Integrated robust adaptive tracking control of non-cooperative fly-around mission subject to input saturation and full state constraints

Yi Huang, Yingmin Jia*

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

31 Citations (Scopus)

Abstract

This paper investigates the relative position and attitude tracking control of non-cooperative fly-around mission in the presence of parameter uncertainties, external disturbances, input saturation and full state constraints. Firstly, an integrated and coupled 6 DOF relative motion dynamic model is established, which is consisted of relative position model depicted in the line-of-sight (LOS) frame and relative attitude model described by Modified Rodriguez parameters (MRPs). Subsequently, by using the backstepping control method, an integrated robust adaptive anti-windup control scheme is proposed, in which uncertain parameters and unknown upper bound of the disturbances are estimated by adaptive technique, and the adverse effects caused by input saturation are reduced by the designed anti-windup compensator. To guarantee the full state constraints satisfied all the time, the barrier Lyapunov function method is incorporated into the backstepping control design. Rigorous stability proofs show that the designed robust adaptive controller guarantees that the relative motion states not only can be restricted in the prescribed constraint regions, but also can converge into the small regions with good robustness. Finally, numerical simulation results demonstrate the effectiveness and performance of the designed control scheme.

Original languageEnglish
Pages (from-to)233-245
Number of pages13
JournalAerospace Science and Technology
Volume79
DOIs
Publication statusPublished - Aug 2018
Externally publishedYes

Keywords

  • Adaptive backstepping control
  • Full state constraints
  • Input saturation
  • Integrated robust tracking control
  • Non-cooperative fly-around mission

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