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Differential Interferometry For Spacecraft NavigationReport proposes use of differential very-long-baseline interferometry to measure accurately angular separation, viewed from Earth, of two spacecraft near another planet. One spacecraft would be in orbit around planet on trajectory already determined accurately, relative to planet, by conventional Doppler tracking. Other spacecraft would be approaching planet. Use of differential very-long-baseline interferometry "tie" between two spacecraft and previously determined "tie" between orbiter and planet increases accuracy of navigation of approaching spacecraft relative to planet.
Document ID
19930000016
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Edwards, Charles D.
(Caltech)
Border, James S.
(Caltech)
Folkner, William M.
(Caltech)
Wood, Lincoln J.
(Caltech)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 1
ISSN: 0145-319X
Subject Category
Electronic Systems
Report/Patent Number
NPO-18417
Report Number: NPO-18417
ISSN: 0145-319X
Accession Number
93B10016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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