DocumentCode :
763453
Title :
Assessment of air-to-air missile guidance and control technology
Author :
Cloutier, James R. ; Evers, Johnny H. ; Feeley, Joseph J
Author_Institution :
Air Force Armament Lab., Eglin AFB, FL, USA
Volume :
9
Issue :
6
fYear :
1989
Firstpage :
27
Lastpage :
34
Abstract :
Current air-to-air missile guidance and control technology is assessed. Areas explored include target state estimation, advanced guidance laws, and bank-to-turn autopilots. The assumptions, benefits, and limitations of recent applications of nonlinear filtering, adaptive filtering, modern control, adaptive control, dual control, differential game theory, and modern control design techniques to the air-to-air missile problem are discussed.<>
Keywords :
aerospace computer control; missiles; reviews; adaptive control; adaptive filtering; advanced guidance laws; air-to-air missile guidance; bank-to-turn autopilots; control technology; differential game theory; dual control; modern control; modern control design techniques; nonlinear filtering; target state estimation; Acceleration; Adaptive control; Adaptive filters; Aerodynamics; Filtering; Force control; Missiles; Modems; State estimation; Target tracking;
fLanguage :
English
Journal_Title :
Control Systems Magazine, IEEE
Publisher :
ieee
ISSN :
0272-1708
Type :
jour
DOI :
10.1109/37.41440
Filename :
41440
Link To Document :
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