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Presentation of flight control design and handling quality commonality by separate surface stability augmentation for the family of commuter airplanesThe methodology and results for a flight control design and implementation for common handling qualities by Separate Surface Stability Augmentation (SSSA) for the family of commuter airplanes are contained. The open and closed loop dynamics and the design results of augmenting for common handling qualities are presented. The physical and technology requirements are presented for implementing the SSSA system. The conclusion of this report and recommendations for changes or improvement are discussed.
Document ID
19880010087
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hensley, Douglas
(Kansas Univ. Lawrence, KS, United States)
Creighton, Thomas
(Kansas Univ. Lawrence, KS, United States)
Haddad, Raphael
(Kansas Univ. Lawrence, KS, United States)
Hendrich, Louis
(Kansas Univ. Lawrence, KS, United States)
Morgan, Louise
(Kansas Univ. Lawrence, KS, United States)
Russell, Mark
(Kansas Univ. Lawrence, KS, United States)
Swift, Gerald
(Kansas Univ. Lawrence, KS, United States)
Date Acquired
September 5, 2013
Publication Date
May 13, 1987
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.26:182567
NASA-CR-182567
Report Number: NAS 1.26:182567
Report Number: NASA-CR-182567
Accession Number
88N19471
Funding Number(s)
CONTRACT_GRANT: NGT-21-002-080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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