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dc.contributor.authorRedman, Paul C.
dc.date.accessioned2016-05-14T01:52:08Zen
dc.date.available2016-05-14T01:52:08Zen
dc.date.issued1976-09en
dc.identifier.issn0884-5123en
dc.identifier.issn0074-9079en
dc.identifier.urihttp://hdl.handle.net/10150/609384en
dc.descriptionInternational Telemetering Conference Proceedings / September 28-30, 1976 / Hyatt House Hotel, Los Angeles, Californiaen_US
dc.description.abstractThis paper describes the hardware and software requirements for a microprocessor-based onboard computer developmental system. In particular, it describes the use of standardized modules which may be assembled in flight form to permit the microprocessor to become a viable alternative to dedicated hard-wired logic implementation in satellite electronic control applications. In addition, it addresses the problem of using electronic control hardware which is common to a majority of applications, with the uniqueness contained in the software. The processor development system includes the basic characteristics of the onboard processor as well as those of the ground-based software development system. The use of these two components to realize a finished onboard processor system is described, and the efficiency advantages of the developmental system are indicated.
dc.description.sponsorshipInternational Foundation for Telemeteringen
dc.language.isoen_USen
dc.publisherInternational Foundation for Telemeteringen
dc.relation.urlhttp://www.telemetry.org/en
dc.rightsCopyright © International Foundation for Telemeteringen
dc.titleA Microprocessor-Based Computer Developmental System for Satellite Applicationen_US
dc.typetexten
dc.typeProceedingsen
dc.contributor.departmentCOMSAT Laboratoriesen
dc.identifier.journalInternational Telemetering Conference Proceedingsen
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
refterms.dateFOA2018-06-16T05:08:30Z
html.description.abstractThis paper describes the hardware and software requirements for a microprocessor-based onboard computer developmental system. In particular, it describes the use of standardized modules which may be assembled in flight form to permit the microprocessor to become a viable alternative to dedicated hard-wired logic implementation in satellite electronic control applications. In addition, it addresses the problem of using electronic control hardware which is common to a majority of applications, with the uniqueness contained in the software. The processor development system includes the basic characteristics of the onboard processor as well as those of the ground-based software development system. The use of these two components to realize a finished onboard processor system is described, and the efficiency advantages of the developmental system are indicated.


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