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Gyroless Yaw-Estimating SystemAlgorithm estimates yaw of spacecraft from equations of motion and readings of nongyroscopic sensors. Intended to be used in monitoring and controlling yaw when yaw gyroscope fails. Modified version useful in monitoring and controlling yaw of terrestrial scientific instrument or aircraft.
Document ID
19930000650
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Stetson, John B., Jr.
(General Electric Co.)
Date Acquired
August 16, 2013
Publication Date
October 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 10
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
GSC-13459
Accession Number
93B10650
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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