教练机2024,Issue(1) :48-52,68.

一种基于混合余度配置电传飞控系统架构设计与分析

Design and Analysis of the Fly-by-Wire System Architecture Based on Mixed Redundancy Configuration

饶明波 李琼 谢慧慈 余云鹏
教练机2024,Issue(1) :48-52,68.

一种基于混合余度配置电传飞控系统架构设计与分析

Design and Analysis of the Fly-by-Wire System Architecture Based on Mixed Redundancy Configuration

饶明波 1李琼 1谢慧慈 1余云鹏1
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作者信息

  • 1. 航空工业洪都,江西南昌,330024
  • 折叠

摘要

系统余度架构设计是实现系统可靠性及容错性等要求的关键途径,本文通过对电传飞控系统余度模型的研究分析,结合电传飞控系统研制的实际情况,提出了一种基于混合余度配置的电传飞控系统余度架构设计方案,并对该方案进行了可靠性预计分析.

Abstract

Systemic redundancy architecture design is a critical approach to achieve the requirements of sys-temic reliability and tolerance.By means of research and analysis of fly-by-wire flight control system redun-dancy model,and in combination with the actual situation for research and development of fly-by-wire control system,this paper puts forward a kind of design scheme for the redundancy architecture of fly-by-wire con-trol system and carries out predictive reliability analysis on this scheme.

关键词

电传飞控系统/余度/架构/可靠性分析

Key words

Fly-by-wire control system/Redundancy/Architecture/Reliability analysis

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出版年

2024
教练机
中航工业江西洪都航空工业集团有限责任公司

教练机

影响因子:0.048
ISSN:1005-7420
参考文献量4
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