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The JPL orbit determination software systemThe Jet Propulsion Laboratory (JPL) orbit determination software system is described. Consisting of a set of computer programs, this system has been developed at JPL for the primary purpose of determining the flight path of deep-space mission spacecraft in NASA's planetary program. Secondary uses include science studies in celestial mechanics and extraterrestrial atmospherics. Attention is given to such features as the capability for processing 30 data types from up to 15 tracking stations, and for precise navigation to natural satellites of outer planets. In addition, the system contains models for such conditions as mascons, atmospheric drag, attitude control, and finite motor burns, to provide for extensive solve-on capabilities.
Document ID
19790063194
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ekelund, J. E.
(California Institute of Technology, Jet Propulsion Laboratory, Navigation Systems Section, Pasadena Calif., United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1979
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AAS PAPER 79-111
Meeting Information
Meeting: American Astronautical Society and American Institute of Aeronautics and Astronautics, Astrodynamics Specialist Conference
Location: Provincetown, MA
Start Date: June 25, 1979
End Date: June 27, 1979
Sponsors: American Astronautical Society, American Institute of Aeronautics and Astronautics
Accession Number
79A47207
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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