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There are a total of 13 record(s) matching your query.
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Performance of differenced range data types in Voyager navigation
Author(s): Taylor, T. H.; Campbell, J. K.; Jacobson, R. A.; Moultrie, B.; Nichols, R. A., Jr.; Riedel, J. E.
Abstract: Voyager radio navigation made use of a differenced rage data type for both Saturn encounters because of the low declination singularity of Doppler data. Nearly simultaneous two-way range from two-station baselines was ...
NASA Center: Jet Propulsion Laboratory Publication Year: 1982
Added to NTRS: 2008-11-10
Accession Number: 83N14329; Document ID: 19830006058
The performance of differential VLBI delay during interplanetary cruise
Author(s): Moultrie, B.; Wolff, P. J.; Taylor, T. H.
Abstract: Project Voyager radio metric data are used to evaluate the orbit determination abilities of several data strategies during spacecraft interplanetary cruise. Benchmark performance is established with an operational data ...
NASA Center: Jet Propulsion Laboratory Publication Year: 1984
Added to NTRS: 2004-11-03
Accession Number: 84A41575; Document ID: 19840058788; Report Number: AIAA PAPER 84-2048
Performance of differenced range data types in Voyager navigation
Author(s): Taylor, T. H.; Campbell, J. K.; Jacobson, R. A.; Moultrie, B.; Nichols, R. A., Jr.; Riedel, J. E.
Abstract: Previously cited in issue 19, p. 2992, Accession no. A82-38893
NASA Center: Jet Propulsion Laboratory Publication Year: 1984
Added to NTRS: 2004-11-03
Accession Number: 84A32707; Document ID: 19840049920
Performance of differenced range data types in Voyager navigation
Author(s): Taylor, T. H.; Campbell, J. K.; Jacobson, R. A.; Moultrie, B.; Nichols, R. A., Jr.; Riedel, J. E.
Abstract: Voyager radio navigation made use of differenced range data type for both Saturn encounters because of the low declination singularity of Doppler data. Nearly simultaneous two-way range from two-station baselines was ...
NASA Center: Jet Propulsion Laboratory Publication Year: 1982
Added to NTRS: 2004-11-03
Accession Number: 82A38893; Document ID: 19820055358; Report Number: AIAA PAPER 82-1473
Application of unconnected phase narrowband Delta VLBI to deep space navigation
Author(s): Ellis, J.; Moultrie, B.; Smith, C. B.
Abstract: Unconnected phase narrowband Delta VLBI data strategies are evaluated for enhancing deep space cruise navigation and for rapidly redetermining the spacecraft trajectory after a midcourse correction maneuver. Results of a ...
NASA Center: Jet Propulsion Laboratory Publication Year: 1981
Added to NTRS: 2004-11-03
Accession Number: 81A45805; Document ID: 19810061401; Report Number: AAS PAPER 81-114
Differential Very Long Baseline Interferometry (delta VLBI) spacecraft tracking system demonstration. Part 2: Data acquisition and processing
Author(s): Christensen, C. S.; Moultrie, B.; Callahan, P. S.; Donivan, F. F.; Wu, S. C.
Abstract: A set of experiments in the use of Differential Very Long Baseline Interferometry (delta VLBI) for spacecraft navigation were completed. Data using both Voyager spacecraft and a single quasar were acquired during the Jupiter ...
NASA Center: Jet Propulsion Laboratory Publication Year: 1980
Added to NTRS: 2004-11-03
Accession Number: 81N13215; Document ID: 19810004704
Galileo Probe delivery and Orbiter approach orbit determination
Author(s): Kenyon, P. R.; Moultrie, B.; Kechichian, J. A.; Nicholson, F. T.
Abstract: The configuration of the Galileo mission, in which the Probe and Orbiter are joined as a single spacecraft (until five months before Jupiter encounter, when the Probe will be released into the atmosphere for the Io flyby) is ...
NASA Center: Jet Propulsion Laboratory Publication Year: 1987
Added to NTRS: 2004-11-03
Accession Number: 87A22413; Document ID: 19870035139; Report Number: AIAA PAPER 87-0096
Galilean satellite tour orbit determination assessment
Author(s): Moultrie, B.; Kenyon, P. R.; Kechichian, J. A.; Davis, R. P.; Nicholson, F. T.
Abstract: Results are given which demonstrate the ability of the orbit determination system to satisfy accuracy requirements in support of the Galileo Project's planned tour of Jupiter's satellites. The results are derived through the ...
NASA Center: Jet Propulsion Laboratory Publication Year: 1987
Added to NTRS: 2004-11-03
Accession Number: 87A22412; Document ID: 19870035138; Report Number: AIAA PAPER 87-0095
Determining spacecraft angular position with Delta VLBI - The Voyager demonstration
Author(s): Border, J. S.; Donivan, F. F.; Finley, S. G.; Hildebrand, C. E.; Moultrie, B.; Skjerve, L. J.
Abstract: A demonstration of a new VLBI-based radio metric data type for interplanetary navigation has been conducted using the Voyager spacecraft on their approach to Saturn. Pseudo-range measurements from stations on ...
NASA Center: Jet Propulsion Laboratory Publication Year: 1982
Added to NTRS: 2004-11-03
Accession Number: 82A40018; Document ID: 19820056483; Report Number: AIAA PAPER 82-1471
Geosynchronous orbiter tracking by VLBI - Demonstration results
Author(s): Donivan, F. F., Jr.; Border, J. S.; Moultrie, B.
Abstract: Results are presented on two experiments which were designed to demonstrate the feasibility of tracking geosynchronous satellites to an accuracy of 5 meters using Very-Long-Baseline Interferometry (VLBI). A communications ...
NASA Center: Jet Propulsion Laboratory Publication Year: 1984
Added to NTRS: 2004-11-03
Accession Number: 84A44227; Document ID: 19840061440; Report Number: AIAA PAPER 84-2051
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