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The use of an aircraft test stand for VTOL handling qualities studiesThe VTOL flight tests stand for testing control concepts on the X-14B VSS aircraft in hover, is described. This stand permits realistic and safe piloted evaluation and checkout of various control systems and of parameter variations within each system to determine acceptability to the pilot. Pilots can use it as a practical training tool to practice procedures and flying techniques and become familiar with the aircraft characteristics. Some examples of test experience are given. The test stand allows the X14B to maneuver in hover from centered position + or - 9.7 deg in roll and + or - 9.3 deg in pitch, about + or - 6 deg in yaw, and + or - 15 cm in vertical translation. The unique vertical free flight freedom enables study of liftoffs and landings with power conditions duplicated. The response on the stand agrees well with that measured in free hovering flight, and pilot comments confirm this.
Document ID
19740020624
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Pauli, F. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Corliss, L. D.
(Army Air Mobility Res. and Develop. Lab. Moffett Field, Calif., United States)
Selan, S. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Gerdes, R. M.
(NASA Ames Research Center Moffett Field, CA, United States)
Gossett, T. D.
(Army Air Mobility Res. and Develop. Lab. Moffett Field, Calif., United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1974
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TM-X-62218
Report Number: NASA-TM-X-62218
Accession Number
74N28737
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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