Persistent Link:
http://hdl.handle.net/10150/615031
Title:
Application for Spacecraft of the 90's Using MicroDACS Technology
Author:
Horn, Paul
Affiliation:
SCI Technology Inc.
Issue Date:
1988-10
Rights:
Copyright © International Foundation for Telemetering
Collection Information:
Proceedings from the International Telemetering Conference are made available by the International Foundation for Telemetering and the University of Arizona Libraries. Visit http://www.telemetry.org/index.php/contact-us if you have questions about items in this collection.
Publisher:
International Foundation for Telemetering
Journal:
International Telemetering Conference Proceedings
Abstract:
Recent developments in electronics have made possible the miniaturization of many of the subsystem components associated with a typical spacecraft data acquisition and control system. This paper describes a low power consumption, fault tolerant, high performance data acquisition and control system design utilizing third generation hardware. The system includes built in test autonomy, redundancy management and fault tolerant communication busses, and supports multiprocessing with up to five 35 Million instructions per second (Mips) processors.
Sponsors:
International Foundation for Telemetering
ISSN:
0884-5123; 0074-9079
Additional Links:
http://www.telemetry.org/

Full metadata record

DC FieldValue Language
dc.language.isoen_USen
dc.titleApplication for Spacecraft of the 90's Using MicroDACS Technologyen_US
dc.contributor.authorHorn, Paulen
dc.contributor.departmentSCI Technology Inc.en
dc.date.issued1988-10-
dc.rightsCopyright © International Foundation for Telemeteringen
dc.description.collectioninformationProceedings from the International Telemetering Conference are made available by the International Foundation for Telemetering and the University of Arizona Libraries. Visit http://www.telemetry.org/index.php/contact-us if you have questions about items in this collection.en
dc.publisherInternational Foundation for Telemeteringen
dc.description.abstractRecent developments in electronics have made possible the miniaturization of many of the subsystem components associated with a typical spacecraft data acquisition and control system. This paper describes a low power consumption, fault tolerant, high performance data acquisition and control system design utilizing third generation hardware. The system includes built in test autonomy, redundancy management and fault tolerant communication busses, and supports multiprocessing with up to five 35 Million instructions per second (Mips) processors.en
dc.description.sponsorshipInternational Foundation for Telemeteringen
dc.identifier.issn0884-5123-
dc.identifier.issn0074-9079-
dc.identifier.urihttp://hdl.handle.net/10150/615031-
dc.identifier.journalInternational Telemetering Conference Proceedingsen
dc.typetexten
dc.typeProceedingsen
dc.relation.urlhttp://www.telemetry.org/en
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