Dynamic modeling and simulation of deploying process for space solar power satellite receiver

Tingting Yin; Zichen Deng; Weipeng Hu; Xindong Wang

doi:10.1007/s10483-018-2293-6

Dynamic modeling and simulation of deploying process for space solar power satellite receiver

Tingting Yin
, Zichen Deng
, Weipeng Hu
, Xindong Wang

航空学院

科研成果: 期刊稿件 › 文章 › 同行评审

8 引用（Scopus）

摘要

To reveal some dynamic properties of the deploying process for the solar power satellite via an arbitrarily large phased array (SPS-ALPHA) solar receiver, the symplectic Runge-Kuttamethod is used to simulate the simplified model with the consideration of the Rayleigh damping effect.

源语言	英语
期刊	Applied Mathematics and Mechanics (English Edition)
卷	39
期	2
DOI	https://doi.org/10.1007/s10483-018-2293-6
出版状态	已出版 - 1 2月 2018

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10.1007/s10483-018-2293-6

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引用此

@article{867323fcb5084297912c3097b885eb54,

title = "Dynamic modeling and simulation of deploying process for space solar power satellite receiver",

abstract = "To reveal some dynamic properties of the deploying process for the solar power satellite via an arbitrarily large phased array (SPS-ALPHA) solar receiver, the symplectic Runge-Kuttamethod is used to simulate the simplified model with the consideration of the Rayleigh damping effect.",

keywords = "Rayleigh damping, separate and transform, solar power satellite, structure preserving, symplectic Runge-Kutta method",

author = "Tingting Yin and Zichen Deng and Weipeng Hu and Xindong Wang",

note = "Publisher Copyright: {\textcopyright} 2017, Shanghai University and Springer-Verlag GmbH Germany, part of Springer Nature.",

year = "2018",

month = feb,

day = "1",

doi = "10.1007/s10483-018-2293-6",

language = "英语",

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journal = "Applied Mathematics and Mechanics (English Edition)",

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T1 - Dynamic modeling and simulation of deploying process for space solar power satellite receiver

AU - Yin, Tingting

AU - Deng, Zichen

AU - Hu, Weipeng

AU - Wang, Xindong

PY - 2018/2/1

Y1 - 2018/2/1

N2 - To reveal some dynamic properties of the deploying process for the solar power satellite via an arbitrarily large phased array (SPS-ALPHA) solar receiver, the symplectic Runge-Kuttamethod is used to simulate the simplified model with the consideration of the Rayleigh damping effect.

AB - To reveal some dynamic properties of the deploying process for the solar power satellite via an arbitrarily large phased array (SPS-ALPHA) solar receiver, the symplectic Runge-Kuttamethod is used to simulate the simplified model with the consideration of the Rayleigh damping effect.

KW - Rayleigh damping

KW - separate and transform

KW - solar power satellite

KW - structure preserving

KW - symplectic Runge-Kutta method

UR - https://www.scopus.com/pages/publications/85030872775

U2 - 10.1007/s10483-018-2293-6

DO - 10.1007/s10483-018-2293-6

M3 - 文章

AN - SCOPUS:85030872775

SN - 0253-4827

VL - 39

JO - Applied Mathematics and Mechanics (English Edition)

JF - Applied Mathematics and Mechanics (English Edition)

IS - 2

ER -

Dynamic modeling and simulation of deploying process for space solar power satellite receiver

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