舰空导弹制导控制一体化仿真  

Integrated Simulation of Guidance and Control of Ship-to-Air Missiles

作　　者：黄敏 杨兴宝[1] 付哲泉 邹佳歧 HUANG Min;YANG Xing-bao;FU Zhe-quan;ZOU Jia-qi(Dalian Naval Academy,Dalian Liaoning 116018,China)

机构地区：[1]海军大连舰艇学院,辽宁大连116018

出　　处：《计算机仿真》2023年第10期13-18,共6页Computer Simulation

摘　　要：为精确模拟舰空导弹拦截目标弹道,精确计算导弹制导精度,必需开展舰空导弹制导控制一体化仿真。在分析某垂直发射舰空导弹飞行控制过程的基础上,建立舰空导弹制导控制一体化仿真所必需模型,包括导弹受力模型、六自由度运动方程组、控制系统模型及制导规律模型,根据所建立模型,采用迭代计算方法,按照一定的仿真计算流程,仿真计算了舰空导弹在惯性初制导段和半主动雷达寻的末制导段的弹道。仿真结果表明,所建立的制导控制一体化模型能有效模拟舰空导弹的惯性制导弹道和半主动雷达寻的制导弹道。In order to accurately simulate the trajectory of ship-to-air missiles and accurately calculate the guidance accuracy of ship-to-air missiles,it is necessary to carry out integrated simulation of guidance and control of ship-to-air missiles.Based on the analysis of the flight control process of a vertically launched ship-to-air missile,the necessary models for the integrated simulation of guidance and control of ship-to-air missiles were built,including missile force models,six degrees of freedom motion equations,the control system model and the guidance law model.According to the built models,and using the iterative calculation method,with a certain simulation calculation process,the trajectories of the ship-to-air missile in initial inertial guidance and final guidance of semi-active radar homing were calculated by simulation.The simulation results show that the integrated guidance and control model can effectively simulate inertial guidance trajectory and semi-active radar homing guidance trajectory of ship-to-air missiles.

关 键 词：舰空导弹 制导 控制 一体化仿真 

分 类 号：TJ765.4[兵器科学与技术—武器系统与运用工程]