Published January 5, 2020
| public
Book Section - Chapter
Sequentially Controlled Dynamic Deployment of Ultra-Thin Shell Structures
Chicago
Abstract
This paper presents an approach to achieve the staged deployment of planar structures composed of multiple thin-shell elements. Releasable constraints are used to prescribe intermediate, known configurations along a strain energy-driven deployment path. An analytical model is derived to design the nominal deployment sequence of the structure by identifying kinematically compatible paths. Then, a finite element model is developed to capture the dynamic behavior of the shells during a staged deployment. Practical considerations, such as the deployment envelope and incorporation of the structure in a deployment mechanism are discussed. Finally, the proposed deployment sequence is demonstrated experimentally.
Additional Information
© 2020 American Institute of Aeronautics and Astronautics. Published Online: 5 Jan 2020.Additional details
- Eprint ID
- 100654
- Resolver ID
- CaltechAUTHORS:20200113-075647741
- Created
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2020-01-13Created from EPrint's datestamp field
- Updated
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2021-11-16Created from EPrint's last_modified field
- Caltech groups
- GALCIT
- Other Numbering System Name
- AIAA Paper
- Other Numbering System Identifier
- 2020-0690