DocumentCode :
1410953
Title :
Comments on "Optimal guidance of proportional navigation"
Author :
Rao, S. Koteswara
Author_Institution :
Naval Sci. & Technol. Lab., Min. of Defense, Visakahpatnam, India
Volume :
34
Issue :
3
fYear :
1998
fDate :
7/1/1998 12:00:00 AM
Firstpage :
981
Lastpage :
982
Abstract :
The author comments on the work of P.-J. Yuan (ibid. vol. 33, pp. 1007-1011, 1997) in which involved with the target motion parameters seem to have been ignored. In practice, the contact is obtained when the target tracking is on and target motion parameters (range, course, bearing, speed, and acceleration of the target) are found out. Various sophisticated versions of Kalman filter generate estimates with minimum variance. As long as the measurements are corrupted with noise, the estimates contain errors and these are described by covariance matrix of the estimated target state vector.
Keywords :
Kalman filters; covariance matrices; missile guidance; motion estimation; target tracking; Kalman filter; bearing; course; covariance matrix; estimates with minimum variance; noise corrupted measurements; optimal guidance; proportional navigation; range; speed; target acceleration; target motion parameters; target state vector; target tracking; Acceleration; Covariance matrix; Motion analysis; Motion estimation; Navigation; Noise measurement; Parameter estimation; State estimation; Target tracking; Weapons;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/7.705907
Filename :
705907
Link To Document :
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