系统仿真学报 ›› 2015, Vol. 27 ›› Issue (10): 2258-2263.

• 建模与仿真理论及方法 • 上一篇    下一篇

巡飞弹拉平段建模分析及可视化仿真

李增彦, 李小民   

  1. 军械工程学院 无人机工程系,石家庄 050003
  • 收稿日期:2015-06-14 修回日期:2015-07-31 出版日期:2015-10-08 发布日期:2020-08-07
  • 作者简介:李增彦(1987-),男,河北石家庄,博士,研究方向为无人机测控与飞行控制理论及应用;李小民(1968-),男,河北保定,博士,教授,研究方向为无人机测控与飞行控制理论及应用。

Modeling Analysis and Visualization Simulation for Leveled Stage of Loitering Munition

Li Zengyan, Li Xiaomin   

  1. Department of UAV Engineering, Ordnance Engineering College, Shijiazhuang 050003, China
  • Received:2015-06-14 Revised:2015-07-31 Online:2015-10-08 Published:2020-08-07

摘要: 巡飞弹可由多种武器平台发射,受投放平台影响,弹载飞行器展开时初始工作状态具有不确定性。弹载飞行器拉平段有别于任意传统飞行模式,针对该特殊过程,建立了拉平段动力学模型;利用Fluent仿真方法获取可靠气动力参数;搭建Simulink飞行仿真模块并设计了俯冲拉平段控制策略;实现Simulink-FlightGear方法实时飞行状态显示。通过仿真实验,得出拉平段飞行特性,如运动参数收敛较慢、具有一定高度损失等特点,这对多种运载平台弹载飞行器初始状态分析、控制算法研究均有借鉴意义。

关键词: 巡飞弹, 拉平段建模, Simulink-FlightGear, 飞行可视化仿真

Abstract: Loitering munition can be launched by various platforms. However, due to the impact of the delivery platform, the initial launching status of the missile-borne aircraft is uncertain. The leveled stage of missile-borne aircraft is different from other traditional flight modes. For this particular process, the dynamic model in leveled stage was established. Reliable aerodynamic parameters were obtained by Fluent's simulation method. Based on Simulink, the flight simulation module and control strategy in leveled stage were designed. Simulink-FlightGear method was used to display the real-time flight state. Through the simulation, flight characteristics in leveled stage are achieved, such as, motion parameters converging slowly and a certain height loss. This study is significant for a variety of missile-borne aircraft delivery platforms to analyze their initial state and research the control algorithm.

Key words: loitering munition, leveled stage modeling, Simulink-FlightGear, flight visual simulation

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