基于特征结构配置的变稳控制技术研究

Study on Variable Stability Control Technique Based on Eigenstructure Assignment

研究了变稳基本原理及变稳控制律设计方法。基于特征结构配置方法,通过设计飞机的纵向和横航向变稳控制律,使原型机模拟目标机的响应特性,并通过Simulink仿真,验证了变稳控制律的跟踪效果。

Studies on basic principle and design method of control laws for variable stability has been conducted, the prototype simulated the response characteristics of target drome resulted from designed longitudinal and lateral variable stability control laws based on eigenstructure assignment, which passed the Simulink simulation to prove the tracing effect of variable stability control laws.