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离散相似法在空-空导弹数字仿真中的应用

王志刚 李伟 张宁

固体火箭技术Issue(5):600-605,6.
固体火箭技术Issue(5):600-605,6.DOI:10.7673/j.issn.1006-2793.2014.05.003

离散相似法在空-空导弹数字仿真中的应用

Application of discrete similar method to the digital simulation for air-to-air missiles

王志刚 1李伟 2张宁1

作者信息

  • 1. 西北工业大学 航天学院,西安 710072
  • 2. 航天飞行动力学技术重点实验室,西安 710072
  • 折叠

摘要

Abstract

To obtain the real-time calculation of attack area for air-to-air missile, a new method for fast simulation was presen-ted. The six degree of freedom simulation model was simplified effectually. Based on the instantaneous equilibrium assumption, the centroid equations of motion was established. The discrete model was built by using the time discrete similar method. Through com-puter simulation to compare the traditional model, variable step integration model, aerodynamic coefficients fitting model and dis-crete model simulation,results show that the aerodynamic coefficients fitting model provides the fastest but least accurate simulation. Compared to the traditional model,the discrete model can greatly increase the simulation velocity with high precision,which may present a feasible project for rapid resolving of attack area of air-to-air missile.

关键词

空-空导弹/瞬时平衡假设/弹道仿真/离散相似法

Key words

air-to-air missile/instantaneous equilibrium assumption/trajectory simulation/discrete similar method

分类

航空航天

引用本文复制引用

王志刚,李伟,张宁..离散相似法在空-空导弹数字仿真中的应用[J].固体火箭技术,2014,(5):600-605,6.

基金项目

上海航天科技创新基金( SAST201203)。 ( SAST201203)

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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