航空兵器Issue(5)：43-47,5.
固体火箭发动机单向可调喷管转换控制研究
Research on Transition Control of Solid Rocket Motor with Unidirectional-Variable Area Nozzle
摘要
Abstract
This paper studies the transition control of solid rocket motor with unidirectional-variable area nozzle based on theoretical analysis and examination. According to different choice of control points, the paper finishes the design, simulation and test of transition controller, and analyses the advantages of different control modes. The research can provide a reference for solid rocket using unidirectional-variable area nozzle.关键词
固体火箭发动机/可调喉部面积喷管/转换控制Key words
solid rocket motor(SRM)/variable throat area nozzle/transition control分类
航空航天引用本文复制引用
周建军,尹自宾..固体火箭发动机单向可调喷管转换控制研究[J].航空兵器,2012,(5):43-47,5.基金项目
基金项目：装备预研基金 （）
