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A high reliability battery management systemOver a period of some 5 years Canadian Astronautics Limited (CAL) has developed a system to autonomously manage, and thus prolong the life of, secondary storage batteries. During the development, the system was aimed at the space vehicle application using nickel cadmium batteries, but is expected to be able to enhance the life and performance of any rechargeable electrochemical couple. The system handles the cells of a battery individually and thus avoids the problems of over, and under, drive that inevitably occur in a battery of cells managed by an averaging system. This individual handling also allow cells to be totally bypassed in the event of failure, thus avoiding the losses associated with low capacity, partial short circuit, and the catastrophe of open circuit. The system has an optional capability of managing redundant batteries simultaneously, adding the advantage of on line reconditioning of one battery, while the other maintains the energy storage capability of the overall system. As developed, the system contains a dedicated, redundant, microprocessor, but the capability exists to have this computing capability time shared, or remote, and operating through a data link. As adjuncts to the basic management system CAL has developed high efficiency, polyphase, power regulators for charge and discharge power conditioning.
Document ID
19870001661
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Moody, M. H.
(Canadian Astronautics Ltd. Ottawa Ontario, Canada)
Date Acquired
August 13, 2013
Publication Date
September 1, 1986
Publication Information
Publication: NASA. Goddard Space Flight Center The 1985 Goddard Space Flight Center Battery Workshop (date)
Subject Category
Electronics And Electrical Engineering
Accession Number
87N11094
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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