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Modeling, simulation and control for a cryogenic fluid management facility, preliminary reportThe synthesis of a control system for a cryogenic fluid management facility was studied. The severe demand for reliability as well as instrumentation and control unique to the Space Station environment are prime considerations. Realizing that the effective control system depends heavily on quantitative description of the facility dynamics, a methodology for process identification and parameter estimation is postulated. A block diagram of the associated control system is also produced. Finally, an on-line adaptive control strategy is developed utilizing optimization of the velocity form control parameters (proportional gains, integration and derivative time constants) in appropriate difference equations for direct digital control. Of special concern are the communications, software and hardware supporting interaction between the ground and orbital systems. It is visualized that specialist in the OSI/ISO utilizing the Ada programming language will influence further development, testing and validation of the simplistic models presented here for adaptation to the actual flight environment.
Document ID
19890006986
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Turner, Max A.
(Houston Univ. Clear Lake, TX., United States)
Vanbuskirk, P. D.
(Lockheed Missiles and Space Co. Burbank, CA., United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Publication Information
Publication: NASA, Lyndon B. Johnson Space Center, First International Conference on Ada (R) Programming Language Applications for the NASA Space Station, Volume 2
Subject Category
Computer Programming And Software
Accession Number
89N16357
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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