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Helicopter simulation validation using flight dataA joint NASA/Army effort to perform a systematic ground-based piloted simulation validation assessment is described. The best available mathematical model for the subject helicopter (UH-60A Black Hawk) was programmed for real-time operation. Flight data were obtained to validate the math model, and to develop models for the pilot control strategy while performing mission-type tasks. The validated math model is to be combined with motion and visual systems to perform ground based simulation. Comparisons of the control strategy obtained in flight with that obtained on the simulator are to be used as the basis for assessing the fidelity of the results obtained in the simulator.
Document ID
19830004842
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Key, D. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Hansen, R. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Cleveland, W. B.
(NASA Ames Research Center Moffett Field, CA, United States)
Abbott, W. Y.
(Army Aviation Engineering Flight Activity)
Date Acquired
September 4, 2013
Publication Date
November 1, 1982
Subject Category
Aircraft Stability And Control
Report/Patent Number
AVRADCOM-TR-82-A-14
NASA-TM-84291
NAS 1.15:84291
A-9063
Report Number: AVRADCOM-TR-82-A-14
Report Number: NASA-TM-84291
Report Number: NAS 1.15:84291
Report Number: A-9063
Accession Number
83N13112
Funding Number(s)
PROJECT: RTOP 992-21-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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