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Flying Qualities Research ChallengesTraditional flying qualities requirements for airplane dynamics are based on airplane modal response characteristics derived from linear small-perturbation analysis. These requirements are supported by a large experimental data base. The challenge to the flying qualities community is to demonstrate how flying qualities, the control system and aircraft configuration are still closely linked. This is evident in the definition of flying qualities and, as far as pilots are concerned, that flying qualities are still the measure of overall design success.
Document ID
19880046867
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Steven M Sliwa
(Langley Research Center Hampton, United States)
Virginia B Marks
(Langley Research Center Hampton, United States)
Frank L George
(Wright Laboratory Wright-Patterson Air Force Base, United States)
J Victor Lebacqz
(Ames Research Center Mountain View, United States)
David Key
(Ames Research Center Mountain View, United States)
Donald T Berry
(Dryden Flight Research Center Rosamond, California, United States)
Date Acquired
August 13, 2013
Publication Date
August 1, 1987
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Aircraft Stability and Control
Meeting Information
Meeting: IEEE National Aerospace and Electronics Conference (NAECON)
Location: Dayton, OH
Country: US
Start Date: May 18, 1987
End Date: May 22, 1987
Sponsors: Institute of Electrical and Electronics Engineers
Accession Number
88A34094
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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