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Simulating a small turboshaft engine in real-time multiprocessor simulator (RTMPS) environmentA Real-Time Multiprocessor Simulator (RTMPS) has been developed at NASA Lewis Research Center. The RTMPS uses parallel microprocessors to achieve computing speeds needed for real-time engine simulation. This report describes the use of the RTMPS system to simulate a small turboshaft engine. The process of programming the engine equations and distributing them over one, two, and four processors is discussed. Steady-state and transient results from the RTMPS simulation are compared with results from a main-frame-based simulation. Processor execution times and the associated execution time savings for the two and four processor cases are presented using actual data obtained from the RTMPS system. Included is a discussion of why the minimum achievable calculation time for the turboshaft engine model was attained using four processors. Finally, future enhancements to the RTMPS system are discussed including the development of a generalized partitioning algorithm to automatically distribute the system equations among the processors in optimum fashion.
Document ID
19860006751
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Milner, E. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Arpasi, D. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-2876
NASA-TM-87216
NAS 1.15:87216
Report Number: E-2876
Report Number: NASA-TM-87216
Report Number: NAS 1.15:87216
Meeting Information
Meeting: SCS Multiconference
Location: San Diego, CA
Country: United States
Start Date: January 23, 1986
End Date: January 25, 1986
Sponsors: Society for Computer Simulation
Accession Number
86N16221
Funding Number(s)
PROJECT: RTOP 505-40-74
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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