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Automating a spacecraft electrical power system using expert systemsSince Skylab, Marshall Space Flight Center (MSFC) has recognized the need for large electrical power systems (EPS's) in upcoming Spacecraft. The operation of the spacecraft depends on the EPS. Therefore, it must be efficient, safe, and reliable. In 1978, as a consequence of having to supply a large number of EPS personnel to monitor and control Skylab, the Electrical power Branch of MSFC began the autonomously managed power system (AMPS) project. This project resulted in the assembly of a 25-kW high-voltage dc test facility and provided the means of getting man out of the loop as much as possible. AMPS includes several embedded controllers which allow a significant level of autonomous operation. More recently, the Electrical Division at MSFC has developed the space station module power management and distribution (SSM/PMAD) breadboard to investigate managing and distributing power in the Space Station Freedom habitation and laboratory modules. Again, the requirement for a high level of autonomy for the efficient operation over the lifetime of the station and for the benefits of enhanced safety has been demonstrated. This paper describes the two breadboards and the hierarchical approach to automation which was developed through these projects.
Document ID
19920002834
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Lollar, L. F.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M-670
NAS 1.60:3161
NASA-TP-3161
Report Number: M-670
Report Number: NAS 1.60:3161
Report Number: NASA-TP-3161
Accession Number
92N12052
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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