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The role of the research simulator in the systems development of rotorcraftThe potential application of the research simulator to future rotorcraft systems design, development, product improvement evaluations, and safety analysis is examined. Current simulation capabilities for fixed-wing aircraft are reviewed and the requirements of a rotorcraft simulator are defined. The visual system components, vertical motion simulator, cab, and computation system for a research simulator under development are described.
Document ID
19810010575
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Statler, I. C. (NASA Ames Research Center Moffett Field, CA, United States)
Deel, A. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1981
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-81276
USAAVRADCOM-TR-81-A-7
Report Number: NASA-TM-81276
Report Number: USAAVRADCOM-TR-81-A-7
Accession Number
81N19101
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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