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A review of helicopter control-display requirements for decelarating instrument approachThis paper reviews research and operational test programs that have dealt with control and display requirements for helicopters performing decelerating approaches in the terminal area under instrument flight conditions. A survey of literature concentrating on flight programs resulted in approximately 50 applicable references which were summarized and classified according to the type of stability/control augmentation that was emphasized. On this basis, display information requirements for each control system type were hypothesized consistent with documented results of these programs. Nine control-display combinations that appear to warrant further ground simulation and flight testing are defined and discussed.
Document ID
19790061332
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Lebacqz, J. V.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 79-1683
Meeting Information
Meeting: Atmospheric Flight Mechanics Conference for Future Space Systems
Location: Boulder, CO
Start Date: August 6, 1979
End Date: August 8, 1979
Accession Number
79A45345
Distribution Limits
Public
Copyright
Other

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