Concurrent development of fault management hardware and software in the SSM/PMADSpace Station issues in fault management are discussed. The system background is described with attention given to design guidelines and power hardware. A contractually developed fault management system, FRAMES, is integrated with the energy management functions, the control switchgear, and the scheduling and operations management functions. The constraints that shaped the FRAMES system and its implementation are considered.
Document ID
19890027965
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Freeman, Kenneth A. (Martin Marietta Corp. Denver, CO, United States)
Walsh, Rick (Martin Marietta Corp. Astronautics Group, Denver, CO, United States)
Weeks, David J. (NASA Marshall Space Flight Center Huntsville, AL, United States)