Dynamics of space deployable structures

Qiang Tian, Jiang Zhao, Cheng Liu, Chunyan Zhou, Haiyan Hu

科研成果: 书/报告/会议事项章节会议稿件同行评审

7 引用 (Scopus)

摘要

The space industry is eager to have the advanced technology of large space structures composed of trusses, cables and meshes. These space structures will deploy on orbit for different space missions. The important scientific basis of the technology is the nonlinear dynamic modeling, analysis and control of those space structures during their deployment and service. In this study, many space deployable structures (such as satellites antenna and spinning solar sail) are described by using the absolute nodal coordinate formulation (ANCF), and the huge set of equations of motion are solve by high efficient parallel generalized-alpha method. Some numerical results are also validated by experiment results.

源语言英语
主期刊名11th International Conference on Multibody Systems, Nonlinear Dynamics, and Control
出版商American Society of Mechanical Engineers (ASME)
ISBN(电子版)9780791857168
DOI
出版状态已出版 - 2015
活动ASME 2015 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2015 - Boston, 美国
期限: 2 8月 20155 8月 2015

出版系列

姓名Proceedings of the ASME Design Engineering Technical Conference
6

会议

会议ASME 2015 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2015
国家/地区美国
Boston
时期2/08/155/08/15

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