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Journal of Projectiles, Rockets, Missiles and Guidance >

2011 , Vol. 31 >Issue 3: 6 - 10

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.03.007

MISSILES AND GUIDANCE TECHNOLOGY

Integrated Design of Missile Guidance and Control Based on Sliding-mode Control

  • MIAO Haochun ,
  • MA Qinghua ,
  • CHEN Yun ,
  • CHENG Dong
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  • 1 Department of Automation, Tsinghua University, Beijing 100084, China
    2 No.203 Research Institute of China Ordance Industries, Xi'an 710065, China

Received date: 2010-10-22

  Online published: 2025-05-30

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Abstract

Integrated guidance and control models in pitch and yaw channels were built on a roll stable anti tank missile in this paper. Conventional and integrated methods were used respectively to design the sliding mode guidance (SMG) law and the integrated guidance and control of adaptive sliding mode (SMGC) in the terminal guidance session. The hardware-in-the-loop based on dSPACE was established and the SMG and SMGC laws were simulated. The results indicate that the integrated method is better than the conventional and the guidance performance has been proved effectively.

Key words： sliding mode control; integrated guidance and control; dSPACE; hardware-in-the-loop

Cite this article

MIAO Haochun , MA Qinghua , CHEN Yun , CHENG Dong . Integrated Design of Missile Guidance and Control Based on Sliding-mode Control[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(3) : 6 -10 . DOI: 10.15892/j.cnki.djzdxb.2011.03.007

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