Rigid-Foldable Doubly Curved Deployable Reflectors Based on Miura–Ori Pattern

This paper introduces a novel deployable reflector concept which achieves single degree-of-freedom folding of solid doubly curved surfaces. A set of folding kinematics is constructed using the Miura–Ori pattern and the Hoberman linkage to allow compact collision-free stowage of a fully rigid truss-supported solid-surface reflector structure. In this paper, the baseline kinematic architecture is introduced, and a design methodology using Bayesian optimization to systematically obtain optimally stowed geometries is detailed. An example design is carried out to demonstrate the methodology. Optimal parameters are produced, the design space is explored, and a detailed design based on the optimal parameters is made, along with its derivative variants. Finally, a prototype model and quantification of surface errors confirm the validity of resulting designs.

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Publication Details

Journal
Journal of Spacecraft and Rockets
Published
2024-11-13
DOI
https://doi.org/10.2514/1.a36107
Citations
3
Primary Topic
Structural Analysis and Optimization
Type
article
Field-Weighted Citation Impact
0.78
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article

Rigid-Foldable Doubly Curved Deployable Reflectors Based on Miura–Ori Pattern

Matthew Santer, Tianshu Wang
3 citations
Journal of Spacecraft and Rockets
Structural Analysis and Optimization
0.78
article

Rigid-Foldable Doubly Curved Deployable Reflectors Based on Miura–Ori Pattern

Matthew Santer, Tianshu Wang
article en
3 citations

Abstract

This paper introduces a novel deployable reflector concept which achieves single degree-of-freedom folding of solid doubly curved surfaces. A set of folding kinematics is constructed using the Miura–Ori pattern and the Hoberman linkage to allow compact collision-free stowage of a fully rigid truss-supported solid-surface reflector structure. In this paper, the baseline kinematic architecture is introduced, and a design methodology using Bayesian optimization to systematically obtain optimally stowed geometries is detailed. An example design is carried out to demonstrate the methodology. Optimal parameters are produced, the design space is explored, and a detailed design based on the optimal parameters is made, along with its derivative variants. Finally, a prototype model and quantification of surface errors confirm the validity of resulting designs.

Journal of Spacecraft and RocketsVol. 62(3)
Imperial College London (GB)
Clean water and sanitation
Openalex Percentile: Top 29%
Structural Analysis and Optimization
0.78
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