基于NBF网络的导弹航向平面滑模控制导引一体化  

Sliding mode control based on NBF net to integrated guidance/autopilot design for missiles

作　　者：顾文锦[1] 张汝川[1] 于进勇[1] 

机构地区：[1]海军航空工程学院控制工程系,山东烟台,264001 海军航空工程学院控制工程系,山东烟台,264001 海军航空工程学院控制工程系,山东烟台,264001

出　　处：《海军航空工程学院学报》2006年第5期510-512,516,共4页Journal of Naval Aeronautical and Astronautical University

基　　金：总装备部预研项目(2002装计字第1468号)

摘　　要：提出了一种反舰导弹针对水面机动目标的航向平面控制导引一体化设计方案.建立了航向平面的一体化控制导引模型,然后基于NBF网络切换增益调节和滑模控制的思想进行了控制导引律的设计,为了验证该一体化设计的有效性和正确性,进行了仿真计算.仿真结果表明,针对高机动的水面目标命中精度很高.A new approach to integrated guidance/autopilot design for missiles against maneuvering targets on the sea is considered in this paper. The integrated guidance/autopilot model of the yaw plane is formulated firstly. And then based on the sliding mode control theory and radial basis function net, the guidance/control law is designed. Finally, to verify the effectiveness and rightness of the integrated design scheme, the simulation of some anti-ship missile against high maneuvering targets are made, the simulation results show the high accuracy of hitting targets has been got.

关 键 词：控制导引一体化 机动目标 航向平面 NBF网络 滑模控制 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]