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基于Matlab Simulink的弹道仿真方法
引用本文:黄成,于鹏,赵锡旺. 基于Matlab Simulink的弹道仿真方法[J]. 海军航空工程学院学报, 2015, 30(2): 169-173
作者姓名:黄成  于鹏  赵锡旺
作者单位:91550部队;海军装备部;92270部队
摘    要:
弹道仿真软件有助于飞航导弹武器飞行试验结果的分析与评定。为此,设计了基于Matlab Simulink的弹道仿真计算方法,建立了六自由度空间弹道数学模型,利用导弹相关的气动数据和控制参数测试了算法,实现了软件,仿真结果证明了该模型的准确性和可信度。

关 键 词:弹道仿真  数学模型  仿真方法

Trajectory Simulation Method Based on Matlab Simulink
HUANG Cheng,YU Peng and ZHAO Xi-wang. Trajectory Simulation Method Based on Matlab Simulink[J]. Journal of Naval Aeronautical Engineering Institute, 2015, 30(2): 169-173
Authors:HUANG Cheng  YU Peng  ZHAO Xi-wang
Affiliation:HUANG Cheng;YU Peng;ZHAO Xi-wang;The 91550th Unit of PLA;Naval Equipment Department;The 92270th Unit of PLA;
Abstract:
The trajectory simulation software can help to analyze and evaluate the flight experimental results of the wingedmissile weapon system. The trajectory simulation method was designed based on Matlab Simulink, the mathematical modelof missile trajectory with six degrees of freedom was established, and the software was programmed and tested using theaerodynamic data and control parameters of the missile. The simulation results is proved the model''s accuracy and reliabil.ity.
Keywords:trajectory simulation   mathematical model   simulation method
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