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dc.contributor.authorFisher, Patrick J.
dc.date.accessioned2016-06-22T22:48:48Z
dc.date.available2016-06-22T22:48:48Z
dc.date.issued1980-10
dc.identifier.issn0884-5123
dc.identifier.issn0074-9079
dc.identifier.urihttp://hdl.handle.net/10150/614301
dc.descriptionInternational Telemetering Conference Proceedings / October 14-16, 1980 / Bahia Hotel, San Diego, Californiaen_US
dc.description.abstractThe task of controlling and monitoring a domestic communications satellite from transfer orbit injection, through the critical apogee motor firing sequence and the drift orbit to on-station operations is addressed in this paper. The Satellite Ground Control System (SGCS) employs the latest technology, equipment and computer software architecture to perform the necessary tasks of monitoring and controlling the INSAT spacecraft to be launched in 1981. This paper documents an approach which allows cooperation of the host country technological capabilities with the specialized technology required to place a satellite in orbit. A unique feature of this design is the utilization of a single minicomputer to perform both real time telemetry tracking and command (TT&C) and background orbital analysis functions at the Satellite Control Center.
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.rights.urihttp://rightsstatements.org/vocab/InC/1.0/
dc.titleSatellite Ground Control System for INSATen_US
dc.typetexten
dc.typeProceedingsen
dc.contributor.departmentFord Aerospace & Communication Corporationen
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.dateFOA2018-09-11T13:48:14Z
html.description.abstractThe task of controlling and monitoring a domestic communications satellite from transfer orbit injection, through the critical apogee motor firing sequence and the drift orbit to on-station operations is addressed in this paper. The Satellite Ground Control System (SGCS) employs the latest technology, equipment and computer software architecture to perform the necessary tasks of monitoring and controlling the INSAT spacecraft to be launched in 1981. This paper documents an approach which allows cooperation of the host country technological capabilities with the specialized technology required to place a satellite in orbit. A unique feature of this design is the utilization of a single minicomputer to perform both real time telemetry tracking and command (TT&C) and background orbital analysis functions at the Satellite Control Center.


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