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A microprocessor application to a strapdown laser gyro navigatorThe replacement of analog circuit control loops for laser gyros (path length control, cross axis temperature compensation loops, dither servo and current regulators) with digital filters residing in microcomputers is addressed. In addition to the control loops, a discussion is given on applying the microprocessor hardware to compensation for coning and skulling motion where simple algorithms are processed at high speeds to compensate component output data (digital pulses) for linear and angular vibration motions. Highlights are given on the methodology and system approaches used in replacing differential equations describing the analog system in terms of the mechanized difference equations of the microprocessor. Standard one for one frequency domain techniques are employed in replacing analog transfer functions by their transform counterparts. Direct digital design techniques are also discussed along with their associated benefits. Time and memory loading analyses are also summarized, as well as signal and microprocessor architecture. Trade offs in algorithm, mechanization, time/memory loading, accuracy, and microprocessor architecture are also given.
Document ID
19810003147
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Giardina, C.
(Singer-Kearfott Little Falls, NJ, United States)
Luxford, E.
(Singer-Kearfott Little Falls, NJ, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1980
Publication Information
Publication: NASA. Goddard Space Flight Center Aerospace Appl. of Microprocessors
Subject Category
Computer Operations And Hardware
Accession Number
81N11655
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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