系统仿真学报 ›› 2018, Vol. 30 ›› Issue (12): 4732-4737.doi: 10.16182/j.issn1004731x.joss.201812030

• 仿真应用工程 • 上一篇    下一篇

基于多散射中心模拟的导弹连射半实物仿真方法

刘柏廷1,2, 王晓雷1,2, 王超磊1,2, 陶渝辉1,2, 杨召伟1,2   

  1. 1. 航天系统仿真重点实验室 北京仿真中心,北京 100854;
    2. 北京市复杂产品先进制造系统工程技术研究中心 北京仿真中心, 北京 100854
  • 收稿日期:2018-06-30 修回日期:2018-08-01 出版日期:2018-12-10 发布日期:2019-01-03
  • 作者简介:刘柏廷(1986-),男,辽宁,硕士,工程师,研究方向为制导控制半实物仿真。
  • 基金资助:
    国家重点研发计划(2017YFC0820100)

Method of Missile Salvo Hardware-in-the-loop Simulation Based on Multi Scattering Center Analog Measurement

Liu Baiting1,2, Wang Xiaolei1,2, Wang Chaolei1,2, Tao Yuhui1,2, Yang Zhaowei1,2   

  1. 1. Science and Technology on Special System Simulation Laboratory, Beijing Simulation Center, Beijing 100854, China;
    2. Beijing Complex Product Advanced Manufacturing Engineering Research Center, Beijing Simulation Center, Beijing 100854, China
  • Received:2018-06-30 Revised:2018-08-01 Online:2018-12-10 Published:2019-01-03

摘要: 针对某型导弹制导控制半实物仿真试验对双发连射状态的验证需求,提出一种基于多散射中心模拟的防空导弹连射半实物仿真试验方法,研究了双发连射状态的仿真方法和复杂射频体目标多散射中心仿真的控制方法。通过构建半实物仿真验证系统,进行了半实物仿真验证试验,验证试验结果表明,该方法可实现前发导弹及目标的体目标模拟,导引头可稳定跟踪多散射目标,目标模拟信号输出保持高质量,导引头测角误差平稳收敛,可有效支撑某型导弹制导控制算法的设计与验证。

关键词: 半实物仿真, 连射, 多散射中心, 前发导弹

Abstract: For the verification requirements of the hardware-in-the-loop simulation test of a missile salvo guidance control system, this paper proposes a hardware-in-the-loop simulation test method for anti-aircraft missile based on multi-scattering center simulation to study the simulation method of missile salvo and the control method of multi-scattering center simulation of complex radio frequency target. The hardware-in-the-loop simulation verification test was carried out by constructing a hardware-in-the-loop simulation verification system. The verification test results show that the method can simulate the first missile and the target. The seeker can stably track the multi-scatter target, the target analog signal output maintains high quality, and the seeker angle error is smoothly converged, which can effectively support the design and verification of guidance control algorithm for a certain type of missile.

Key words: hardware-in-the-loop simulation test, missile salvo, multi scattering center, first missile

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