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A differential game solution to the Coplanar tail-chase aerial combat problemNumerical results obtained in a simplified version of the one on one aerial combat problem are presented. The primary aim of the data is to specify the roles of pursuer and evader as functions of the relative geometry and of the significant physical parameters of the problem. Numerical results are given in a case in which the slower aircraft is more maneuverable than the faster aircraft. A third order dynamic model of the relative motion is described, for which the state variables are relative range, bearing, and heading. The ranges at termination are arbitary in the present version of the problem, so the weapon systems of both aircraft can be visualized as forward firing high velocity weapons, which must be aimed at the tail pipe of the evader. It was found that, for the great majority of the ralative geometries, each aircraft can evade the weapon system of the other.
Document ID
19760010828
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Merz, A. W.
(Aerophysics Research Corp. Bellevue, WA, United States)
Hague, D. S.
(Aerophysics Research Corp. Bellevue, WA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Systems Analysis
Report/Patent Number
NASA-CR-137809
Report Number: NASA-CR-137809
Accession Number
76N17916
Funding Number(s)
CONTRACT_GRANT: NAS2-8844
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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