Persistent Link:
http://hdl.handle.net/10150/608380
Title:
MULTI FUNCTION RF MODULE
Author:
Kumar, Y. Ashok; Aprem, T. J.; Nadar, M.
Affiliation:
ISRO
Issue Date:
1996-10
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:
Generally, to meet the Telemetry and Tracking functions in space probes, RF packages are realised using dedicated circuit configurations and different building blocks. While this approach is warranted for certain Space missions, for some Space programmes, which are basically Technology demonstrators and where the main emphasis is on higher flexibility with minimal complexity - usage of multifunction RF modules (MFRM), would be highly avantageous. The MFRM, which can be considered as a RF package, has a flexible configuration and is built around Common basic building blocks like broadband MMIC, wide band amplifiers, switches, Dielectric Resonant Oscillators (DRO), Numerically Controlled Oscillators (NCO), etc. It also has a Microcontroller, whose function is to select the required configuration and make necessary interconnections between the building blocks, so as to achieve a specific end function, based on the pre set commands from system designer. The commands can either be preprogrammed or they can be through uplink Telecommand signals from the ground stations. A brief outline of the results of the proto unit of a MFRM which can be configured for different end RF functions, through a microcontroller is presented in the paper. It is expected that in Space missions like LEO programmes, Microsats, Reentry, Microgravity experiments etc, the MFRM approach would offer greater flexibility to the system designer at reduced-cost, complexity and production turn around time.
Keywords:
Multifunction; MFRM; NCO; DRO; Microsat
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.titleMULTI FUNCTION RF MODULEen_US
dc.contributor.authorKumar, Y. Ashoken
dc.contributor.authorAprem, T. J.en
dc.contributor.authorNadar, M.en
dc.contributor.departmentISROen
dc.date.issued1996-10en
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.abstractGenerally, to meet the Telemetry and Tracking functions in space probes, RF packages are realised using dedicated circuit configurations and different building blocks. While this approach is warranted for certain Space missions, for some Space programmes, which are basically Technology demonstrators and where the main emphasis is on higher flexibility with minimal complexity - usage of multifunction RF modules (MFRM), would be highly avantageous. The MFRM, which can be considered as a RF package, has a flexible configuration and is built around Common basic building blocks like broadband MMIC, wide band amplifiers, switches, Dielectric Resonant Oscillators (DRO), Numerically Controlled Oscillators (NCO), etc. It also has a Microcontroller, whose function is to select the required configuration and make necessary interconnections between the building blocks, so as to achieve a specific end function, based on the pre set commands from system designer. The commands can either be preprogrammed or they can be through uplink Telecommand signals from the ground stations. A brief outline of the results of the proto unit of a MFRM which can be configured for different end RF functions, through a microcontroller is presented in the paper. It is expected that in Space missions like LEO programmes, Microsats, Reentry, Microgravity experiments etc, the MFRM approach would offer greater flexibility to the system designer at reduced-cost, complexity and production turn around time.en
dc.subjectMultifunctionen
dc.subjectMFRMen
dc.subjectNCOen
dc.subjectDROen
dc.subjectMicrosaten
dc.description.sponsorshipInternational Foundation for Telemeteringen
dc.identifier.issn0884-5123en
dc.identifier.issn0074-9079en
dc.identifier.urihttp://hdl.handle.net/10150/608380en
dc.identifier.journalInternational Telemetering Conference Proceedingsen
dc.typetexten
dc.typeProceedingsen
dc.relation.urlhttp://www.telemetry.org/en
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