NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Emerging technologies in microguidance and controlEmploying recent advances in microfabrication, the Charles Stark Draper Laboratory has developed inertial guidance instruments of very small size and low cost. Microfabrication employs the batch processing techniques of solid state electronics, such as photolithography, diffusion, and etching, to carve mechanical parts. Within a few years, microfabricated gyroscopes should perform in the 10 to 100 deg/h range. Microfabricated accelerometers have demonstrated performance in the 50 to 500 microgravity range. These instruments will result in not only the redesign of conventional military products, but also new applications that could not exist without small, inexpensive sensors and computing. Draper's microfabricated accelerometers and gyroscopes will be described and test results summarized. Associated electronics and control issues will also be addressed. Gimballed, vibrating gyroscopes and force rebalance accelerometers constructed from bulk silicon, polysilicon surface-machined tuning fork gyroscopes, and quartz resonant accelerometers and gyroscopes are examined. Draper is pursuing several types of devices for the following reasons: to address wide ranges of performance, to realize construction in a flat pack, and to lessen the risks associated with emerging technologies.
Document ID
19940025284
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Weinberg, Marc S.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Date Acquired
September 6, 2013
Publication Date
June 15, 1993
Publication Information
Publication: JPL, Proceedings of the Workshop on Microtechnologies and Applications to Space Systems
Subject Category
Aircraft Communications And Navigation
Accession Number
94N29788
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available