可变冗余架构四余度飞管计算机技术研究

陈茜; 高扬; 曲翕; 吴铭; 樊光焘

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可变冗余架构四余度飞管计算机技术研究

计算机工程与应用 | 更新时间：2026-09-04

- 可变冗余架构四余度飞管计算机技术研究
- Research on four redundancy flight control computer with variable redundancy architecture
- 微电子学与计算机 2021年38卷第9期页码：67-73
- 作者机构：
  
  西安微电子技术研究所,陕西,西安,710054
- 作者简介：
- 基金信息：
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- 纸质出版：2021
- 稿件说明：
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陈茜, 高扬, 曲翕, 吴铭, 樊光焘. 可变冗余架构四余度飞管计算机技术研究[J]. 微电子学与计算机, 2021, 38(9): 67-73.

CHEN Xi, GAO Yang, QU Xi, et al. Research on four redundancy flight control computer with variable redundancy architecture[J]. 2021, 38(9): 67-73.
陈茜, 高扬, 曲翕, 吴铭, 樊光焘. 可变冗余架构四余度飞管计算机技术研究[J]. 微电子学与计算机, 2021, 38(9): 67-73. DOI：

CHEN Xi, GAO Yang, QU Xi, et al. Research on four redundancy flight control computer with variable redundancy architecture[J]. 2021, 38(9): 67-73. DOI：

摘要

飞管计算机作为空天飞机关键电子产品，全程参与飞行器的飞行控制.针对其强实时性、高可靠性、抗辐照、长寿命的特点，提出了一种结合自检测(BIT)技术、当班表决技术的可变冗余架构四余度计算机技术，可以通过故障检测、自恢复、当班权控制、多模表决等技术实现不同的冗余架构管理.结合工程实践，从飞管计算机的系统架构出发，分析了两种四余度架构模式；通过自检测技术快速进行故障检测和定位，进而利用当班表决实现四余度的升降级管理与重构.通过建立可靠性模型进行分析，四模并联模式5年(约4.5万小时)的可靠度高达0.995.该技术已成功应用于某天地往返飞行器.

Abstract

As a key electronic product of space aircraft

flight control computer participates in the flight control of aircraft throughout the process

which has the characteristics of strong real-time performance

high reliability

radiation resistance and long life. A variable redundancy architecture four-redundancy computer technology is proposed

which combines the self-detection (BIT) technology and on-duty voting technology. It can realize different redundancy architecture management through fault detection

self-recovery

on-duty control

multi-mode voting and other technologies. Combined with the engineering practice

two four-redundancy architecture modes are analyzed from the system architecture of the flight control computer. Through the self-detection technology

the fault detection and location can be carried out quickly

and then the promotion and degradation management and reconstruction of the four-redundancy can be realized by the on-duty voting

and the reliability model can be established for the analysis. The reliability of four-mode parallel mode in 5 years (about 45

000 hours) is as high as 0.995. The technology has been successfully applied to a space shuttle.

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references

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