DocumentCode
1147357
Title
Missile Guidance Based on Kalman Filter Estimation of Target Maneuver
Author
Tang, Y.M. ; Borrie, J.A.
Author_Institution
Luoyang Dynamic Institute Chinese Aeronautical Establishment People´´s Republic of China
Issue
6
fYear
1984
Firstpage
736
Lastpage
741
Abstract
A fourth-order extended Kalman filter is developed to estimate target maneuvers, and a guidance law using these estimates is implemented.
Keywords
Acceleration; Aerodynamics; Equations; Gaussian noise; Missiles; Noise measurement; Sampling methods; State estimation; Time measurement; Virtual manufacturing;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1984.310456
Filename
4103979
Link To Document