Survey of piloting factors in V/STOL aircraft with implications for flight control system designFlight control system design factors involved for pilot workload relief are identified. Major contributors to pilot workload include configuration management and control and aircraft stability and response qualities. A digital fly by wire stability augmentation, configuration management, and configuration control system is suggested for reduction of pilot workload during takeoff, hovering, and approach.
Document ID
19780011168
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ringland, R. F. (Systems Technology, Inc. Hawthorne, CA, United States)
Craig, S. J. (Systems Technology, Inc. Hawthorne, 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