基于Simulink的飞航式火箭助飞鱼雷空中弹道仿真  

Research on air trajectory simulation of the cruising rocket assisted torpedo based on simulink

作　　者：曲延明[1] 周明[2] 林宗祥[1] 

机构地区：[1]海军大连舰艇学院研究生管理大队,辽宁大连116018 [2]海军大连舰艇学院装备自动化系,辽宁大连116018

出　　处：《舰船科学技术》2011年第12期107-111,共5页Ship Science and Technology

摘　　要：为研究飞航式火箭助飞鱼雷空中弹道参数设计问题,首先分析其空中运动过程,根据空中弹道的特点,建立了纵向运动方程组。采用MATLAB/Simulink软件建立了仿真模型,并就发射倾角、雷箭分离条件等对空中弹道的影响进行仿真计算。本文的研究成果对飞航式火箭助飞鱼雷空中弹道设计及作战效能研究有一定的参考价值。To research the issue of designing air trajectory parameter of the cruising rocket assisted torpedo, the paper analyzed its movement process in the air, and constructed the equational group of lengthways movement according to its air trajectory, and set up the simulation model based on MATLAB/Simulink, and calculated the influence aroused by some factors such as firing angle and the separate condition of torpedo and rocket. The conclusion of the paper has a certain extent meaning to the ballistic design and operational effectiveness of cruising rocket assisted torpedo.

关 键 词：飞航式火箭助飞鱼雷 空中弹道 仿真 

分 类 号：TJ761.5[兵器科学与技术—武器系统与运用工程] TJ63