DocumentCode :
982416
Title :
Closed-form solution of pure proportional navigation
Author :
Becker, Klaus
Author_Institution :
Forschungsinst. fuer Funk & Math., Wachtberg-Werthhoven, West Germany
Volume :
26
Issue :
3
fYear :
1990
fDate :
5/1/1990 12:00:00 AM
Firstpage :
526
Lastpage :
533
Abstract :
The closed-form solution of the equations of motion of an ideal missile pursuing a nonmaneuvering target according to the pure proportional navigation law is obtained as a function of the polar coordinates for all real navigation constants N⩾2. The solution is given in the form of a uniformly convergent infinite product which reduces to a product of a finite number of factors if the navigation constant is a rational number. The solution is discussed, and necessary and sufficient conditions are stated for vanishing, bounded, and unbounded missile acceleration in the final phase of pursuit
Keywords :
missiles; navigation; acceleration; closed-form solution; differential equations; equations of motion; missiles guidance; nonmaneuvering target; polar coordinates; pure proportional navigation; pursuit; trajectories; Acceleration; Closed-form solution; Differential equations; Equations; Erbium; Geometry; Missiles; Navigation; Nonlinear systems; Sufficient conditions; Virtual manufacturing;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/7.106131
Filename :
106131
Link To Document :
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