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Landing flying qualities evaluation criteria for augmented aircraftThe criteria evaluated were: Calspan Neal-Smith; Onstott (Northrop Time Domain); McDonnell-Douglas Equivalent System Approach; R. H. Smith Criterion. Each criterion was applied to the same set of longitudinal approach and landing flying qualities data. A revised version of the Neal-Smith criterion which is applicable to the landing task was developed and tested against other landing flying qualities data. Results indicated that both the revised Neal-Smith criterion and the Equivalent System Approach are good discriminators of pitch landing flying qualities; Neal-Smith has particular merit as a design guide, while the Equivalent System Approach is well suited for development of appropriate military specification requirements applicable to highly augmented aircraft.
Document ID
19810005458
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Radford, R. C.
(Calspan Advanced Technology Center Buffalo, NY, United States)
Smith, R.
(Calspan Advanced Technology Center Buffalo, NY, United States)
Bailey, R.
(Calspan Advanced Technology Center Buffalo, NY, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1980
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-163097
CALSPAN-6339-F-3
Report Number: NASA-CR-163097
Report Number: CALSPAN-6339-F-3
Accession Number
81N13969
Funding Number(s)
PROJECT: RTOP 505-06-64
CONTRACT_GRANT: NAS4-2534
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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