DocumentCode :
3423161
Title :
Aeolotropic filter design and measurement gating for remote tracking with gridlock error
Author :
Chen, Richard C. ; Blair, William D.
Author_Institution :
Naval Surface Warfare Center, Dahlgren, VA, USA
fYear :
1997
fDate :
9-11 Mar 1997
Firstpage :
75
Lastpage :
80
Abstract :
Analyzes the effect of gridlock (i.e. alignment) errors on a target track filtering algorithm used for tracking with radar measurements from a remote platform. The case considered is that in which two ships are located in a 2D Cartesian coordinate system, and radar measurements from one (remote) platform are used by another (local) platform to estimate the target position and velocity in the local platform coordinate system. Relative location errors only are considered. The effects of gridlock error on the parameters of the remote platform filtering algorithm, as determined by a set of given design criteria, are investigated. In particular, the effects of gridlock error on the filter measurement gating threshold and filter gain coefficients are analyzed
Keywords :
errors; position measurement; radar tracking; ships; target tracking; tracking filters; velocity measurement; 2D Cartesian coordinate system; aeolotropic filter design; alignment errors; design criteria; filter gain coefficients; filter measurement gating threshold; gridlock error; local platform coordinate system; radar measurements; relative location errors; remote platform; remote tracking; ships; target position estimation; target track filtering algorithm; target velocity estimation; Algorithm design and analysis; Coordinate measuring machines; Filtering algorithms; Filters; Gain measurement; Goniometers; Marine vehicles; Radar measurements; Radar tracking; Target tracking;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
System Theory, 1997., Proceedings of the Twenty-Ninth Southeastern Symposium on
Conference_Location :
Cookeville, TN
ISSN :
0094-2898
Print_ISBN :
0-8186-7873-9
Type :
conf
DOI :
10.1109/SSST.1997.581582
Filename :
581582
Link To Document :
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