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Trial maneuver generation and selection in the Paladin tactical decision generation systemTo date, increased levels of maneuverability and controllability in aircraft have been postulated as tactically advantageous, but little research has studied maneuvers or tactics that make use of these capabilities. In order to help fill this void, a real-time tactical decision generation system for air combat engagements, Paladin, has been developed. Paladin models an air combat engagement as a series of discrete decisions. A detailed description of Paladin's decision making process is presented. This includes the sources of data used, methods of generating reasonable maneuvers for the Paladin aircraft, and selection criteria for choosing the 'best' maneuver. Simulation results are presented that show Paladin to be relatively insensitive to errors introduced into the decision process by estimation of future positional and geometric data.
Document ID
19930013899
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Chappell, Alan R.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Mcmanus, John W.
(NASA Langley Research Center Hampton, VA, United States)
Goodrich, Kenneth H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:107722
NASA-TM-107722
Report Number: NAS 1.15:107722
Report Number: NASA-TM-107722
Accession Number
93N23088
Funding Number(s)
PROJECT: RTOP 505-64-30-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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