飞控系统性能与可靠性一体化设计技术

陈云霞; 曾声奎; 晋严尊

飞控系统性能与可靠性一体化设计技术

1.
北京航空航天大学工程系统工程系, 北京 100083
2. 中国空空导弹研究院, 洛阳 471009

详细信息

作者简介:
陈云霞(1977-),女,安徽怀宁人,讲师,chenyunxia@buaa.edu.cn.

中图分类号: TB 114.3; TP 391.9
计量
- 文章访问数: 3709
- HTML全文浏览量: 95
- PDF下载量: 1425
- 被引次数: 0
出版历程
- 收稿日期: 2007-03-05
- 网络出版日期: 2008-02-29

Integrating design of performance and reliability for flight control systems

1.
Dept. of System Engineering of Engineering Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
2. China Airborne Missile Academy, Luoyang 471009, China

摘要

摘要: 通过分析性能与可靠性一体化设计国内外相关研究工作的研究成果与不足,提出了性能与可靠性一体化设计(IDPaR,Integrating Design for Performance and Reliability)的研究思路.从产品发生故障的内、外因角度建立了性能与可靠性一体化设计综合模型,提出了性能可靠度的定义和计算方法.并针对典型飞控系统,给出了各类内外影响因素的具体建模方法,总结提出了性能与可靠性一体化设计算法流程和分析方法.最后以某型导弹为案例,进行性能与可靠性一体化设计技术的应用验证.
- 性能与可靠性 /
- 一体化设计 /
- 建模与仿真 /
- 飞控系统
Abstract: By analyzing and summarizing the achievements and shortages of related research works about integrating design of performance and reliability (IDPaR), the research thought of IDPaR was put forward. From considering the internal and external factors related to product failure, a generic modeling method of comprehensive model for IDPaR was given, and definition of performance-reliability and calculation formulas were presented. According to flight control system, the detailed modeling methods of all kinds of influencing factors were described, and the algorithm flow and analyzing methods of IDPaR were summarized and proposed. Finally, taking X-missile-s flight control system as a typical case, the correctness of the model and algorithm were verified by simulation result.
- performance and reliability /
- integrating design /
- modeling and simulation /
- flight control system

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参考文献(1)

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