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Studies of Pilot-Induced OscillationTotal In-Flight Simulator permits reliable evaluation of landing characteristics of aircraft with PIO. Report discusses simulation requirements for investigating PIO characteristics and includes evaluation of relative merits of simulators. Observations of interest to those studying landing characteristics of other aircraft and to those designing pilot-training programs.
Document ID
19860000382
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Powers, B. G.
Date Acquired
August 12, 2013
Publication Date
July 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 10
Issue: 4
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
ARC-11601
Report Number: ARC-11601
ISSN: 0145-319X
Accession Number
86B10382
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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