北京航空航天大学学报 ›› 2010, Vol. 36 ›› Issue (12): 1485-1489.

• 论文 • 上一篇    下一篇

基于保障系统三维模型的飞机RMS仿真分析方法

栗金卓1, 王乃超2, 马麟2   

  1. 1. 北京航空航天大学 经济管理学院, 北京 100191;
    2. 北京航空航天大学 可靠性与系统工程学院, 北京 100191
  • 收稿日期:2010-07-19 出版日期:2010-12-30 发布日期:2010-12-30
  • 作者简介:栗金卓(1962-),男,北京人,博士生,tian_jia_zhuang@163.com.

RMS research based on three dimension model of support system with simulation method for military aircraft

Li Jinzhuo1, Wang Naichao2, Ma Lin2   

  1. 1. School of Economics and Management, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
    2. School of Reliability and Systems Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
  • Received:2010-07-19 Online:2010-12-30 Published:2010-12-30

摘要: 利用仿真方法研究军用飞机可靠性维修性保障性(RMS,Reliability, Maintainability and Supportability)设计指标确定问题.介绍了保障系统三维模型的内涵,结合三维模型原理和模块化设计原则建立了飞机RMS仿真分析框架,对框架内各模块功能及内涵给予了介绍.给出了仿真分析总体流程,以及对仿真数据进行后处理获得评价参数的计算方法.运用蒙特卡罗仿真方法对军用飞机的RMS设计指标进行实例分析,获得了满足保障效能要求的RMS设计指标方案集,对研制阶段装备设计指标论证有重要的参考价值.

Abstract: The issue of how to obtain reasonable reliability, maintainability and supportability (RMS) design parameters in the development of military aircraft was researched.The framework of RMS design parameters simulation model was constructed via the three-dimensional model of support system and the rule of modular design principle. The framework contains four modules includinag mission module, function model, operations and maintenance model, support organization module and which are the kernel of the framework. The relationship and the content of data streams between these modular were expatiated. According to the definition of evaluation parameters, the method of how to calculate them using simulation data was given. To verify the feasibility and validity of the simulation framework, the Monte Carlo simulation is used in the trade-off RMS design parameters and a family of design values fulfilling the constraints of support effectiveness requirements is obtained.

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