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Implementation of a blade element UH-60 helicopter simulation on a parallel computer architecture in real-timeA high-performance platform for development of real-time helicopter flight simulations based on a simulation development and analysis platform combining a parallel simulation development and analysis environment with a scalable multiprocessor computer system is described. Simulation functional decomposition is covered, including the sequencing and data dependency of simulation modules and simulation functional mapping to multiple processors. The multiprocessor-based implementation of a blade-element simulation of the UH-60 helicopter is presented, and a prototype developed for a TC2000 computer is generalized in order to arrive at a portable multiprocessor software architecture. It is pointed out that the proposed approach coupled with a pilot's station creates a setting in which simulation engineers, computer scientists, and pilots can work together in the design and evaluation of advanced real-time helicopter simulations.
Document ID
19910032090
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Moxon, Bruce C.
(MasPar Computer Corp. Sunnyvale, CA, United States)
Green, John A.
(Advanced Rotorcraft Technology, Inc. Mountain View, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 90-3164
Accession Number
91A16713
Funding Number(s)
CONTRACT_GRANT: NAS2-11960
Distribution Limits
Public
Copyright
Other

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