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SDO-Based Command Filtered Adaptive Neural Tracking Control for MIMO Nonlinear Systems With Time-Varying Constraints. | LitMetric

AI Article Synopsis

  • The article presents an adaptive neural tracking control method for complex multi-input multi-output nonlinear systems, focusing on uncertainties and time-varying constraints.
  • It employs neural networks to approximate uncertainties and introduces a saturation disturbance observer (SDO) to reduce estimation errors compared to traditional methods.
  • The method includes three layers of constraints (prescribed performance functions, actual constraints, and virtual constraints) to ensure performance while addressing challenges like the "explosion of complexity" and singularity issues, demonstrated through a numerical simulation for unmanned aerial vehicle flight control.

Article Abstract

In this article, an adaptive neural tracking control based on saturation disturbance observer (SDO) and command filter is studied for multiple-input-multiple-output nonlinear systems with time-varying constraints and system uncertainties. By employing neural networks (NNs), the system uncertainties are approximated. The SDO is proposed to estimate the composited disturbances which consist of NN approximation errors and the external bounded disturbances. Compared with the traditional disturbance observer, the SDO can reduce the estimation error to some extent. The control requirements are achieved based on the multiconstraints which contain three layers: 1) prescribed performance functions (PPFs); 2) actual constraints; and 3) virtual constraints. The errors remain within the prescribed small neighborhood of zero by using the PPFs, the error constraints ensure that the time-varying constraints are never violated even if the PPFs are not available, and the virtual constraints are applied in a new time-varying barrier Lyapunov function (TVBLF) to design virtual controllers and controller to solve the singularity problem of the traditional TVBLF. In addition, the command filter is introduced to solve the problem of "explosion of complexity." Finally, a numerical simulation verifies the effectiveness of the proposed scheme for a flight control of unmanned aerial vehicle.

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Source
http://dx.doi.org/10.1109/TCYB.2023.3325456DOI Listing

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