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A multiple objective optimization approach to aircraft control systems designThe design of an aircraft lateral control system, subject to several performance criteria and constraints, is considered. While in the previous studies of the same model a single criterion optimization, with other performance requirements expressed as constraints, has been pursued, the current approach involves a multiple criteria optimization. In particular, a Pareto optimal solution is sought.
Document ID
19790063949
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Tabak, D.
(NASA Langley Research Center Hampton, VA, United States)
Schy, A. A.
(NASA Langley Research Center Hampton, VA, United States)
Johnson, K. G.
(NASA Langley Research Center Hampton, Va., United States)
Giesy, D. P.
(NASA Langley Research Center; Vought Corp. Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Aircraft Stability And Control
Meeting Information
Meeting: 1978 Conference on Decision and Control
Location: San Diego, CA
Start Date: January 10, 1979
End Date: January 12, 1979
Accession Number
79A47962
Distribution Limits
Public
Copyright
Other

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