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Current limiting remote power control moduleThe power source for the Space Station Freedom will be fully utilized nearly all of the time. As such, any loads on the system will need to operate within expected limits. Should any load draw an inordinate amount of power, the bus voltage for the system may sag and disrupt the operation of other loads. To protect the bus and loads some type of power interface between the bus and each load must be provided. This interface is most crucial when load faults occur. A possible system configuration is presented. The proposed interface is the Current Limiting Remote Power Controller (CL-RPC). Such an interface should provide the following power functions: limit overloading and resulting undervoltage; prevent catastrophic failure and still provide for redundancy management within the load; minimize cable heating; and provide accurate current measurement. A functional block diagram of the power processing stage of a CL-RPC is included. There are four functions that drive the circuit design: rate control of current; current sensing; the variable conductance switch (VCS) technology; and the algorithm used for current limiting. Each function is discussed separately.
Document ID
19910009674
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hopkins, Douglas C.
(Auburn Univ. AL, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1990
Publication Information
Publication: Alabama Univ., Research Reports: 1990 NASA(ASEE Summer Faculty Fellowship Program
Subject Category
Electronics And Electrical Engineering
Accession Number
91N18987
Funding Number(s)
CONTRACT_GRANT: NGT-01-002-099
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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