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Trajectory-Estimation Error AnalysisOrbital and Geodetic Parameter Estimation Error Analysis Program (ORAN) is Bayesian least-squares simulation program for orbital trajectories. ORAN does not process data; rather, computes accuracy of results of data reduction if measurements are processed by minimum-variance data-reduction program. Actual data used to provide time when given measurement was available and estimated noise on that measurement.
Document ID
19820000193
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Putney, B.
Date Acquired
August 10, 2013
Publication Date
March 1, 1983
Publication Information
Publication: NASA Tech Briefs
Volume: 7
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
GSC-12766
ISSN: 0145-319X
Report Number: GSC-12766
Accession Number
82B10193
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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