轻型反坦克导弹复合制导模式设计与仿真分析  

Design and Simulation Analysis of Composite Guidance Mode for Light Anti-tank Missile

作　　者：杨芳 YANG Fang(Xi’an Aeronautical University,Xi’an 710077,China)

机构地区：[1]西安航空学院,西安710077

出　　处：《火力与指挥控制》2020年第6期165-169,共5页Fire Control & Command Control

摘　　要：对某型捷联惯性中制导+红外图像末制导的多用途轻型反坦克导弹的制导控制系统进行了研究,建立了制导控制方程、虚拟比例导引方程以及复合制导的交班过程方程等。结合某反坦克导弹总体参数,建立了弹体运动学模型、制导控制系统等仿真模型,并基于Matlab/Simulink和半实物仿真技术对其进行了仿真试验。试验结果表明,利用捷联惯性中制导+红外末制导复合制导的方法,可以有效提高导弹的制导精度及导弹在复杂战场上的生存能力。The guidance control system of a multi-purpose light anti-tank missile based on strapdown inertial midcourse guidance and infrared image terminal guidance is studied.The guidance control equation,virtual proportional guidance equation and shift equation are established.Combined with the overall parameters of an anti-tank missile,the kinematics model,guidance control system and other simulation models are established,and the simulation tests are carried out based on Matlab/Simulink and semi-physical simulation technology.The test results show that the strapdown inertial midcourse guidance and infrared terminal guidance combined guidance method can effectively improve the guidance accuracy of the missile,and improve the missile's survivability in the complex battlefield.

关 键 词：惯性中制导 红外末制导 复合制导 弹道 半实物仿真 

分 类 号：TJ765.3[兵器科学与技术—武器系统与运用工程]