2021
DOI: 10.2514/1.a35047
|View full text |Cite
|
Sign up to set email alerts
|

Frequency-Domain Response Prediction of a Launch Vehicle Coupled with New Payloads

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2

Citation Types

0
2
0

Year Published

2023
2023
2024
2024

Publication Types

Select...
2
1

Relationship

0
3

Authors

Journals

citations
Cited by 3 publications
(2 citation statements)
references
References 1 publication
0
2
0
Order By: Relevance
“…acting on the interface DoFs. Without considering damping for the time being, the motion equation of service system of lightweight structure can be written in the following block form [34]…”
Section: Inherent Rigid-flex Coupling Relation Of Hsrsmentioning
confidence: 99%
“…acting on the interface DoFs. Without considering damping for the time being, the motion equation of service system of lightweight structure can be written in the following block form [34]…”
Section: Inherent Rigid-flex Coupling Relation Of Hsrsmentioning
confidence: 99%
“…The displacement x o = X o e jωt on the interface DoFs, the displacement x i = X i e jωt on the internal DoFs, and the excitation load f o = F o e jωt acting on the interface DoFs. Without considering damping for the time being, the motion equation of the service system of a lightweight structure can be written in the following block form [34]:…”
Section: Inherent Rigid-flex Coupling Relation Of Hsrsmentioning
confidence: 99%