
Christine E. Gregg- PhD
- Engineer at National Aeronautics and Space Administration
Christine E. Gregg
- PhD
- Engineer at National Aeronautics and Space Administration
About
24
Publications
6,352
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359
Citations
Introduction
Christine E. Gregg received her Ph.D. from the Department of Mechanical Engineering, University of California, Berkeley. She is currently a researcher employed at NASA Ames Research Center, geographically based in the greater Boston Area. Her research interests include advanced manufacturing, ultra-light structures, autonomous structural systems, robotics, metamaterials, antennas, and in-space servicing manufacturing and assembly (ISAM).
Major Awards: NASA Honor Award (Early Career, Group)
Current institution
Additional affiliations
August 2013 - present
Publications
Publications (24)
We introduce and analyze a model for self-reconfigurable robots made up of unit-cube modules. Compared to past models, our model aims to newly capture two important practical aspects of real-world robots. First, modules often do not occupy an exact unit cube, but rather have features like bumps extending outside the allotted space so that modules c...
Versatile programmable materials have long been envisioned that can reconfigure themselves to adapt to changing use cases in adaptive infrastructure, space exploration, disaster response, and more. We introduce a robotic structural system as an implementation of programmable matter, with mechanical performance and scale on par with conventional hig...
We propose and numerically validate a patch reflectarray modeling approach suitable for small patches that describes each patch as a pair of polarizable magnetic dipoles. We introduce an extraction technique to obtain the effective polarizability of the patch dipoles via full-wave simulations on individual patches, followed by a beamforming design...
We propose and numerically validate a patch reflectarray modeling approach that describes each patch as a pair of polarizable magnetic dipoles. We introduce an extraction technique to obtain the effective polarizability of the patch dipoles via full-wave simulations on individual patches. This dipole framework serves as an alternative to the ray tr...
Ultralight materials present an opportunity to dramatically increase the efficiency of load-bearing aerostructures. To date, however, these ultralight materials have generally been confined to the laboratory bench-top, due to dimensional constraints of the manufacturing processes. We show a programmable material system applied as a large-scale, ult...
Architected lattice materials are some of the stiffest and strongest materials at ultra‐light density (<10 mg cm⁻³), but scalable manufacturing with high‐performance constituent materials remains a challenge that limits their widespread adoption in load‐bearing applications. We show mesoscale, ultra‐light (5.8 mg cm⁻³) fiber‐reinforced polymer comp...
The accidental untying of a shoelace while walking often occurs without warning. In this paper, we discuss the series of events that lead to a shoelace knot becoming untied. First, the repeated impact of the shoe on the floor during walking serves to loosen the knot. Then, the whipping motions of the free ends of the laces caused by the leg swing p...
We present a modular, reconfigurable system for building large structures. This system uses discrete lattice elements, called digital materials, to reversibly assemble ultralight structures that are 99.7% air and yet maintain sufficient specific stiffness for a variety of structural applications and loading scenarios. Design, manufacturing, and cha...
Real world systems that are candidates for vibrational energy harvesting rarely vibrate at a single frequency, nor are these frequencies constant over time. This necessitates that vibration harvesters operate over a wide bandwidth or tune their resonance. Most tunable devices require additional energy or active control to achieve resonance over var...
Questions
Question (1)
They were popular in the 1960-1980's, but are no longer standard.