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兵工学报 ›› 2016, Vol. 37 ›› Issue (3): 408-413.doi: 10.3969/j.issn.1000-1093.2016.03.004

• 论文 • 上一篇    下一篇

防空武器模拟动态飞行试验方法

丁天宝, 杨东, 何朝, 王琨   

  1. (西北机电工程研究所, 陕西 咸阳 712099)
  • 收稿日期:2015-04-23 修回日期:2015-04-23 上线日期:2016-05-24
  • 通讯作者: 丁天宝 E-mail:tbding@yeah.net
  • 作者简介:丁天宝(1962—), 男, 研究员
  • 基金资助:
    西北机电工程研究所预先研究项目(2014-01-FJ1335)

New Method of Dynamic Flight Simulation Experiment for Anti-aircraft Weapon

DING Tian-bao, YANG Dong, HE Zhao, WANG Kun   

  1. (Northwest Institute of Mechanical and Electrical Engineering,Xianyang 712099,Shaanxi,China)
  • Received:2015-04-23 Revised:2015-04-23 Online:2016-05-24
  • Contact: DING Tian-bao E-mail:tbding@yeah.net

摘要: 为解决防空武器模拟动态飞行试验问题,提出了防空武器模拟动态飞行试验系统工作原理和方法,建立了模拟动态飞行试验目标真值数学模型、稳定试验摇摆量真值数学模型。通过某典型防空武器系统模拟动态飞行试验验证,证明了模拟动态飞行试验原理和所建立的数学模型的正确性。该方法建立了防空武器动态飞行试验系统的理论基础,模型可用于模拟动态飞行试验数据处理和误差分析。

关键词: 兵器科学与技术, 防空武器, 动态飞行试验, 真值

Abstract: A new principle of dynamic flight simulation experiment for anti-aircraft weapon is presented for the simulation experiment of anti-aircraft weapon in laboratory. A mathematical model of obtaining the tagart truth values and a mathematical model of obtaining the truth values of pitch and roll positions of tracker are established. The dynamic flight simulation experiment principle and the mathematical models are verified through dynamic flight simulation experiment. The principle and the key technologies of simulating dynamic flight experiment are valuable for dynamic flight simulation experiment of anti-aircraft weapons, which will promote the research and development of new anti-aircraft weapons. The proposed method is used to establish the theoretical basis of the dynamic flying experimental system, which can be used for data processing and error analysis.

Key words: ordnance science and technology, anti-aircraft weapon, dynamic flight experiment, truth value

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