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Structural Aspects of Flexible Aircraft ControlThe specialists' meeting dealt with design issues and more specifically Structural Aspects of Flexible Aircraft Control. Twenty six papers and a keynote address were presented with the following objectives: How the design methods used in the development of military fighter aircraft can be improved, and applied to transport aircraft design applications. There were three sessions covering the following topics: (1) Aeroservoelasticity; (2) Active Control for Flexible Structures I; and (3) Active Control for Flexible Structures II.
Document ID
20000053157
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Date Acquired
August 19, 2013
Publication Date
May 1, 2000
Publication Information
Publication: Structural Aspects of Flexible Aircraft Control
Publisher: North Atlantic Treaty Organization
ISBN: 92-837-0014-7
Subject Category
Aeronautics (General)
Report/Patent Number
Report Number: RTO-MP-36
Report Number: AC/323(AVT)TP/17
ISBN: 92-837-0014-7
RTO-MP-36
AC/323(AVT)TP/17
Meeting Information
Meeting: Specialists'' Meeting of the RTO Applied Vehicle Technology Panel (AVT): Structural Aspects of Flexible Aircraft Control
Location: Ottawa, Ontario
Country: CA
Start Date: October 18, 1999
End Date: October 20, 1999
Sponsors: North Atlantic Treaty Organization
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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