2017
DOI: 10.21608/asat.2017.22449
|View full text |Cite
|
Sign up to set email alerts
|

Improvement of Passive Vibration Damping of Satellite Solar Array Using Adaptive Boundary Conditions

Abstract: Satellite solar array structures experience several loads during deployment and in orbit operations. Such loads cause vibrations and can lead to premature failure or improper service operation, hence, solar arrays must be designed to attenuate these vibrations. In addition, solar arrays must be as light weight as possible, which renders their design process as a fairly complicated one. An innovative approach is presented in this paper for improving the passive vibration damping of solar arrays by using adaptiv… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1

Citation Types

0
3
0

Year Published

2024
2024
2024
2024

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
(3 citation statements)
references
References 2 publications
0
3
0
Order By: Relevance
“…In this case, as the stifness matrix has a frequency dependent characteristic, the eigenvalue converges through iterative calculation. In equation (24), λ * k represents the complex eigenvalue. Te natural frequency and loss coefcient can be defned from the complex eigenvalue λ * k .…”
Section: Approximationmentioning
confidence: 99%
See 2 more Smart Citations
“…In this case, as the stifness matrix has a frequency dependent characteristic, the eigenvalue converges through iterative calculation. In equation (24), λ * k represents the complex eigenvalue. Te natural frequency and loss coefcient can be defned from the complex eigenvalue λ * k .…”
Section: Approximationmentioning
confidence: 99%
“…where F represents the magnitude of the disturbance for each mode. Tis is nonconservative and is added to the right side of the equation of motion in equation (24). At this point, by calculating the weight vector q, the displacement of the beam can be calculated, and the displacement of the remaining layers is also determined.…”
Section: Forced Vibration By Disturbancementioning
confidence: 99%
See 1 more Smart Citation