飞行器可靠性与性能一体化设计初步研究  

Primary Study of Reliability and Performance Incorporate Design of Aerocraft

作　　者：夏青[1] 钱山[1] 张士峰[1] 蔡洪[1] 

机构地区：[1]国防科学技术大学航天与材料工程学院,长沙410073

出　　处：《弹箭与制导学报》2009年第1期257-259,263,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：飞行器可靠性设计与性能设计的分离制约了飞行器设计水平的提高。文中介绍了一体化设计的概念和发展情况,提出了可靠性与性能一体化设计的技术理论,并对其进行三维空间内的分析,给出了实现的概要方法。The advance of aerocraft design was restricted by the separate of reliability design and performance design. The conception and development of incorporate design were introduced in the paper, the technology theory of reliability and performance incorporate design was studied and analyzed in three-dimension space, and the general methods were also discussed.

关 键 词：可靠性设计 性能设计 一体化设计 多学科设计优化 不确定性设计 

分 类 号：V11[航空宇航科学与技术—人机与环境工程]