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弹箭与制导学报 >

2019 , Vol. 39 >Issue 2: 64 - 68

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2019.02.016

基于 dSPACE 的“硬件在回路”导弹控制系统设计与仿真

  • 陈韵 ,
  • 马清华 ,
  • 王根 ,
  • 苗昊春 ,
  • 刘琳
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  • 1 西北工业大学航天学院, 西安 710072
    2 西安现代控制技术研究所, 西安 710065

陈韵(1981-),女,浙江江山人,高级工程师,博士研究生,研究方向:导弹制导与控制。

收稿日期: 2018-04-04

  网络出版日期: 2025-05-20

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Study on HIL Missile Control System Design and Simulation Platform Based on dSPACE

  • CHEN Yun ,
  • MA Qinghua ,
  • WANG Gen ,
  • MIAO Haochun ,
  • LIU Lin
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  • 1 School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China
    2 Xi'an Modern Control Technology Research Institute, Xi'an 710065, China

Received date: 2018-04-04

  Online published: 2025-05-20

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摘要

基于dSPACE实时仿真系统提供的强大运算能力及各种成熟的硬件接口电路,文中研究了导弹控制系统的“硬件在回路”设计与仿真方法。给出系统架构及设计流程,介绍了执行机构舵机测试及模型辨识方法,将舵机实物引入导弹控制回路的设计过程中,实现了从传统的数字离线仿真过程到“硬件在回路”的设计与仿真,克服了传统纯数字模型不能真实代表制导部件性能的缺点,提高了导弹控制系统设计的工作效率及可靠性。

关键词： dSPACE; 硬件在回路; 模型辨识; 导弹六自由度仿真

本文引用格式

陈韵 , 马清华 , 王根 , 苗昊春 , 刘琳 . 基于 dSPACE 的“硬件在回路”导弹控制系统设计与仿真[J]. 弹箭与制导学报, 2019 , 39(2) : 64 -68 . DOI: 10.15892/j.cnki.djzdxb.2019.02.016

Abstract

In this paper hardware-in-the-loop(HIL) missile control system simulation platform based on dSPACE is provided. dSPACE has the key benefits of powerful operational capability and convenient hardware interface. The system structure design and development steps were analyzed. The actuator is the real physical part in the platform and the model of the actuator is identified. This platform realized the HIL design and simulation, and the simulation process is similar to the real environment. Experimental results showed that the dSPACE based real-time simulation system is an excellent platform for missile control system design which enhanced the efficiency and reliability.

Key words： dSPACE; hardware-in-the-loop (HIL) simulation; model identification; missile six-degree-of-freedom simulation

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参考文献

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刘小明, 周浩, 陈万春,等. 基于Simulink/RT-LAB的导弹制导系统 HIL仿真平台设计[J]. 红外与激光工程, 2007, 36 (增刊): 366- 369.
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