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Doubly-Differenced Measurements for Orbit DeterminationsReport describes accurate method of determining orbit of low-altitude Earth satellite. Method insensitive to clock errors and provides continuous determination of orbit. Report examines effects of employing fewer ground stations, applying different solution strategies, and introducing fictitious thrust parameters to minimize geopotential modeling error - one of major error sources.
Document ID
19850000040
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Wu, S. C.
(CALTECH)
Ondraski, V. J.
(CALTECH)
Date Acquired
August 12, 2013
Publication Date
June 1, 1985
Publication Information
Publication: NASA Tech Briefs
Volume: 9
Issue: 1
ISSN: 0145-319X
Subject Category
Electronic Systems
Report/Patent Number
NPO-16111
Report Number: NPO-16111
ISSN: 0145-319X
Accession Number
85B10040
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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