DocumentCode
1126010
Title
The closed-form solution of true proportional navigation
Author
Guelman, M.
Author_Institution
Ministry of Defence, Tel Aviv, Israel
Issue
4
fYear
1976
fDate
7/1/1976 12:00:00 AM
Firstpage
472
Lastpage
482
Abstract
The closed-form solution of the equations of motion of an ideal missile pursuing a nonmaneuvering target according to the true propotional navigation law is obtained. An analysis of the solution is performed, and the conditions necessary for the missile to reach the target are determined.
Keywords
Acceleration; Closed-form solution; Missiles; Navigation; Performance analysis; Proportional control; Rotation measurement; Trajectory;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1976.308328
Filename
4101676
Link To Document