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Flight Vehicle Integration Panel Workshop on Pilot Induced OscillationsInstability of the pilot/airframe combination has been a problem of manned flight. Rapid advances made in aviation following World War 2 greatly increased the incidence of PIO problems and the amount of research and development work aimed at understanding and mitigating these difficulties. Criteria and requirements were developed to be used in design to obtain satisfactory PIO qualities, but, in spite of all this work and the great flexibility in available modern control design technologies, PIO problems still often occur with new aircraft. It is clear that a universal solution of the PIO problem still evades the engineering community. The cost of these problems financially and in program delay is significant. This AGARD Flight Mechanics Workshop summary report contains presentations and discussions that aim toward the elimination and avoidance of PIO's by increasing the knowledge of PIO's and the problems associated with them.
Document ID
19950024640
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Date Acquired
August 16, 2013
Publication Date
January 1, 1995
Publication Information
Publication: AGARD Flight Vehicle Integration Panel Workshop on Pilot Induced Oscillations
Publisher: North Atlantic Treaty Organization
ISBN: 92-836-1013-X
Subject Category
Air Transportation And Safety
Report/Patent Number
AGARD-CP-335
ISBN: 92-836-1013-X
Report Number: AGARD-AR-335
Accession Number
95N31061
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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