolation performance was greatly enhanced after optimization. This study shows that the method is an effective and efficient tool that can be used in the design phase of VIPs.
publisherAmerican Society of Civil Engineers
titleModeling and Optimization of Octostrut Vibration Isolation Platform by FRF-Based Substructuring Method
typeJournal Paper
journal volume28
journal issue3
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000416
treeJournal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 003
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record