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The Performance of Differential VLBI Delay During Interplanetary CruiseProject Voyager radio metric data are used to evaluate the orbit determination utilities of several data strategies during spacecraft interplanetary cruise. Benchmark performance is established with an operational data strategy of conventional coherent Doppler, coherent range, and explicitly differenced range data from two intercontinental baselines to ameliorate the low declination singularity of the Doppler data. Employing a Voyager operations trajectory as a reference, the performance of the operational data strategy is compared to the performances of data strategies using differential VLBI delay data (spacecraft delay minus quasar delay) in combination with the aforementioned conventional data types. The comparison of strategy performances indicates that high accuracy cruise orbit determination can be achieved with a data strategy employing differential VLBI delay data, where the quantity of coherent radio metric data was reduced by over 95% with a concurrent 90% reduction in the DSN time allocated to radio metric data acquisition.
Document ID
19850005675
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Moultrie, B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wolff, P. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Taylor, T. H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 12, 2013
Publication Date
November 15, 1984
Publication Information
Publication: The Telecommunications and Data Acquisition Rept.
Subject Category
Communications And Radar
Accession Number
85N13984
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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