MIISSILES AND GUIDANCE TECHNOLOGY

Fractional-order PIDμDν Attitude Controller for Hypersonic Missile in Reentry

  • QIN Changmao ,
  • QI Naiming
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  • Aerospace Engineering Department, Harbin Institute of Technology, Harbin 150001, China

Received date: 2009-08-23

  Online published: 2025-05-28

Abstract

For hypersonic missile in complex environment of reentry, the fractional-order PIDμDν (FOC) was applied to attitude control of missile and tunes FOC parameters by the ITAE index combining with its ten-order Tustin+CFE digital implementation. The simulation results show that compared with traditional PID controller, FOC has better control effect and stronger robustness when aerodynamic parameters change.

Cite this article

QIN Changmao , QI Naiming . Fractional-order PIDμDν Attitude Controller for Hypersonic Missile in Reentry[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(4) : 26 -28 . DOI: 10.15892/j.cnki.djzdxb.2010.04.016

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