DocumentCode
978229
Title
Linear Quadratic Differential Games Guidance Law for Dual Controlled Missiles
Author
Shima, Tal ; Golan, Oded M.
Author_Institution
Technion-Israel Inst. of Technol., Haifa
Volume
43
Issue
3
fYear
2007
fDate
7/1/2007 12:00:00 AM
Firstpage
834
Lastpage
842
Abstract
A novel guidance law designed specifically for a missile having forward and aft control systems is presented. For the derivation a linear quadratic differential games formulation of the end-game interception scenario is used. Conditions for achieving perfect intercept are given and new game spaces are presented. It is also shown that increasing the direct lift associated with the canard control allows intercepting targets with higher maneuvering capability, while for the tail control the effect is opposite.
Keywords
linear quadratic control; missile guidance; canard control; dual controlled missiles; end game interception scenario; guidance law; linear quadratic differential games; maneuvering capability; Aerodynamics; Character generation; Control systems; Delay; Force control; Missiles; Navigation; Nonlinear control systems; Programmable control; Tail;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.2007.4383577
Filename
4383577
Link To Document