DocumentCode :
487217
Title :
Application of the Mixed Guidance Strategy Concept in 3D
Author :
Forte, Isaac ; Shinar, Josef
Author_Institution :
Doctoral Student, Faculty of Aeronautical Engineering, Technion-Israel Institute of Technology, Haifa 32000, Israel
fYear :
1988
fDate :
15-17 June 1988
Firstpage :
149
Lastpage :
154
Abstract :
In recent previous works, dealing with the terminal phase of the missile-aircraft encounter in noisy environment, a new approach of "mixed guidance strategy" was proposed for an assumed planar geometry. If the target aircraft maneuvers and applies electronic jinking simultaneously, the problem becomes a three-dimensional one. The present paper investigates this problem and shows that in a three dimensional scenario the optimal "mixed" guidance strategy has to be determined by a genuine three-dimensional design procedure.
Keywords :
Acceleration; Aerospace electronics; Aerospace engineering; Aircraft; Control systems; Equations; Games; Geometry; Missiles; Motion control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1988
Conference_Location :
Atlanta, Ga, USA
Type :
conf
Filename :
4789707
Link To Document :
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