反舰导弹航向平面控制导引一体化设计  

Integrated Guidance/Control Design of Yaw Plane for Anti-ship Missile

作　　者：李木易 高志华[2] 

机构地区：[1]海军装备部,北京100841 [2]海军航空工程学院,山东烟台264001

出　　处：《战术导弹技术》2011年第3期77-80,共4页Tactical Missile Technology

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,首先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,仿真结果显示在针对高机动的水面目标时的命中精度很高.A concept of integrated guidance/control design of yaw plane for anti-ship missile against water mobile targets is put forward. An integrated guidance/control model is established for guidance/control law design on the basis of inversion and variable structure theory. Simulation of certain type of missile is made to verify the effectiveness and correctness of the integrated design method. Simulation results show that it features high accuracy in hitting highly maneuvering water targets.

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：TJ013.2[兵器科学与技术—兵器发射理论与技术]