摘要
通过分析飞航导弹侧向运动特点,将飞航导弹侧向运动视为多变量控制对象进行了研究.根据导弹飞行特点与性能要求,确定了侧向运动的性能指标,包括跟踪性能指标、稳定性指标和输入扰动抑制指标等.应用定量反馈理论设计了导弹侧向运动的多变量控制器与前置滤波器,并对结果进行了时域仿真与分析.
The lateral movements of aerodynamic missile are considered as multi-variable control systems by means of analyzing the characteristics of the lateral movements of aerodynamic missile. According to the quantitative feedback theory, the specifications of the lateral movements of aerodynamic missile is determined by the characteristics of the missile and the performance requirements. The multi-variable controllers and the pre-fiher are designed. The results are simulated and analyzed in the time domain.
出处
《战术导弹技术》
2009年第4期45-50,共6页
Tactical Missile Technology
关键词
飞航导弹
定量反馈理论
多变量控制
aerodynamic missile
quantitative teedback theory
multi-variable control
