On-orbit vibration testing for space structures

Jay Chung Chen; James L. Fanson

doi:10.1016/0094-5765(90)90063-Q

On-orbit vibration testing for space structures

Jay Chung Chen^*
, James L. Fanson

^*Corresponding author for this work

Research output: Contribution to journal › Journal Article › peer-review

2 Citations (Scopus)

Abstract

A simulated on-orbit modal test using active members as the excitation source has been performed on the Precision Truss. Using the step sine testing technique, the frequency response functions are obtained and the modal parameters are extracted by the curve-fitting method. Total of 10 global modes and 3 local modes are obtained. The results are compared with those obtained by the conventional external excitation test.

Original language	English
Pages (from-to)	457-466
Number of pages	10
Journal	Acta Astronautica
Volume	21
Issue number	6-7
DOIs	https://doi.org/10.1016/0094-5765(90)90063-Q
Publication status	Published - 1990
Externally published	Yes

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10.1016/0094-5765(90)90063-Q

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@article{607b614280f741668f65640e3fff6039,

title = "On-orbit vibration testing for space structures",

abstract = "A simulated on-orbit modal test using active members as the excitation source has been performed on the Precision Truss. Using the step sine testing technique, the frequency response functions are obtained and the modal parameters are extracted by the curve-fitting method. Total of 10 global modes and 3 local modes are obtained. The results are compared with those obtained by the conventional external excitation test.",

author = "Chen, \{Jay Chung\} and Fanson, \{James L.\}",

year = "1990",

doi = "10.1016/0094-5765(90)90063-Q",

language = "English",

volume = "21",

pages = "457--466",

journal = "Acta Astronautica",

issn = "0094-5765",

publisher = "Elsevier Ltd",

number = "6-7",

}

TY - JOUR

T1 - On-orbit vibration testing for space structures

AU - Chen, Jay Chung

AU - Fanson, James L.

PY - 1990

Y1 - 1990

N2 - A simulated on-orbit modal test using active members as the excitation source has been performed on the Precision Truss. Using the step sine testing technique, the frequency response functions are obtained and the modal parameters are extracted by the curve-fitting method. Total of 10 global modes and 3 local modes are obtained. The results are compared with those obtained by the conventional external excitation test.

AB - A simulated on-orbit modal test using active members as the excitation source has been performed on the Precision Truss. Using the step sine testing technique, the frequency response functions are obtained and the modal parameters are extracted by the curve-fitting method. Total of 10 global modes and 3 local modes are obtained. The results are compared with those obtained by the conventional external excitation test.

UR - https://openalex.org/W1976832715

UR - https://www.webofscience.com/wos/woscc/full-record/WOS:A1990EC38700012

UR - https://www.scopus.com/pages/publications/45149137123

U2 - 10.1016/0094-5765(90)90063-Q

DO - 10.1016/0094-5765(90)90063-Q

M3 - Journal Article

AN - SCOPUS:45149137123

SN - 0094-5765

VL - 21

SP - 457

EP - 466

JO - Acta Astronautica

JF - Acta Astronautica

IS - 6-7

ER -

On-orbit vibration testing for space structures

Abstract

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