DocumentCode
1137376
Title
Proportional Navigation with a Maneuvering Target
Author
Guelman, M.
Author_Institution
Ministry of Defence Armament Development Authority Tel-Aviv, Israel
Issue
3
fYear
1972
fDate
5/1/1972 12:00:00 AM
Firstpage
364
Lastpage
371
Abstract
A qualitative analysis of the trajectories of a missile pursuing a maneuvering target according to the proportional navigation law is presented. Conditions for a missile to reach the target from any initial state are determined. The existence of a boundary for the required missile acceleration is demonstrated.
Keywords
Acceleration; Aerospace and electronic systems; Differential equations; Missiles; Navigation; Performance analysis; Time varying systems;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1972.309520
Filename
4102960
Link To Document