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dc.contributor.authorSlivkoff, W. J.
dc.date.accessioned2016-07-07T19:32:08Z
dc.date.available2016-07-07T19:32:08Z
dc.date.issued1985-10
dc.identifier.issn0884-5123
dc.identifier.issn0074-9079
dc.identifier.urihttp://hdl.handle.net/10150/615723
dc.descriptionInternational Telemetering Conference Proceedings / October 28-31, 1985 / Riviera Hotel, Las Vegas, Nevadaen_US
dc.description.abstractSpace-Ground-Link-System (SGLS) is a specific capability of an earth terminal which, in conjunction with a space vehicle (SV) transponder, provides Tracking, Telemetry and Commanding (TT&C) services for space vehicles. This paper describes a multi-purpose, single chassis earth terminal receiver/ processor (R/P) which provides and supports those services. The R/P utilizes digital design techniques and microprocessor executed algorithims that provides a design that is physically small (12 inch high chassis), reliable (MTBF > 4000 hours) and parameters/performance that exceed most present and future TT&C requirements.
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.titleMULTI-PURPOSE SIGNAL CHASSIS SGLS RECEIVER/PROCESSORen_US
dc.typetexten
dc.typeProceedingsen
dc.contributor.departmentStanford Telecommunications, Inc.en
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.dateFOA2018-09-11T14:24:03Z
html.description.abstractSpace-Ground-Link-System (SGLS) is a specific capability of an earth terminal which, in conjunction with a space vehicle (SV) transponder, provides Tracking, Telemetry and Commanding (TT&C) services for space vehicles. This paper describes a multi-purpose, single chassis earth terminal receiver/ processor (R/P) which provides and supports those services. The R/P utilizes digital design techniques and microprocessor executed algorithims that provides a design that is physically small (12 inch high chassis), reliable (MTBF > 4000 hours) and parameters/performance that exceed most present and future TT&C requirements.


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