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Description of the control system design for the SSF PMAD DC testbedThe Power Management and Distribution (PMAD) DC Testbed Control System for Space Station Freedom was developed using a top down approach based on classical control system and conventional terrestrial power utilities design techniques. The design methodology includes the development of a testbed operating concept. This operating concept describes the operation of the testbed under all possible scenarios. A unique set of operating states was identified and a description of each state, along with state transitions, was generated. Each state is represented by a unique set of attributes and constraints, and its description reflects the degree of system security within which the power system is operating. Using the testbed operating states description, a functional design for the control system was developed. This functional design consists of a functional outline, a text description, and a logical flowchart for all the major control system functions. Described here are the control system design techniques, various control system functions, and the status of the design and implementation.
Document ID
19910020952
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Baez, Anastacio N.
(NASA Lewis Research Center Cleveland, OH, United States)
Kimnach, Greg L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:105202
NASA-TM-105202
E-6505
Report Number: NAS 1.15:105202
Report Number: NASA-TM-105202
Report Number: E-6505
Meeting Information
Meeting: Intersociety Energy Conversion Engineering Conference
Location: Boston, MA
Country: United States
Start Date: August 4, 1991
End Date: August 9, 1991
Sponsors: ACS, AIChE, ANS, ASME, IEEE, AIAA, SAE
Accession Number
91N30266
Funding Number(s)
PROJECT: RTOP 474-42-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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