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A Summery of an In-flight Evaluation of Control System Pure Time Delays During Landing Using the F-8 DFBW AirplaneAn in-flight investigation of the effect of pure time delays on low L/D space shuttle type landing tasks was undertaken. The results indicate that the sensitivity of the pilot ratings to changes in pure time delay in pitch is strongly affected by the task and only slightly affected by changes in control system augmentation mode. Low L/D spot landings from a lateral offset were twice as sensitive to pure time delay as normal low L/D landings. For comparison purposes, formation flying was also investigated, and was found to be less sensitive to time delay than the landing tasks.
Document ID
19800061744
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Berry, D. T.
(NASA Flight Research Center Edwards, CA, United States)
Powers, B. G.
(NASA Flight Research Center Edwards, CA, United States)
Szalai, K. J.
(NASA Flight Research Center Edwards, CA, United States)
Wilson, R. J.
(NASA Flight Research Center Edwards, Calif., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 80-1626
Report Number: AIAA PAPER 80-1626
Meeting Information
Meeting: Atmospheric Flight Mechanics Conference
Location: Danvers, MA
Start Date: August 11, 1980
End Date: August 13, 1980
Accession Number
80A45914
Distribution Limits
Public
Copyright
Other

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