Mission reliability assessment for battle-plane based on flight profile

[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)