垂直发射型舰空导弹比例导引三维弹道仿真研究  

Research on 3-Dimensional Trajectory Simulation of Proportional Guidance Ship-to-air Missile

作　　者：马其东[1] 马雷挺[1] 钟志通[1] 

机构地区：[1]海军大连舰艇学院,大连116018

出　　处：《导弹与航天运载技术》2008年第3期15-18,共4页Missiles and Space Vehicles

摘　　要：在对垂直发射型舰空导弹典型飞行弹道进行分析的基础上,将导弹运动学弹道分成无控段、转弯段和制导段,根据导弹弹道特征和制导特性,分别建立和推导了各段弹道的仿真模型。利用MATLAB语言的图形界面集成开发环境GUIDE创建了三维弹道仿真验证和演示软件,以检验弹道仿真模型的正确性和适用性。Based on the characteristics of trajectory of the vertical-launched missile kinematics and the characteristics of proportional guidance, respectively establishing and deducting the trajectory simulating model of non control phase, turn phase and guidance phase of the vertical launched ship-to-air missile. Taking use of graphic interface of MATLAB language and integrated developing environment GUIDE to carry out 3-dimensional trajectory simulation test and program performance, so as to verify the correctness and applicability of the trajectory simulation model.

关 键 词：弹道仿真 舰空导弹 比例导引法 MATLAB 

分 类 号：V448.153[航空宇航科学与技术—飞行器设计]