Study of A Pursuit-Evasion Guidance Law for High Performance Aircraft

This paper discusses the study of a one-on-one aircraft pursuit-evasion gidance scheme for high performance aircraft. The research objective is to implement a guidance law derived earlier [1] using differential game theory [2] in conjunction with the theory of feedback linearization. Unlike earlier...

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Bibliographic Details
Published in:	1989 American Control Conference pp. 2469 - 2474
Main Authors:	Williams, Peggy S., Antoniewicz, Robert F., Duke, Eugene L., Menon, P.K.A.
Format:	Conference Proceeding
Language:	English
Published:	IEEE 01-06-1989
Subjects:	Content addressable storage Elevators Equations Feedback Game theory Geometry Military aircraft Optimal control Solid modeling Weapons
Online Access:	Get full text
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Summary:	This paper discusses the study of a one-on-one aircraft pursuit-evasion gidance scheme for high performance aircraft. The research objective is to implement a guidance law derived earlier [1] using differential game theory [2] in conjunction with the theory of feedback linearization. Unlike earlier research in this area, the present formulation explicitly recognizes the two sided nature of the pursuit-evasion scenario. Present research implements this guidance law in a realistic model of a modern high performance fighter aircraft [3]. The present paper will discuss the details of the guidance law, implementation in a highly detailed simulation of a high performance fighter, and numerical results for two engagement geometries. Modifications of the guidance law for on-board implementation will also be discussed.
DOI:	10.23919/ACC.1989.4790603