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