直接力/气动力复合控制非线性控制律研究  

Nonlinear Control Law for a Missile with Lateral Thrust

作　　者：王建琦[1] 贾晓洪[1] 杨育荣[1] 李海峰[1] 

机构地区：[1]中国空空导弹研究院,河南洛阳471009

出　　处：《弹箭与制导学报》2007年第5期1-3,共3页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：针对直接力/气动力复合控制非线性弹体模型,通过单通道的设计和仿真,进行了非线性控制律的验证。控制律是在反馈线性化(非线性动态逆)的基础上结合模糊控制和神经网络——FCMAC的优点,采取的一种鲁棒自适应方法,对导弹的非线性模型进行了控制器的设计。仿真结果表明了该控制方案的可行性。According to the nonlinear missile model of side jet force and aerodynamic force compound control, design and simulation based on single channel is presented to verify the nonlinear control law. The control law is based on feedback linearization（nonlinear dynamic inversion） and combine with the advantage of fuzzy control and neural network-FCMAC. A robust and self-adaptive method is adopted to design the nonlinear controller. Result of simulation shows the feasibility of this kind of control method.

关 键 词：直接力 复合控制 非线性控制 动态逆 神经网络 

分 类 号：TJ765.2[兵器科学与技术—武器系统与运用工程]