NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Design of Rigid-Flex PCB Robotics Leveraging Validated Finite Element SimulationsThe use of rigid-flex printed circuit board (PCB) as primary structure has the potential to reduce the weight and volume of robotic systems. In the case of robotics for interplanetary exploration, these systems can leverage origami-inspired folding for increased mobility options and reduced storage volume. Folding rigid-flex PCB robotics can be constructed with rigid PCB connected by short Nomex fabric hinges coupled with flex PCB ribbon cables that permits enhanced system flexibility and energy dissipation to promote impact survivability. This paper presents a design methodology of rigid-flex PCB systems with an emphasis on impact resistance. The design process considers solder joint adequacy, panel bending, and fracture using a finite element (FE) model. The proposed design methodology is developed using a case study with NASA JPL's Pop-Up Folding Flat Explorer Robot (PUFFER). First, the finite-element (FE) modeling methodology is presented with consideration to both frequency and time-domain modeling applications, which include operational self-contact analysis and high impact scenarios. The time-domain impact modeling methodology utilizes hyperelastic material properties for the Nomex hinges. This modeling method is validated using image correlation of PUFFER drop tests. A flowchart is presented to guide users through a validated Abaqus modeling procedure for highly flexible rigid-flex systems. Next, a case study is presented in which PUFFER is subject to drop heights representative of falls into Lunar pits and then the design is refined for a more optimum impact performance. Finally, the results of the case study are used to inform a generalized design methodology for rigid-flex PCB robotics subject to high-impact loads with the considerations presented.
Document ID
20220013066
Acquisition Source
2230 Support
Document Type
Accepted Manuscript (Version with final changes)
Authors
John Bell
(Clemson University Clemson, South Carolina, United States)
Laura Redmond
(Clemson University Clemson, South Carolina, United States)
Kalind Carpenter
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Jean-Pierre De La Croix
(Jet Propulsion Lab La Cañada Flintridge, California, United States)
Date Acquired
August 24, 2022
Publication Date
August 10, 2022
Publication Information
Publication: 2022 IEEE Aerospace Conference (AERO)
Publisher: IEEE
Volume: 2022
Issue Publication Date: August 10, 2022
ISSN: 1095-323X
Subject Category
Computer Operations And Hardware
Funding Number(s)
CONTRACT_GRANT: 80NM0018D0004
CONTRACT_GRANT: 80NSSC20M0054
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
No Preview Available