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Collaborative research on V/STOL control system/cockpit display tradeoffs under the NASA/MOD joint aeronautical programSummarized here are activities that have taken place from 1979 to the present in a collaborative program between NASA Ames Research Center and the Royal Aerospace Establishment (now Defence Research Agency), Bedford on flight control system and cockpit display tradeoffs for low-speed and hover operations of future V/STOL aircraft. This program was created as Task 8A of the Joint Aeronautical Program between NASA in the United States and the Ministry of Defence (Procurement Executive) in the United Kingdom. The program was initiated based on a recognition by both parties of the strengths of the efforts of their counterparts and a desire to participate jointly in future simulation and flight experiments. In the ensuing years, teams of NASA and RAE engineers and pilots have participated in each other's simulation experiments to evaluate control and display concepts and define design requirements for research aircraft. Both organizations possess Harrier airframes that have undergone extensive modification to provide in-flight research capabilities in the subject areas. Both NASA and RAE have profited by exchanges of control/display concepts, design criteria, fabrication techniques, software development and validation, installation details, and ground and flight clearance techniques for their respective aircraft. This collaboration has permitted the two organizations to achieve jointly substantially more during the period than if they had worked independently. The two organizations are now entering the phase of flight research for the collaborative program as currently defined.
Document ID
19920023544
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Franklin, J. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Nicholas, O. P.
(Royal Aircraft Establishment Bedford, United Kingdom)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-103910
NAS 1.15:103910
A-92039
Accession Number
92N32788
Funding Number(s)
PROJECT: RTOP 533-02-37
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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