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Bandwidth Criteria for Category I and II PIOsThis presentation gives information on: pitch criteria based on airplane Bandwidth; apply research, experimental, operational data; compare Smith-Geddes, Gibson, Neal-Smith criteria; bandwidth criteria for Category II PIO; control/response sensitivity and PIO; extension to roll a axis; and some recommendations.
Document ID
20010038272
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Mitchell, David G. (Hoh Aeronautics, Inc. Lomita, CA United States)
Klyde, David H. (NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
August 20, 2013
Publication Date
April 1, 2001
Publication Information
Publication: Pilot-Induced Oscillation Research: The Status at the End of the Century
Volume: 1
Subject Category
Aircraft Stability And Control
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle20010038270Collected WorksPilot-Induced Oscillation Research: The Status at the End of the Century20010038270Collected WorksPilot-Induced Oscillation Research: The Status at the End of the Century
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