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Configuration management during transition for a powered lift STOL aircraftPresented in this paper are the analytical and moving-base simulation results of a study to improve flight safety and operations of V/STOL type aircraft. One of the more significant and novel aspects of the work accomplished has been the concept and implementation of a configuration management flight control system designed to take the guesswork out of, and improve the operational safety of, transition flight in the region from cruise to STOL.
Document ID
19740055084
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Johnson, W. A.
Craig, S. J. (Systems Technology, Inc. Hawthorne, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
August 1, 1974
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER 74-836
Report Number: AIAA PAPER 74-836
Meeting Information
Meeting: Mechanics and Control of Flight Conference
Location: Anaheim, CA
Start Date: August 5, 1974
End Date: August 9, 1974
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A37834
Funding Number(s)
CONTRACT_GRANT: NAS2-6441
Distribution Limits
Public
Copyright
Other

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