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A study of a proposed modified torsional agility metricA new candidate lateral agility metric, the modified torsional agility parameter, is proposed and tested through generic, nonlinear, non-real-time flight simulation programs of the F-18 and F-5A. The metric is aimed at quantifying high subsonic loaded roll capabilities which might be useful in modern air combat. The metric is considered to be straightforward for testing and measuring based on nonreal-time unmanned flight simulation. The metric is found to be sensitive to pilot input errors of less than full lateral stick to capture bank angle, when tested using unmanned flight simulations. It is suggested that, for redesigned configurations of both aircraft with improved lateral agility, the major benefit would be provided by fast and highly effective rudders, and a high level of pitch, roll, and yaw damping at moderate to high normal load factor levels.
Document ID
19910062559
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Valasek, John
(Kansas Univ. Lawrence, KS, United States)
Eggold, David P.
(Kansas Univ. Lawrence, KS, United States)
Downing, David R.
(Kansas, University Lawrence, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1991
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 91-2883
Meeting Information
Meeting: AIAA Atmospheric Flight Mechanics Conference
Location: New Orleans, LA
Country: United States
Start Date: August 12, 1991
End Date: August 14, 1991
Accession Number
91A47182
Funding Number(s)
CONTRACT_GRANT: NCC2-588
Distribution Limits
Public
Copyright
Other

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