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Journal of Projectiles, Rockets, Missiles and Guidance >

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

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

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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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

Cite this article

CHEN Yun , MA Qinghua , WANG Gen , MIAO Haochun , LIU Lin . Study on HIL Missile Control System Design and Simulation Platform Based on dSPACE[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2019 , 39(2) : 64 -68 . DOI: 10.15892/j.cnki.djzdxb.2019.02.016

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