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22085

Dynamics of a Flexible Beam Moving in Earth Orbit

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Last updated: 04 Jan 2025

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Abstract

Elastic properties of manoeuvring object orbiting earth is discussed herein. Deflections in an elastic beam produced as a result of its motion and external forces are determined using Kane's dynamical equations. Inertia, internal, control, and gravity forces are included to develop modes shapes of vibrations. Deflections at end points are then determined, consequently mass centre position along with beam orientation is amended to have precise positions of end point, where docking with other objects are attained.

DOI

10.21608/asat.2018.22085

Keywords

Elasticity of beams, Kane's dynamical equation, Vibration, LEO maneuver

Authors

First Name

Ahmed

Last Name

Badawy

MiddleName

-

Affiliation

Egyptian Armed Forces, Egypt.

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Orcid

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Volume

15

Article Issue

AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 15 – May 28 - 30, 2013

Related Issue

4183

Issue Date

2013-05-01

Receive Date

2018-12-17

Publish Date

2018-12-17

Page Start

1

Page End

12

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 15_Issue AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 15 &nd….pdf

PDF . 350.4kB

Link

https://asat.journals.ekb.eg/article_22085.html

Detail API

https://asat.journals.ekb.eg/service?article_code=22085

Order

32

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

Dynamics of a Flexible Beam Moving in Earth Orbit

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Article

Created At

22 Jan 2023