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GPS early-orbit subsystem for earth satellitesThe early-orbit capability of the Goddard Trajectory Determination System, which determines starting vectors for earth satellites from angles-only or range-angles observations, is described and documented. Early-orbit results obtained from a variety of satellites, data types and methods of solution are also presented.
Document ID
19730019002
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Laczo, V. T.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Maury, J. L.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1972
Subject Category
Space Sciences
Report/Patent Number
NASA-TM-X-66286
X-552-72-502
Report Number: NASA-TM-X-66286
Report Number: X-552-72-502
Accession Number
73N27734
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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