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Closing the design loop on HiMAT (highly maneuverable aircraft technology)The design methodology used in the HiMAT program and the wind tunnel development activities are discussed. Selected results from the flight test program are presented and the strengths and weaknesses of testing advanced technology vehicles using the RPV concept is examined. The role of simulation on the development of digital flight control systems and in RPV's in particular is emphasized.
Document ID
19850006527
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Putnam, T. W. (NASA Ames Research Center Moffett Field, CA, United States)
Robinson, M. R. (Rockwell International)
Date Acquired
September 5, 2013
Publication Date
December 1, 1984
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NA-84-1893
NAS 1.15:85923
NASA-TM-85923
Report Number: NA-84-1893
Report Number: NAS 1.15:85923
Report Number: NASA-TM-85923
Meeting Information
Meeting: Congr. of the International Council of the Aeronautical Sciences,
Location: Toulouse
Country: France
Start Date: September 9, 1984
End Date: September 14, 1984
Accession Number
85N14836
Funding Number(s)
PROJECT: RTOP 533-03-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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