中文摘要：

为了提高导弹的高精度指标,采用计算机仿真技术建立面对称巡航导弹模型,对于导弹性能的研究具有重要的意义。提出了在无风干扰下面对称巡航导弹飞行的多维泰勒网优化控制方案,首先建立导弹的全通道六自由度仿真模型,采用多维泰勒网优化算法设计控制器,运用单纯形法优化控制器参数。分析比较PID优化控制器、滑模优化控制器和多维泰勒网优化控制器对无风干扰下导弹飞行姿态的控制效果。仿真结果表明,多维泰勒网优化控制器在三者中具有最好的控制效果。

英文摘要：

In this paper,multi-dimensional Taylor network optimal control scheme of the plan symmetrical cruise missile flight without wind disturbance is proposed.Firstly,the simulation model of the missile with full channels and six degrees of freedom is established,multi-dimensional Taylor network optimization （MTN） algorithm is used to design controller,and simplex method is applied to optimize controller＇s parameters.PID optimal controller,sliding mode optimal controller and MTN optimal controller for missile flight attitude control effect without wind disturbance are analyzed and compared in this paper.