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运载火箭测量系统综合化设计与实现

刘来方

现代电子技术2024,Vol.47Issue(8):171-174,4.
现代电子技术2024,Vol.47Issue(8):171-174,4.DOI:10.16652/j.issn.1004-373x.2024.08.028

运载火箭测量系统综合化设计与实现

Design and implementation of integrated measurement system for launch vehicle

刘来方1

作者信息

  • 1. 中国西南电子技术研究所,四川 成都 610036
  • 折叠

摘要

Abstract

In allusion to the problems of single function,fixed working system,and closed system architecture of traditional measurement systems for launch vehicles,a suitable open system architecture based on integrated modular avionics(IMA)for current applications is proposed based on the constraints of the launch vehicle platform and by analysing the technical characteristics,iterative process,and limitations of the system.The development of the comprehensive RF terminal based on this architecture is completed,achieving a miniaturized,lightweight,low-power,and flexible and scalable comprehensive measurement system.The designed system can meet the overall application requirements and has broad application prospects in the aerospace field.

关键词

运载火箭/测量系统/综合射频终端/综合化架构/电子系统/性能测试

Key words

launch vehicle/measurement system/comprehensive RF terminal/integrated architecture/electronic systems/performance testing

分类

信息技术与安全科学

引用本文复制引用

刘来方..运载火箭测量系统综合化设计与实现[J].现代电子技术,2024,47(8):171-174,4.

现代电子技术

OA北大核心CSTPCD

1004-373X

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