摘要
采用劳斯稳定判别法,结合某旋转弹的实际控制结构和弹体特性,对不同控制结构对静稳定度适应程度进行了分析,重点研究了不同的控制系统回路结构对弹体稳定特性的适应能力,为旋转弹控制系统设计提供更有针对性的参考。
By combining the actual control structure and missile characteristics, Routh criterion was used to analyze the relationship between the control loop structure of control system and the static stability of rolling airframe missile. Different control loop structures have different adaptabilities for static stability or static instability, which is of great significance for control system design of rolling airframe missile
出处
《现代防御技术》
北大核心
2014年第5期55-59,共5页
Modern Defence Technology
关键词
旋转弹
稳定性
静不稳定
劳斯判据
rolling airframe missile
static stability
static instability
Routh criterion
