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MAX - An advanced parallel computer for space applicationsMAX is a fault-tolerant multicomputer hardware and software architecture designed to meet the needs of NASA spacecraft systems. It consists of conventional computing modules (computers) connected via a dual network topology. One network is used to transfer data among the computers and between computers and I/O devices. This network's topology is arbitrary. The second network operates as a broadcast medium for operating system synchronization messages and supports the operating system's Byzantine resilience. A fully distributed operating system supports multitasking in an asynchronous event and data driven environment. A large grain dataflow paradigm is used to coordinate the multitasking and provide easy control of concurrency. It is the basis of the system's fault tolerance and allows both static and dynamical location of tasks. Redundant execution of tasks with software voting of results may be specified for critical tasks. The dataflow paradigm also supports simplified software design, test and maintenance. A unique feature is a method for reliably patching code in an executing dataflow application.
Document ID
19930035063
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lewis, Blair F.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bunker, Robert L.
(JPL Pasadena, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: AIAA(NASA International Symposium on Space Information Systems, 2nd, Pasadena, CA, Sept. 17-19, 1990, Proceedings. Vol. 2 (A93-19048 05-82)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Computer Systems
Accession Number
93A19060
Distribution Limits
Public
Copyright
Other

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