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
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;
Conference_Titel :
American Control Conference, 1988
Conference_Location :
Atlanta, Ga, USA