DocumentCode :
1460497
Title :
Acoustic hit indicator
Author :
Levanon, Nadav
Author_Institution :
Dept. of Electr. Eng. Syst., Tel Aviv Univ., Israel
Volume :
37
Issue :
1
fYear :
2001
fDate :
1/1/2001 12:00:00 AM
Firstpage :
304
Lastpage :
309
Abstract :
An improved acoustic target is considered. Acoustic targets estimate the hit coordinates of a supersonic projectile using the time of arrival (TOA) of the supersonic shock wave at several acoustic transducers located in the vicinity of the target. An improved target allows oblique hits, likely in firing practices involving roaming infantry and armor. Four trajectory parameters are estimated: two hit coordinates (x,h) on a virtual, vertical, target plane; horizontal angle of incidence; projectile velocity. Explicit expressions are provided of the expected TOA measurements and their derivatives with respect to the estimated parameters. The expressions simplify a least-squares iterative algorithm and accelerate its convergence. Expected error contour maps are provided
Keywords :
Newton method; acoustic transducers; ballistics; convergence of numerical methods; direction-of-arrival estimation; least squares approximations; military equipment; projectiles; shock waves; weapons; Gauss-Newton method; acoustic hit indicator; acoustic transducers; armour; convergence; expected error contour maps; firing practice; hit coordinates; horizontal angle of incidence; hostile fire direction; improved acoustic target; least-squares iterative algorithm; oblique hits; projectile velocity; random measurement errors; roaming infantry; supersonic projectile; supersonic shock wave; time of arrival; trajectory parameters; virtual vertical target plane; Acceleration; Acoustic measurements; Acoustic transducers; Convergence; Electric shock; Iterative algorithms; Parameter estimation; Pressure measurement; Projectiles; Trajectory;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/7.913692
Filename :
913692
Link To Document :
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