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Journal of Projectiles, Rockets, Missiles and Guidance >

2016 , Vol. 36 >Issue 4: 20 - 24,43

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2016.04.006

MISSILES AND GUIDANCE TECHNOLOGY

Tracking-differentiator-based Backstepping Control of Hypersonic Vehicles

  • WANG Xuehou ,
  • WAN Mingjuan ,
  • BU Xiangwei ,
  • WEI Gang
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  • 1 Jiangxi Hongdu Aviation Industry Group Corporation Limited, Nanchang 330033, China
    2 Air and Missile Defense College, Air Force Engineering University, Xi'an 710051, China

Received date: 2015-08-01

  Online published: 2025-05-30

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Abstract

A backstepping controller was exploited for an uncertain hypersonic vehicle model. A tracking differentiator (TD) was employed to reconstruct states of flight-path angle and angle-of-attack in the presence of measurement noise. Then, a velocity controller was devised based on dynamic inversion and an altitude controller was explored using backstepping. Moreover, the TD was applied to handle the problem of "explosion of terms". In order to guarantee the controller's robustness against model parameter perturbation, a new disturbance observer was constructed. Simulation results show that the investigated controller exhibits strong robustness and can provide excellent tracking performance.

Key words： hypersonic vehicles; backstepping control; tracking differentiator (TD); reconstruction; disturbance observer

Cite this article

WANG Xuehou , WAN Mingjuan , BU Xiangwei , WEI Gang . Tracking-differentiator-based Backstepping Control of Hypersonic Vehicles[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2016 , 36(4) : 20 -24,43 . DOI: 10.15892/j.cnki.djzdxb.2016.04.006

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