Selecting and Optimizing Origami Flasher Pattern Configurations for Finite-Thickness Deployable Space Arrays

Author:

Bolanos Diana1,Varela Katie1,Sargent Brandon1,Stephen Mark A.2,Howell Larry L.1,Magleby Spencer P.1

Affiliation:

1. Brigham Young University Compliant Mechanism Research, Department of Mechanical Engineering, , Provo, UT 84602

2. NASA Goddard Space Flight Center Instrument Systems and Technology Division, , Greenbelt, MD 20771

Abstract

Abstract Design parameters of the origami flasher pattern can be modified to meet a variety of design objectives for deployable array applications. The focus of this paper is to improve the understanding of design parameters, objectives, and trade-offs of origami flasher pattern configurations. Emphasis is placed on finite-thickness flasher models that would enable engineering applications. The methods presented aim to provide clarity on the effects of tuning flasher parameters based on existing synthesis tools. The results are demonstrated in the design of a flasher-based deployable LiDAR telescope where optimization is used to converge on optimal design parameters and the results are implemented in proof-of-concept hardware.

Funder

National Aeronautics and Space Administration

Rocky Mountain NASA Space Grant Consortium

Publisher

ASME International

Subject

Computer Graphics and Computer-Aided Design,Computer Science Applications,Mechanical Engineering,Mechanics of Materials

Reference20 articles.

1. Automated CAD and Modeling of Origami Structures for Reconfigurable Antenna Applications;Khan,2019

2. Variational Level Set Method for Topology Optimization of Origami Fold Patterns;Ye;ASME J. Mech. Des.,2022

3. Accommodating Thickness in Origami-Based Deployable Arrays;Zirbel;ASME J. Mech. Des.,2013

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