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An autonomous Nimbus Doppler positioning systemA single-pass Doppler positioning system was developed at the GSFC in support of the Nimbus-6 mission. The system was designed to satisfy the following requirements: compatibility with the PDP 11/70 minicomputer; single-pass recovery of up to 250 positions with a two-sigma accuracy of 5 km; high reliability with a minimum of human interaction; and near real-time responsiveness. The system consists of a numerical integrator which includes only the J2 term (earth flattening) of the earth's gravity field, an editing routine, a first guess algorithm, a least squares position recovery program, and a routine for generating a 95% confidence circle based on a computer covariance matrix. An analysis and quantification of the following error sources that limit system accuracy are presented: orbit error, radial aliasing, computational difficulties with overhead passes, oscillator drift, and ambiguity problems. Results of system reliability tests and sample outputs are included.
Document ID
19820029100
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Garza-Robles, R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Argentiero, P.
(U.S. Defense Mapping Agency, Hydrographic/Topographic Center Washington, DC, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1981
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Meeting Information
Meeting: In: National Aerospace Meeting
Location: Trevose, PA
Start Date: April 8, 1981
End Date: April 10, 1981
Accession Number
82A12635
Distribution Limits
Public
Copyright
Other

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