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

关键词：

D O I：

暂无

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.

引用

页码：345 / 348

页数：4

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