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A real-time, dual processor simulation of the rotor system research aircraftA real-time, man-in-the loop, simulation of the rotor system research aircraft (RSRA) was conducted. The unique feature of this simulation was that two digital computers were used in parallel to solve the equations of the RSRA mathematical model. The design, development, and implementation of the simulation are documented. Program validation was discussed, and examples of data recordings are given. This simulation provided an important research tool for the RSRA project in terms of safe and cost-effective design analysis. In addition, valuable knowledge concerning parallel processing and a powerful simulation hardware and software system was gained.
Document ID
19770009074
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Mackie, D. B.
(NASA Ames Research Center Moffett Field, CA, United States)
Alderete, T. S.
(Computer Sciences Corp. Mountain View, Calif, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1977
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
A-6652
NASA-TN-D-8328
Report Number: A-6652
Report Number: NASA-TN-D-8328
Accession Number
77N16017
Funding Number(s)
PROJECT: RTOP 504-09-42
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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