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Flight evaluation of augmented controls for approach and landing of powered-lift aircraftFlight experiments were conducted with Ames Research Center's Quiet Short-Haul Research Aircraft to evaluate the influence of highly augmented control modes on the ability of pilots to execute precision instrument flight operations in the terminal area, particularly approaches to and landings on a short runway. The aircraft is a powered-lift, short-takeoff and landing configuration that is equipped with a modern digital fly-by-wire flight control system, a head-up display, and a solar head-down display that make it possible to investigate control concepts and display format and content for full envelope, powered-lift operations. Considerable attention has been devoted in this flight program to assessing flightpath and airspeed command and stabilization modes developed using nonlinear, inverse model-following methods. The primary benefit of this control concept was realized when the pilot was required to execute a complex transition and approach under instrument conditions and in the presence of a wide range of wind and turbulence conditions.
Document ID
19870030481
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Franklin, J. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Hynes, C. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Hardy, G. H.
(NASA Ames Research Center Moffett Field, CA, United States)
Martin, J. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Innis, R. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1986
Publication Information
Publication: Journal of Guidance, Control, and Dynamics
Volume: 9
ISSN: 0731-5090
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 85-1944
ISSN: 0731-5090
Report Number: AIAA PAPER 85-1944
Accession Number
87A17755
Distribution Limits
Public
Copyright
Other

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