Parametric study on the use of Hoberman mechanisms for reconfigurable antenna and solar arrays
- 1 March 2010
- conference paper
- conference paper
- Published by Institute of Electrical and Electronics Engineers (IEEE) in 2010 IEEE Aerospace Conference
- No. 1095323X,p. 1-8
- https://doi.org/10.1109/aero.2010.5446956
Abstract
One of the primary concerns associated with the design of small satellites is achieving power capacities sufficient to support payload and mission operations while simultaneously retaining communications capabilities. Furthermore, small satellites must be able to easily transform from their tightly stowed configurations to their fully operational mode. To address these concerns, this paper presents the theoretical modeling and analysis of a class of foldable mechanisms, based on the Hoberman mechanism's kinematic theory, and their parametric coupling with the system parameters of both an antenna array and a solar array. The resulting models provide viable solar array and antenna array designs to generate power and communications capabilities on small satellites.Keywords
This publication has 2 references indexed in Scilit:
- Design of Autonomous Foldable Docking Mechanism for Small Space VehiclesPublished by ASME International ,2009
- A kinematic theory for radially foldable planar linkagesInternational Journal of Solids and Structures, 2007