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Design of a mixer for the thrust-vectoring system on the high-alpha research vehicleOne of the advanced control concepts being investigated on the High-Alpha Research Vehicle (HARV) is multi-axis thrust vectoring using an experimental thrust-vectoring (TV) system consisting of three hydraulically actuated vanes per engine. A mixer is used to translate the pitch-, roll-, and yaw-TV commands into the appropriate TV-vane commands for distribution to the vane actuators. A computer-aided optimization process was developed to perform the inversion of the thrust-vectoring effectiveness data for use by the mixer in performing this command translation. Using this process a new mixer was designed for the HARV and evaluated in simulation and flight. An important element of the Mixer is the priority logic, which determines priority among the pitch-, roll-, and yaw-TV commands.
Document ID
19960041445
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Pahle, Joseph W.
(NASA Dryden Flight Research Center Edwards, CA United States)
Bundick, W. Thomas
(NASA Langley Research Center Hampton, VA United States)
Yeager, Jessie C.
(Lockheed Engineering and Sciences Co. Hampton, VA United States)
Beissner, Fred L., Jr.
(Lockheed Engineering and Sciences Co. Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1996
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-110228
NAS 1.15:110228
Report Number: NASA-TM-110228
Report Number: NAS 1.15:110228
Accession Number
96N31389
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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