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Flight evaluation of highly augmented controls and electronic displays for precision approach and landing of powered-lift aircraftExperiments were conducted on simulators and on the Quiet Short-Haul Research Aircraft to evaluate the effect of highly augmented control modes and electronic displays on the ability of pilots to execute precision approaches and landings on a short runway. It is found that the primary benefits of highly augmented flightpath and airspeed controls and electronic displays are realized when the pilot is required to execute precisely a complex transition and approach under instrument conditions and in the presence of a wide range of wind and turbulence conditions. A flightpath and airspeed command and stabilization system incorporating nonlinear, inverse system concepts produced fully satisfactory flightpath control throughout the aircraft's terminal operating envelope.
Document ID
19850063783
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
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)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 85-1944
Meeting Information
Meeting: Guidance, Navigation and Control Conference
Location: Snowmass, CO
Start Date: August 19, 1985
End Date: August 21, 1985
Accession Number
85A45934
Distribution Limits
Public
Copyright
Other

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