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 The classical extended Kalman filter (EKF) is no longer applicable to such an uncertain system, and so a new extended interval Kalman filter (EIKF) is developed for tracking the missile system.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