DocumentCode
835551
Title
Accurate solution of proportional navigation for maneuvering targets
Author
Mahapatra, R. ; Shukla, U.S.
Author_Institution
Dept. of Aerosp. Eng., Indian Inst. of Sci., Bangalore, India
Volume
25
Issue
1
fYear
1989
Firstpage
81
Lastpage
89
Abstract
An accurate solution is presented of the nonlinear differential equations describing motion under proportional navigation when the target is laterally maneuvering. A quasilinearization (QL) approach is used, followed by a perturbation technique to obtain closed-form solutions for trajectory parameters. An explicit expression for the pursuer lateral acceleration is derived and shown to contain contributions due to initial heading error and target maneuver, with a coupling between the two effects. The solution is shown to be a substantial and consistent generalization or an earlier accurate solution for nonmaneuvering targets and also of classical linear solutions for maneuvering targets. The generalized QL solution presented provides very accurate estimates of pursuer lateral acceleration over a much broader range of engagement geometries and target maneuvers than presently available closed-form solutions.<>
Keywords
military systems; nonlinear differential equations; proportional control; closed-form solutions; laterally maneuvering targets; missile guidance; nonlinear differential equations; perturbation technique; proportional navigation; quasilinearization; trajectory parameters; Acceleration; Closed-form solution; Force control; Geometry; Linear approximation; Motion analysis; Motion control; Navigation; Nonlinear equations; Perturbation methods;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/7.18664
Filename
18664
Link To Document