反舰导弹航向平面控制导引一体化设计  

A New Approach to Integrated Guidance/Autopilot Design for Antiship Missiles

作　　者：于进勇[1] 张友安[1] 顾文锦[1] 

机构地区：[1]海军航空工程学院自动控制系,山东烟台264001

出　　处：《飞行力学》2005年第3期67-69,共3页Flight Dynamics

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,然后基于反演和变结构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,基于某型导弹进行了仿真计算。仿真结果表明,针对高机动的水面目标时的命中精度很高。A new approach to integrated guidance/autopilot design for missiles against maneuvering targets on the sea is considered in this study. The integrated guidance/autopilot model of the yaw plane is formulated firstly. And then based on the backstepping idea and variable structure theory, the guidance/ control law is designed. Finally, to verify the effectiveness and rightness of the integrated design scheme, the simulation of some antiship missile against high maneuvering targets have been made, the simulation results have shown 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 变结构控制 反演 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]