Integral terminal sliding-mode-based singularity-free finite-time tracking control for entry vehicle with input saturation

Ganghui Shen, Yuanqing Xia*, Bing Cui, Panfeng Huang

*Corresponding author for this work

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Abstract

This paper investigates the finite-time tracking control problem for entry vehicle under input saturation and uncertainty. First, a new integral terminal sliding mode surface is devised, which not only renders fast finite-time convergence, but also presents an explicit estimate of settling time. Subsequently, a singularity-free adaptive integral terminal sliding mode control approach is exploited with application of the designed integral terminal sliding mode surface, anti-windup compensator and adaptive technique, which ensures the superior control performance. By introducing linear and fractional power feedback functions into the adaptation mechanism and anti-windup compensator, the designed controller achieves finite-time convergence of tracking errors and estimation errors, while circumventing the overestimation of control gain. Moreover, the finite-time stability is proved by employing Lyapunov theory and bi-limit homogeneity technique. The results of a Monte Carlo simulation show that the final tracking precision within 3 km of the target is improved about 40% under the developed controller.

Original languageEnglish
Article number108260
JournalAerospace Science and Technology
Volume136
DOIs
Publication statusPublished - May 2023

Keywords

  • Adaptive control
  • Entry vehicle
  • Finite-time control
  • Integral terminal sliding mode
  • Trajectory tracking

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Shen, G., Xia, Y., Cui, B., & Huang, P. (2023). Integral terminal sliding-mode-based singularity-free finite-time tracking control for entry vehicle with input saturation. Aerospace Science and Technology, 136, Article 108260. https://doi.org/10.1016/j.ast.2023.108260