DocumentCode
1150810
Title
High Dynamic GPS Receiver Using Maximum Likelihood Estimationand Frequency Tracking
Author
Hurd, W.J. ; Statman, J.I. ; Vilnrotter, V.A.
Author_Institution
Jet Propulsion Laboratory, 4800 Oak Grove Drive, Pasadena, CA 91109
Issue
4
fYear
1987
fDate
7/1/1987 12:00:00 AM
Firstpage
425
Lastpage
437
Abstract
A new high dynamic global positioning system (GPS) receiver ispresented and its performance characterized by analysis,simulation, and demonstration. The demonstration receiver is abreadboard model capable of tracking a single simulated satellitesignal in pseudorange and range rate. Pseudorange and range rateestimates are made once every 20 ms, using a maximum likelihoodestimator, and are tracked by means of a third-order fadingmemory filter in a feedback configuration. The receiver trackspseudorange with rms errors of under 1 m when subjected tosimulated 50 g, 40 g/s circular trajectories. The tracking thresholdis approximately 28 dB·Hz, which provides 12 dB margin relativethe the minimum specified signal strength, assuming 3.5 dB systemnoise figure and 0 dB antenna gain.
Keywords
Acceleration; Aerodynamics; Bandwidth; Delay estimation; Frequency estimation; Global Positioning System; Maximum likelihood estimation; Satellites; Tracking loops; Vehicle dynamics;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1987.310876
Filename
4104371
Link To Document