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固体火箭发动机性能可靠性评估的Bayes方法
引用本文:张士峰,蔡洪.固体火箭发动机性能可靠性评估的Bayes方法[J].固体火箭技术,2003,26(4):9-11.
作者姓名:张士峰  蔡洪
作者单位:国防科技大学航天与材料工程学院,长沙,410073
摘    要:在研制阶段试验信息以及积累以往试验信息的基础上,运用Bayes方法,建立了固体火箭发动机性能可靠性仿真模型,给出了仿真模型可信性检验的最大熵谱方法;将仿真信息作为验前信息,结合现场试验信息确定了性能可靠性的近似分布,并给出了性能可靠性的点估计和置信下限估计。

关 键 词:固体火箭发动机  可靠性评估  Bayes方法  仿真模型  性能可靠性  最大熵谱估计
文章编号:1006-2793(2003)04-0009-03

Bayesian approach of performance reliability assessment of solid rocket motors
ZHANG Shi-feng,CAI Hong//College of Aerospace and Material Engineering,National Univ. of Defense Technology,Changsha,China..Bayesian approach of performance reliability assessment of solid rocket motors[J].Journal of Solid Rocket Technology,2003,26(4):9-11.
Authors:ZHANG Shi-feng  CAI Hong//College of Aerospace and Material Engineering  National Univ of Defense Technology  Changsha  China
Institution:ZHANG Shi-feng,CAI Hong//College of Aerospace and Material Engineering,National Univ. of Defense Technology,Changsha410073,China.
Abstract:By using Bayesian method and based on the accumulated test data,the performance reliability simulation models of solid rocket motors are established. The simulation credibility test with maximum entropy spectrum method is presented .The approximate distribution of performance reliability is determined in accordance with simulated pretest data and in-situ test data. Finally, the paper gives an example to show Bayesian approach's validity.
Keywords:solid propellant rocket motor  performance reliability assessment  maximum entropy spectrum estimation  Bayesian approach
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