DocumentCode :
1442002
Title :
Tracking an incoming ballistic missile using an extended interval Kalman filter
Author :
Siouris, George M. ; Chen, Guanrong ; Wang, Jianrong
Author_Institution :
Air Force Inst. of Technol., Wright-Patterson AFB, OH, USA
Volume :
33
Issue :
1
fYear :
1997
Firstpage :
232
Lastpage :
240
Abstract :
The important tracking problem by radar of an incoming ballistic missile system, which contains uncertainty in modeling and noise in both dynamics and measurements, is studied. The classical extended Kalman filter (EKF) is no longer applicable to such an uncertain system, and so a new extended interval Kalman filter (EIKF) is developed for tracking the missile system. Computer simulation is presented to show the effectiveness of the EIKF algorithm for this uncertain and nonlinear ballistic missile tracking problem.
Keywords :
Kalman filters; digital simulation; military computing; missiles; noise; nonlinear systems; radar signal processing; radar tracking; simulation; uncertainty handling; dynamics; extended interval Kalman filter; incoming ballistic missile; measurements; modeling; nonlinear ballistic missile tracking; uncertainty; Aerospace engineering; Azimuth; Force measurement; Laser radar; Military computing; Missiles; Optical devices; Radar measurements; Radar tracking; Target tracking;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/7.570753
Filename :
570753
Link To Document :
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