一种靶弹机动飞行控制装置的设计  

A Design of Maneuver Flight Control Equipment for Target Missile

作　　者：王刚[1] 刘基睿 付京来[1] WANG Gang;LIU Jirui;FU Jinglai(No.91851 Troops of PLA,Huludao 125001)

机构地区：[1]91851部队,葫芦岛125001

出　　处：《舰船电子工程》2022年第6期199-203,共5页Ship Electronic Engineering

基　　金：装备理论研究课题“靶弹航迹控制与弹道拓展技术研究”资助。

摘　　要：设计了一种能够控制靶弹进行水平机动飞行和垂直机动飞行的控制装置。该靶弹机动飞行控制装置由计算机模块、信号调理模块、壳体和专用电缆构成,该装置安装在某型由退役反舰导弹改装的靶弹上,可以对靶弹航向控制通道和高度控制通道进行控制,使靶弹具备机动飞行能力。最后利用靶弹飞控模型进行仿真,验证了靶弹机动飞行控制装置输出的航向控制信号和高度控制信号可以使靶弹具备机动飞行能力。A control equipment which can control the target missile to maneuver in verticial and horigion driection is designed.The target missile maneuver flight control equipment is composed of computer module,signal conditioning module,case and cable.The equipment is used in a target missile which is modified from a decommissioned anit-ship missile.It can be used to control the course and height control channel of the target missile and enable the target missile to maneuver.In the end,a target missle flight control modle is used for simulation.The simulation conforms that the course and height control signal output by the target missile maneuver flight control equipment enable the target missile to maneuver.

关 键 词：靶弹 机动飞行 控制装置 

分 类 号：TN768[电子电信—电路与系统]