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Error modeling for differential GPSDifferential Global Positioning System (DGPS) positioning is used to accurately locate a GPS receiver based upon the well-known position of a reference site. In utilizing this technique, several error sources contribute to position inaccuracy. This thesis investigates the error in DGPS operation and attempts to develop a statistical model for the behavior of this error. The model for DGPS error is developed using GPS data collected by Draper Laboratory. The Marquardt method for nonlinear curve-fitting is used to find the parameters of a first order Markov process that models the average errors from the collected data. The results show that a first order Markov process can be used to model the DGPS error as a function of baseline distance and time delay. The model's time correlation constant is 3847.1 seconds (1.07 hours) for the mean square error. The distance correlation constant is 122.8 kilometers. The total process variance for the DGPS model is 3.73 sq meters.
Document ID
19950022295
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Blerman, Gregory S.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Date Acquired
September 6, 2013
Publication Date
May 12, 1995
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
CSDL-T-1241
NASA-CR-188367
NAS 1.26:288367
Report Number: CSDL-T-1241
Report Number: NASA-CR-188367
Report Number: NAS 1.26:288367
Accession Number
95N28716
Funding Number(s)
CONTRACT_GRANT: NAS9-18426
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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