固体冲压发动机燃气流量伺服控制方法研究  

Study on the method of gas flow servo control in solid rocket ramjet

作　　者：刘源翔[1] 张冬旭[1] 石建国 姚晓先[1] 

机构地区：[1]北京理工大学宇航学院,北京100081 [2]哈尔滨建成集团有限公司,哈尔滨150030

出　　处：《战术导弹控制技术》2012年第1期32-37,45,共7页

摘　　要：为了减小燃气可控的燃气发生器工作工程中产生的逆响应，提出了三种控制方法。建立了燃气发生器的数学模型，根据模型仿真结果，对三种控制方法进行比较与分析。Three methods of control were proposed for reducing negative response when gas generator which can control gas flow was working. Mathematical models of gas generator were built. And the three methods of control were compared according to the result of stimulation.

关 键 词：燃气可控 燃气发生器 仿真实验 

分 类 号：V435[航空宇航科学与技术—航空宇航推进理论与工程]