DESIGN OF A MEASUREMENT BUS FOR PAYLOAD TELEMETRY AND COMMAND DATA HANDLING

被引：0
|
作者：
Zigiotto, Anderson [1 ]
Wittkamp, Markus [2 ]
机构：
[1] Inst Aeronaut & Espaco, Praca Mal Eduardo Gomes 50, BR-12228904 Sao Jose Dos Campos, SP, Brazil
[2] German Aerosp Ctr, Mobile Rocket Base, D-8234 Wessling, Germany
来源：
PROCEEDINGS OF THE 19TH ESA SYMPOSIUM ON EUROPEAN ROCKET AND BALLOON PROGRAMMES AND RELATED RESEARCH | 2009年 / 671卷
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D O I：
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中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The use of modularized architectures for telemetry, telecommand and control is an appropriate solution for flexible payload systems design. Specialized modules must be connected to each other or to a main computer through a bus that meets system requirements such as speed, flexibility and reliability. This paper describes the specification and design of a simple, deterministic, high data rate bus for handling payload telemetry, telecommand and control data. This Measurement Bus is specified to run at up to 40 Mb/s.
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页码：345 / 348
页数：4
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