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Design Specification for a Thrust-Vectoring, Actuated-Nose-Strake Flight Control Law for the High-Alpha Research VehicleSpecifications for a flight control law are delineated in sufficient detail to support coding the control law in flight software. This control law was designed for implementation and flight test on the High-Alpha Research Vehicle (HARV), which is an F/A-18 aircraft modified to include an experimental multi-axis thrust-vectoring system and actuated nose strakes for enhanced rolling (ANSER). The control law, known as the HARV ANSER Control Law, was designed to utilize a blend of conventional aerodynamic control effectors, thrust vectoring, and actuated nose strakes to provide increased agility and good handling qualities throughout the HARV flight envelope, including angles of attack up to 70 degrees.
Document ID
19960044512
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Bacon, Barton J.
(NASA Langley Research Center Hampton,VA United States)
Carzoo, Susan W.
(NASA Langley Research Center Hampton,VA United States)
Davidson, John B.
(NASA Langley Research Center Hampton,VA United States)
Hoffler, Keith D.
(NASA Langley Research Center Hampton,VA United States)
Lallman, Frederick J.
(NASA Langley Research Center Hampton,VA United States)
Messina, Michael D.
(NASA Langley Research Center Hampton,VA United States)
Murphy, Patrick C.
(NASA Langley Research Center Hampton,VA United States)
Ostroff, Aaron J.
(NASA Langley Research Center Hampton,VA United States)
Proffitt, Melissa S.
(NASA Langley Research Center Hampton,VA United States)
Yeager, Jessie C.
(NASA Langley Research Center Hampton,VA United States)
Foster, John V.
(NASA Langley Research Center Hampton,VA United States)
Bundick, W. Thomas
(NASA Langley Research Center Hampton,VA United States)
Connelly, Patrick J.
(NASA Dryden Flight Research Center Edwards, CA United States)
Kelly, John W.
(NASA Dryden Flight Research Center Edwards, CA United States)
Pahle, Joseph W.
(NASA Dryden Flight Research Center Edwards, CA United States)
Thomas, Michael
(NASA Dryden Flight Research Center Edwards, CA United States)
Wichman, Keith D.
(NASA Dryden Flight Research Center Edwards, CA United States)
Wilson, R. Joseph
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1996
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-110217
NAS 1.15:110217
Report Number: NASA-TM-110217
Report Number: NAS 1.15:110217
Accession Number
96N32025
Funding Number(s)
PROJECT: RTOP 505-68-30-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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