基于MATLAB/Simulink的直升机载导弹制导控制系统建模与仿真  

Modeling and Simulation of Missile Guidance System for Helicopter Based on MATLAB/Simulink

作　　者：吴彤薇[1] 吴震[1] 

机构地区：[1]中国空空导弹研究院,河南洛阳471009

出　　处：《航空兵器》2010年第5期23-26,38,共5页Aero Weaponry

摘　　要：文中建立了直升机载导弹的六自由度制导控制系统的数学模型,编制了以MAT-LAB/Simulink语言为基础的仿真软件。仿真结果表明,与实际飞行试验数据达到很好的拟合,说明采用六自由度制导控制系统的数学模型进行设计的正确性。This paper establishes the mathematics model of six-degree-freedom guidance control system model of missile for helicopter. Then it writes the simulation software using the modularization design method based on MATLAB/Simulink language. The simulation results show that it is close to the actual flight test results,this design which approaches using a six-degree-freedom missile for helicopter model is accurate.

关 键 词：直升机载导弹 建模 MATLAB/SIMULINK 仿真 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]