NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Integrated low power digital gyro control electronicsEmbodiments of the invention generally encompass a digital, application specific integrated circuit (ASIC) has been designed to perform excitation of a selected mode within a vibratory rate gyroscope, damping, or force-rebalance, of other modes within the sensor, and signal demodulation of the in-phase and quadrature components of the signal containing the angular rate information. The ASIC filters dedicated to each channel may be individually programmed to accommodate different rate sensor designs/technology or variations within the same class of sensors. The ASIC architecture employs a low-power design, making the ASIC, particularly suitable for use in power-sensitive applications.
Document ID
20080005072
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
M'Closkey, Robert
Challoner, A. Dorian
Grayver, Eugene
Hayworth, Ken J.
Date Acquired
August 24, 2013
Publication Date
July 5, 2005
Subject Category
Computer Operations And Hardware
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-603557
Patent Number: US-PATENT-6,915,215
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-6,915,215
Patent Application
US-PATENT-APPL-SN-603557
No Preview Available