MATEC Web of Conferences (Jan 2018)

A Specific Sliding Mode Control for Autopilot Design of Bank-to-Turn Missiles

  • Huai Zepeng,
  • Wang Hongbo,
  • Gong Min,
  • Ren Pengfei,
  • Xu Zijian,
  • Cheng Lingxiao

DOI
https://doi.org/10.1051/matecconf/201817901015
Journal volume & issue
Vol. 179
p. 01015

Abstract

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This paper studies the BTT missile's sliding mode flight controller. Firstly, the control model is established according to dynamic inverse method and the general dynamic equation of the missile flying in the atmosphere. Then, the sliding mode controller is designed and it adopts the time-varying sliding mode surface, the self-defined reaching law and the adaptive control parameters. Finally, three sets of simulation are carried out to prove the flight controller designed in this paper for BTT missile can follow the guidance instructions and meet operational needs.