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Pilot centered requirements in control/display designA method developed for predicting pilot opinion ratings for particular vehicles and tasks using optimal control pilot model is described and an outline of a flight director design procedure based upon the optimal control pilot model is given. Longitudinal and lateral control of a helicopter in hover and in a -6 deg constant ground speed-command landing approach are considered. Emphasis is placed on display design for optimum V/STOL control.
Document ID
19780011167
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hess, R. A. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 9, 2013
Publication Date
August 1, 1977
Publication Information
Publication: Naval Postgraduate School Proc. of the Navy(NASA VSTOL Flying Qualities
Subject Category
Aircraft Design, Testing And Performance
Accession Number
78N19110
Distribution Limits
Public
Copyright
Public Use Permitted.

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