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High dynamic GPS receiver using maximum likelihood estimation and frequency trackingA new high dynamic global positioning system (GPS) receiver is presented and its performance characterized by analysis, simulation, and demonstration. The demonstration receiver is a breadboard model capable of tracking a single simulated satellite signal in pseudorange and range rate. Pseudorange and range rate estimates are made once every 20 ms, using a maximum likelihood estimator, and are tracked by means of a third-order fading memory filter in a feedback configuration. The receiver tracks pseudorange with rms errors of under 1 m when subjected to simulated 50 g, 40 g/s circular trajectories. The tracking threshold is approximately 28 dB-Hz, which provides 12 dB margin relative to the minimum specified signal strength, assuming 3.5 dB system noise figure and 0 dBi antenna gain.
Document ID
19880028133
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hurd, W. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Statman, J. I.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Vilnrotter, V. A.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 13, 2013
Publication Date
July 1, 1987
Publication Information
Publication: IEEE Transactions on Aerospace and Electronic Systems
Volume: AES-23
ISSN: 0018-9251
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
ISSN: 0018-9251
Accession Number
88A15360
Funding Number(s)
CONTRACT_GRANT: AF TASK RE-182
Distribution Limits
Public
Copyright
Other

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