摘要
基于模糊逻辑 ,建立了评判固体火箭发动机总体设计水平两级指标体系和模糊综合评判方法 ,采用给定满意区间的方法提高了可量化指标隶属度的准确性。算例表明 ,该方法较全面地反映了固体火箭发动机总体设计水平。
Based on fuzzy logic, an index system of two grades and a fuzzy comprehensive assessment method judging the system design level of solid rocket motors is set up. It adopts the method in which satisfaction range is given to raise precision of membership function of measurable indexes. An illustration indicates that this method can reflect the system design level of soild rocket motor well.
出处
《固体火箭技术》
EI
CAS
CSCD
北大核心
2001年第4期16-19,共4页
Journal of Solid Rocket Technology
