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A design procedure and handling quality criteria for lateral directional flight control systemsA practical design procedure for aircraft augmentation systems is described based on quadratic optimal control technology and handling-quality-oriented cost functionals. The procedure is applied to the design of a lateral-directional control system for the F4C aircraft. The design criteria, design procedure, and final control system are validated with a program of formal pilot evaluation experiments.
Document ID
19730001410
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Stein, G. (Honeywell, Inc. Minneapolis, MN, United States)
Henke, A. H. (Honeywell, Inc. Minneapolis, MN, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1972
Publication Information
Publication: NASA, Washington 7th Ann. Conf. on Manual Control
Subject Category
Biotechnology
Accession Number
73N10137
Funding Number(s)
CONTRACT_GRANT: F33615-70-C-1190
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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