4.7 Article

Global Neural Dynamic Surface Tracking Control of Strict-Feedback Systems With Application to Hypersonic Flight Vehicle

Journal

Publisher

IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TNNLS.2015.2456972

Keywords

Dynamic surface control; global stability; hypersonic flight vehicle; indirect and direct neural control; smooth switching; strict-feedback system

Funding

  1. National Science Foundation of China [61304098, 61134004, 61473120]
  2. Natural Science Basic Research Plan in Shaanxi Province [2014JQ8326, 2015JM6272]
  3. Fundamental Research Funds for the Central Universities [3102015AX001, 2015ZM065]
  4. Beijing Natural Science Basic Research Plan [4142028]

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This paper studies both indirect and direct global neural control of strict-feedback systems in the presence of unknown dynamics, using the dynamic surface control (DSC) technique in a novel manner. A new switching mechanism is designed to combine an adaptive neural controller in the neural approximation domain, together with the robust controller that pulls the transient states back into the neural approximation domain from the outside. In comparison with the conventional control techniques, which could only achieve semiglobally uniformly ultimately bounded stability, the proposed control scheme guarantees all the signals in the closed-loop system are globally uniformly ultimately bounded, such that the conventional constraints on initial conditions of the neural control system can be relaxed. The simulation studies of hypersonic flight vehicle (HFV) are performed to demonstrate the effectiveness of the proposed global neural DSC design.

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