DocumentCode
2990561
Title
Design and development of the frequency generation system for the ACeS spacecraft
Author
Dayaratna, L. ; Ramos, L.G. ; Moser, M. ; Buondelmonte, C.
Author_Institution
Lockheed Martin Commun. & Power Center, Newtown, PA, USA
Volume
3
fYear
1999
fDate
13-19 June 1999
Firstpage
1051
Abstract
The ACeS Communication Satellite (Garuda-1), developed by Lockheed Martin CPC and due to be launched in 1999, will be the first mobile communications satellite employing a centralized frequency generation system (FGS) consisting of 420 synthesizers. In order to generate the local oscillator frequencies for the various frequency (up/down) converters, a centralized FGS is employed. Coherent signal processing is achieved by generating all local oscillator signals from a highly stable 10 MHz reference frequency source. The frequency conversion architecture utilizing a dedicated programmable synthesizer for each of the 364 payload converters and the associated FGS is unique to this type of payload. The design requirements of small size, low mass, and low power consumption were met by a unique design concept that is modular and easy to test.
Keywords
frequency convertors; frequency synthesizers; mobile satellite communication; 10 MHz; ACeS spacecraft; Garuda-1; Lockheed Martin CPC; centralized frequency generation system; coherent signal processing; dedicated programmable synthesizer; frequency generation system; local oscillator frequencies; local oscillator signals; mobile communications satellite; payload converters; power consumption; reference frequency source; up/down converters; Artificial satellites; Energy consumption; Frequency conversion; Frequency synthesizers; Local oscillators; Mobile communication; Payloads; Signal generators; Signal processing; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Microwave Symposium Digest, 1999 IEEE MTT-S International
Conference_Location
Anaheim, CA, USA
Print_ISBN
0-7803-5135-5
Type
conf
DOI
10.1109/MWSYM.1999.779568
Filename
779568
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