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Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 1: 37 - 40

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.01.007

MISSILES AND GUIDANCE TECHNOLOGY

The Missile Control System Design Based on ADRC

  • ZHANG Yi ,
  • MA Qinghua ,
  • CHEN Yun ,
  • YAN Xianjun
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  • No. 203 Research Institute of China Ordnance Industries, Xi'an 710065, China

Received date: 2011-05-07

  Online published: 2025-05-29

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Abstract

The active disturbance rejection controller (ADRC) technology was used to research the new design method and application of missile control system. Based on the traditional design methods and principles, the design methods and application of attitude acceleration and altitude controller with ADRC were proposed, and compared with the traditional methods by six DOF simulations. The results show that the method proposed has high robustness and adaptability, and has good application prospects in missile control system design.

Key words： active disturbance rejection controller; acceleration controller; attitude control; altitude control

Cite this article

ZHANG Yi , MA Qinghua , CHEN Yun , YAN Xianjun . The Missile Control System Design Based on ADRC[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(1) : 37 -40 . DOI: 10.15892/j.cnki.djzdxb.2012.01.007

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