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Analysis of augmented aircraft flying qualities through application of the Neal-Smith criterionThe Neal-Smith criterion is examined for possible applications in the evaluation of augmented fighter aircraft flying qualities. Longitudinal and lateral flying qualities are addressed. Based on the application of several longitudinal flying qualities data bases, revisions are proposed to the original criterion. Examples are given which show the revised criterion to be a good discriminator of pitch flying qualities. Initial results of lateral flying qualities evaluation through application of the Neal-Smith criterion are poor. Lateral aircraft configurations whose flying qualities are degraded by roll ratcheting effects map into the Level 1 region of the criterion. A third dimension of the criterion for flying qualities specification is evident. Additional criteria are proposed to incorporate this dimension into the criterion structure for flying qualities analysis.
Document ID
19820026927
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bailey, R. E.
(Calspan Advanced Technology Center Buffalo, NY, United States)
Smith, R. E.
(Calspan Advanced Technology Center Buffalo, NY, United States)
Date Acquired
August 10, 2013
Publication Date
August 1, 1981
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 81-1776
Meeting Information
Meeting: Guidance and Control Conference
Location: Albuquerque, NM
Start Date: August 19, 1981
End Date: August 21, 1981
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
82A10462
Distribution Limits
Public
Copyright
Other

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