Mission reliability assessment for battle-plane based on flight profile
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摘要: 针对作战飞机故障数据的特点,分析了作战飞机不同飞行剖面对其任务可靠性的影响.在此基础上,定义了飞行剖面折合系数、建立了作战飞机任务可靠性模型.基于该模型给出了作战飞机在不同飞行剖面下的任务可靠性评估方法.针对想定任务剖面,采用剖面合成的方法把其处理为典型飞行剖面的线性组合,并由此给出了作战飞机在想定剖面下任务可靠性的预测方法.实例表明基于飞行剖面的作战飞机任务可靠性评估方法合理可行,便于工程应用.Abstract: The mission reliability of battle-plane varied under different flight profiles. According to the characteristics of battle-plane's fault data, the flight profile conversion factor was introduced to establish the mission reliability model of battle-plane. Based on the model, the statistical inference method of failure rate for battle-plane was proposed, and the mission reliability was assessed under a given flight profile. For a scenario flight profile, a synthetic method was used to describe it as a weighted combination of typical profiles. Thus, the prediction method of mission reliability under the scenario flight profile was put forward by using the failure rates under typical profiles. The illustrative example shows that the method is reasonable and straightforward for engineering.
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Key words:
- battle-plane /
- flight profile /
- reliability assessment /
- environment conversion factor
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[1] 《飞机设计手册》总编委会.飞机设计手册第20册:可靠性、维修性设计[M].北京:航空工业出版社,1999:414-418 The general editorial board of the aircraft design manual．Aircraft design manual part 20:reliability and maintainability design[M]．Beijing:Aviation Industry Press,1999:414-418(in Chinese) [2] Sohn S Y,Yoon K B,Chang I S.Random effects model for the reliability management of modules of a fighter aircraft[J].Reliability Engineering & System Safety,2006,91(4):433-437 [3] MIL-STD-810F Test method standard for environmental engineering considerations and laboratory tests[S] [4] 《飞机设计手册》总编委会.飞机设计手册第4册:军用飞机总体设计[M].北京:航空工业出版社,2005:18-22 The general editorial board of the aircraft design manual．Aircraft design manual part 4:military aircraft design[M]．Beijing:Aviation Industry Press,2005:18-22(in Chinese) [5] Shi Q,Tian J,Man Q.Damage effect analysis and experiment for electronic equipment in impact vibration environment[J].Journal of Systems Engineering and Electronics,2009,20(6):1384-1388 [6] Elsayed E A,Wang H Z.Bayes & classical estimation of environmental factors for the binomial distribution[J].IEEE Transactions on Reliability,1996,45(4):661-665 [7] 洪东跑,马小兵,赵宇,等.基于比例风险模型的环境折合系数确定方法[J].北京航空航天大学学报,2010,36(4):443-446 Hong Dongpao,Ma Xiaobing,Zhao Yu,et al.Environment referring factor based on proportional hazards model[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(4):443-446(in Chinese) [8] 刘文珽.结构可靠性设计手册[M].北京:国防工业出版社,2008:493-501 Liu Wenting.Design handbook for structural reliability[M].Beijing:National Defense Industry Press,2008:493-501(in Chinese) -
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