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An integrated and modular digital modeling approach for the space station electrical power system developmentAn electrical power system for the Space Station was designed, developed and built. This system provides for electrical power generation, conditioning, storage, and distribution. The initial configuration uses photovoltaic power generation. The power system control is based on a hierarchical architecture to support the requirements of automation. In the preliminary design and technology development phase of the program, various modeling techniques and software tools were evaluated for the purpose of meeting the Space Station power system modeling requirements. Rocketdyne and LeRC jointly selected the EASY5 simulation software, developed by Boeing Computer Services, as a system level modeling tool. The application of the selected analytical modeling approach to represent the entire power system is described. Typical results of model predictions are also summarized. The equipment modeled includes solar arrays, dc to ac converters, resonant inverters, battery storage system, alternator, transmission line, switch gear, and system level microprocessor controls. During the advanced development phase of this program, several models were developed using this approach.
Document ID
19880013551
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gombos, Frank J.
(Rockwell International Corp. Canoga Park, Calif., United States)
Dravid, Narayan
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-4155
NAS 1.15:100904
NASA-TM-100904
Report Number: E-4155
Report Number: NAS 1.15:100904
Report Number: NASA-TM-100904
Accession Number
88N22935
Funding Number(s)
PROJECT: RTOP 474-42-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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