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Real-Time Estimation Of Aiming Error Of Spinning AntennaSpinning-spacecraft dynamics and amplitude variations in communications links studied from received-signal fluctuations. Mathematical model and associated analysis procedure provide real-time estimates of aiming error of remote rotating transmitting antenna radiating constant power in narrow, pencillike beam from spinning platform, and current amplitude of received signal. Estimates useful in analyzing and enhancing calibration of communication system, and in analyzing complicated dynamic effects in spinning platform and antenna-aiming mechanism.
Document ID
19920000430
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Dolinsky, Shlomo
(Caltech)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 7
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
NPO-17829
Accession Number
92B10430
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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