Dynamics of space deployable structures

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

doi:10.1115/DETC2015-46159

Dynamics of space deployable structures

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

School of Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

7 Citations (Scopus)

Abstract

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.

Original language	English
Title of host publication	11th International Conference on Multibody Systems, Nonlinear Dynamics, and Control
Publisher	American Society of Mechanical Engineers (ASME)
ISBN (Electronic)	9780791857168
DOIs	https://doi.org/10.1115/DETC2015-46159
Publication status	Published - 2015
Event	ASME 2015 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2015 - Boston, United States Duration: 2 Aug 2015 → 5 Aug 2015

Publication series

Name	Proceedings of the ASME Design Engineering Technical Conference
Volume	6

Conference

Conference	ASME 2015 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2015
Country/Territory	United States
City	Boston
Period	2/08/15 → 5/08/15

Access to Document

10.1115/DETC2015-46159

Cite this

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title = "Dynamics of space deployable structures",

abstract = "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.",

author = "Qiang Tian and Jiang Zhao and Cheng Liu and Chunyan Zhou and Haiyan Hu",

note = "Publisher Copyright: {\textcopyright} Copyright 2015 by ASME.; ASME 2015 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2015 ; Conference date: 02-08-2015 Through 05-08-2015",

year = "2015",

doi = "10.1115/DETC2015-46159",

language = "English",

series = "Proceedings of the ASME Design Engineering Technical Conference",

publisher = "American Society of Mechanical Engineers (ASME)",

booktitle = "11th International Conference on Multibody Systems, Nonlinear Dynamics, and Control",

address = "United States",

}

Tian, Q, Zhao, J, Liu, C, Zhou, C & Hu, H 2015, Dynamics of space deployable structures. in 11th International Conference on Multibody Systems, Nonlinear Dynamics, and Control. Proceedings of the ASME Design Engineering Technical Conference, vol. 6, American Society of Mechanical Engineers (ASME), ASME 2015 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2015, Boston, United States, 2/08/15. https://doi.org/10.1115/DETC2015-46159

Dynamics of space deployable structures. / Tian, Qiang; Zhao, Jiang; Liu, Cheng et al.
11th International Conference on Multibody Systems, Nonlinear Dynamics, and Control. American Society of Mechanical Engineers (ASME), 2015. (Proceedings of the ASME Design Engineering Technical Conference; Vol. 6).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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AU - Zhao, Jiang

AU - Liu, Cheng

AU - Zhou, Chunyan

AU - Hu, Haiyan

PY - 2015

Y1 - 2015

N2 - 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.

AB - 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.

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DO - 10.1115/DETC2015-46159

M3 - Conference contribution

AN - SCOPUS:84982142821

T3 - Proceedings of the ASME Design Engineering Technical Conference

BT - 11th International Conference on Multibody Systems, Nonlinear Dynamics, and Control

PB - American Society of Mechanical Engineers (ASME)

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Y2 - 2 August 2015 through 5 August 2015

ER -

Dynamics of space deployable structures

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