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Study of a pursuit-evasion guidance law for high performance aircraftThe study of a one-on-one aircraft pursuit-evasion guidance scheme for high-performance aircraft is discussed. The research objective is to implement a guidance law derived earlier using differential game theory 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. The present research implements the guidance law in a realistic model of a modern high-performance fighter aircraft. Also discussed are 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 onboard implementation is also discussed.
Document ID
19890066713
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Williams, Peggy S.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Menon, P. K. A.
(Georgia Institute of Technology Atlanta, United States)
Antoniewicz, Robert F.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Duke, Eugene L.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Aircraft Stability And Control
Meeting Information
Meeting: 1989 American Control Conference
Location: Pittsburgh, PA
Country: United States
Start Date: June 21, 1989
End Date: June 23, 1989
Accession Number
89A54084
Distribution Limits
Public
Copyright
Other

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