A power system testbed has been assembled to advance the development of large autonomous electrical power systems required for the space station, spacecraft, and aircraft. The power system for this effort was designed to simulate single- or dual-bus autonomous power systems, or autonomous systems that reconfigure from a single bus to a dual bus following a severe fault. The approach taken was to provide a flexible power system design with two computer systems for control and management. One computer operates as the control system and performs basic control functions, data and command processing, charge control, and provides status to the second computer. The second computer contains expert system software for mission planning, load management, fault identification and recovery, and sends load and configuration commands to the control system.
Development of an autonomous power system testbed
Entwicklung einer Pruefanlage fuer Energiesysteme der Raumfahrttechnik
1985
6 Seiten, 6 Bilder, 1 Quelle
Aufsatz (Konferenz)
Englisch
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