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Flight test design for CH-47 parameter identificationThe VTOL Approach and Landing Technology (VALT) program is a significant experimental research program aimed at establishing a data base for rotorcraft operation in a terminal area environment. Work was undertaken to determine helicopter math models suitable for analyzing maneuvers along a VTOL trajectory and to apply these math models to determine the flight test procedures of greatest effectiveness in establishing helicopter dynamic characteristics in this mode of operation. As the principal result of this investigation, a flight test specification is presented for the CH-47 VALT aircraft operating along the specified VTOL trajectory of the VALT program.
Document ID
19790006854
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hall, W. E., Jr.
(Systems Control, Inc. Palo Alto, CA, United States)
Vincent, J.
(Systems Control, Inc. Palo Alto, CA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1978
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-158948
Report Number: NASA-CR-158948
Accession Number
79N15025
Funding Number(s)
CONTRACT_GRANT: NAS1-14010
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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