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Pilot evaluation of an advanced hingeless rotor XY-15 simulationA piloted simulation of an advanced hingeless rotor XV-15 tilt-rotor aircraft was carried out. The evaluation was made by a pilot from NASA-Ames who had previous experience flying a simulation of the current gimballed rotor NASA/Army XV-15. It was pointed out that some modifications to the force feel system were needed in order to provide rapid force trimming during rapid maneuvers. Some additional tailoring of the SCAS system was required to achieve good nap-of-the-earth performance. Overall pilot opinion on the hingeless rotor XV-15 tilt rotor was favorable. Brief discussion on the mathematical models and the simulator configuration are presented. The maneuvers and pilot comments are given along with some engineering comments.
Document ID
19780002103
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mcveigh, M. A.
(Boeing Vertol Co. Philadelphia, PA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1977
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AD-A051306
D210-11255-1
NASA-CR-152034
Report Number: AD-A051306
Report Number: D210-11255-1
Report Number: NASA-CR-152034
Accession Number
78N10046
Funding Number(s)
CONTRACT_GRANT: NAS2-8048
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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