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Validation of a real-time engineering simulation of the UH-60A helicopterA real-time simulation of the UH-60A Black Hawk Helicopter based on the Sikorsky Gen Hel mathematical model is compared with flight test data and Sikorsky's nonreal-time computer program. An overview of the mathematical model is given, including a description of updates and expansion of the model by NASA. Also, real-time programming requirements and techniques are explained. The simulation displays very good agreement with flight test data and excellent with the nonreal-time program on which it is based. The large dedication of effort required to develop the real-time program suggests a need for development of generalized techniques for real-time simulation of high-fidelity physical models of rotorcraft.
Document ID
19870008283
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ballin, Mark G.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1987
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-88360
A-86407
NAS 1.15:88360
Accession Number
87N17716
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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