一类飞行器的多变量鲁棒控制
Multivariable Robust Control for a Type of Missiles
-
摘要: 对一类飞行器建立了数学模型并进行了分析,使用非最小相位控制系统的智能设计方 法,设计了飞行器的多变量鲁棒控制系统.基于真实模型的控制系统仿真证实了这一设计方 法的有效性.该设计方法对航空航天控制工程具有参考意义.Abstract: In this paper the mathematical model of a type of missiles has been obtained and analyzed, then a multivariable robust control system of the missile is designed by means of intelligent approach to non-minimum phase control system design. Simulation of the control system based on the genuine model showed the effectiveness of the approach. The described design approach can serve as a means for aeronautical and astronautical control engineering.
计量
- 文章访问数: 2135
- HTML全文浏览量: 109
- PDF下载量: 1033
- 被引次数: 0