PDE Modeling and Basic Vibration Control for Flexible Satellite

Zhijie Liu; Jinkun Liu

doi:10.1007/978-981-15-2596-4_3

PDE Modeling and Basic Vibration Control for Flexible Satellite

Zhijie Liu^*
, Jinkun Liu

^*此作品的通讯作者

自动化科学与电气工程学院

University of Science and Technology Beijing

科研成果: 书/报告/会议事项章节 › 章节 › 同行评审

摘要

Satellites have gained much attention in the past decades for the purpose of remote sensing, communication and so on [8–10]. Considering a complex environment and space mission constraints, flexible satellite characterized by light weight structure, limitation of mass, low energy consumption and reduced launch cost, are widely used. Flexible satellites usually consists of a central rigid hub and long flexible appendages such as solar panels.

源语言	英语
主期刊名	Springer Tracts in Mechanical Engineering
出版商	Springer
页	25-43
页数	19
DOI	https://doi.org/10.1007/978-981-15-2596-4_3
出版状态	已出版 - 2020

出版系列

姓名	Springer Tracts in Mechanical Engineering
ISSN（印刷版）	2195-9862
ISSN（电子版）	2195-9870

联合国可持续发展目标

此成果有助于实现下列可持续发展目标：

可持续发展目标 7 经济适用的清洁能源

访问文件

10.1007/978-981-15-2596-4_3

其它文件与链接

链接到 Scopus 的出版物

引用此

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title = "PDE Modeling and Basic Vibration Control for Flexible Satellite",

abstract = "Satellites have gained much attention in the past decades for the purpose of remote sensing, communication and so on [8–10]. Considering a complex environment and space mission constraints, flexible satellite characterized by light weight structure, limitation of mass, low energy consumption and reduced launch cost, are widely used. Flexible satellites usually consists of a central rigid hub and long flexible appendages such as solar panels.",

author = "Zhijie Liu and Jinkun Liu",

note = "Publisher Copyright: {\textcopyright} 2020, Tsinghua University Press.",

year = "2020",

doi = "10.1007/978-981-15-2596-4\_3",

language = "英语",

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AU - Liu, Jinkun

PY - 2020

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AB - Satellites have gained much attention in the past decades for the purpose of remote sensing, communication and so on [8–10]. Considering a complex environment and space mission constraints, flexible satellite characterized by light weight structure, limitation of mass, low energy consumption and reduced launch cost, are widely used. Flexible satellites usually consists of a central rigid hub and long flexible appendages such as solar panels.

UR - https://www.scopus.com/pages/publications/85083437829

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DO - 10.1007/978-981-15-2596-4_3

M3 - 章节

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T3 - Springer Tracts in Mechanical Engineering

SP - 25

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BT - Springer Tracts in Mechanical Engineering

PB - Springer

ER -

PDE Modeling and Basic Vibration Control for Flexible Satellite

摘要

出版系列

联合国可持续发展目标

访问文件

其它文件与链接

指纹

引用此