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Optimal feedback strategies for pursuit-evasion and interception in a planeVariable-speed pursuit-evasion and interception for two aircraft moving in a horizontal plane are analyzed in terms of a coordinate frame fixed in the plane at termination. Each participant's optimal motion can be represented by extremal trajectory maps. These maps are used to discuss sub-optimal approximations that are independent of the other participant. A method of constructing sections of the barrier, dispersal, and control-level surfaces and thus determining feedback strategies is described. Some examples are shown for pursuit-evasion and the minimum-time interception of a straight-flying target.
Document ID
19830010474
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Rajan, N.
(NAS-NRC Washington, D.C., United States)
Ardema, M. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1983
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:84311
NASA-TM-84311
A-9177
Report Number: NAS 1.15:84311
Report Number: NASA-TM-84311
Report Number: A-9177
Accession Number
83N18745
Funding Number(s)
PROJECT: RTOP 505-34-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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