The Research of Flight Reliability Evaluation of Missile

摘要：

In this paper, the evaluation method for the flight reliability of missile has been proposed, for solving the problem that the small sample of missile flight experiment, mainly based on the maximum entropy method and the Bayes rules. We build up a flight reliability block diagram of missile and then discuss how to select the environmental factor during data integrated. The results show the feasibility of the proposed method.

关键词： flight reliability environmental factor Bayes maximum entropy method missile weapon system

作者: Ting-Xue XU Qi DONG Yong-Liang ZHANG Ya-Wen ZHAO

作者单位: Department of Ordnance Science and Technology Naval Aeronautical and Astronautical University Yantai Flight Brigade 2 of Troop 91967 Troop 91967 of PLA Shahe, China

会议类型: 国际会议

会议名称: 2011 International Conference on Quality,Reliability,Risk,Maintenance,and Safety Engineering(2011年质量、可靠性、风险、维修性与安全性国际会议暨第二届维修工程国际学术会议 ICQR2MSE 2011)

会议地点: 西安

会议语种:英文

页码: 829-831

在线出版日期: 2011-06-17（万方平台首次上网日期，不代表论文的发表时间）