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Impact of longitudinal flying qualities upon the design of a transport with active controlsDirect constrained parameter optimization was used to optimally size a medium range transport for minimum direct operating cost. Several stability and control constraints were varied to study the sensitivity of the configuration to specifying the unaugmented flying qualities of transports designed with relaxed static stability. Additionally, a number of handling quality related design constants were studied with respect to their impact to the design.
Document ID
19800061699
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Sliwa, S. M.
(NASA Langley Research Center Flight Dynamics and Control Div., Hampton, Va., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 80-1570
Meeting Information
Meeting: Atmospheric Flight Mechanics Conference
Location: Danvers, MA
Start Date: August 11, 1980
End Date: August 13, 1980
Accession Number
80A45869
Distribution Limits
Public
Copyright
Other

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