DocumentCode :
1137302
Title :
Application of the Volterra Series to the Analysis and Design of an Angle Track Loop
Author :
Landau, Mark ; Leondes, C.T.
Author_Institution :
Hughes Aircraft Company Culver City, Calif.
Issue :
3
fYear :
1972
fDate :
5/1/1972 12:00:00 AM
Firstpage :
306
Lastpage :
318
Abstract :
A typical function of an angle tracking loop is to keep a radar antenna pointed at a target. The error in pointing is directly related to successful operation of the tracking device; therefore, its behavior is of interest. For a tracker with a general polynomial nonlinearity, an arbitrary initial pointing error, and a bounded deterministic input, a method is developed for finding upper bounds on the magnitude of the tracking error using Volterra series techniques. Convergence regions of the Volterra series are also obtained. Applications of these results are made to a second-order tracking device.
Keywords :
Aircraft; Cities and towns; Convergence; Geometry; Radar antennas; Radar tracking; Spaceborne radar; Target tracking; Tracking loops; Upper bound;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.1972.309513
Filename :
4102953
Link To Document :
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