Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
6954060 | Mechanical Systems and Signal Processing | 2018 | 16 Pages |
Abstract
In the course of designing a spacecraft with thin-walled appendages, system-level trade-offs are routinely performed. Since it is unclear how severely the vibrations of flexible appendages might affect their proper functioning or the control of the spacecraft, it is of paramount importance to validate experimentally thin-walled structures thoroughly for their dynamic and stability behaviours.
Related Topics
Physical Sciences and Engineering
Computer Science
Signal Processing
Authors
Sebastian Oberst, Sean Tuttle,