2016
DOI: 10.3788/ope.20162402.0372
|View full text |Cite
|
Sign up to set email alerts
|

Suppression of random vibration response of optical satellite by matching honeycomb stiffened plates’ structural parameters

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
0
0

Year Published

2023
2023
2023
2023

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
(1 citation statement)
references
References 0 publications
0
0
0
Order By: Relevance
“…Tan et al combined the satellite's own structure. The method of adding stiffened rib plates was proposed to solve the problem of excessive response [7].…”
Section: Introductionmentioning
confidence: 99%
“…Tan et al combined the satellite's own structure. The method of adding stiffened rib plates was proposed to solve the problem of excessive response [7].…”
Section: Introductionmentioning
confidence: 99%