It was found that improvement could be obtained if work load of pilot were decreased by providing partial automatic control; one of demands placed on system was its ability to deal with maneuvers and atmospheric disturbances typical for terminal phase of approach near ground; results obtained including analog simulation work and flight testing; system characteristics and recommended piloting techniques were applied to automatic speed control, designed for experimental research aircraft of STOL capability.
Improvements in longitudinal stability and control during landing approach of STOL aircraft
Can Aeronautics Space J
Canadian Aeronautics and Space Journal ; 11 , n 4
1965
11 pages
Article (Journal)
English
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