A journal of IEEE and CAA , publishes high-quality papers in English on original theoretical/experimental research and development in all areas of automation
Volume 2 Issue 2
Apr.  2015

IEEE/CAA Journal of Automatica Sinica

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Article Contents
Delong Hou, Qing Wang and Chaoyang Dong, "Output Feedback Dynamic Surface Controller Design for Airbreathing Hypersonic Flight Vehicle," IEEE/CAA J. of Autom. Sinica, vol. 2, no. 2, pp. 186-197, 2015.
Citation: Delong Hou, Qing Wang and Chaoyang Dong, "Output Feedback Dynamic Surface Controller Design for Airbreathing Hypersonic Flight Vehicle," IEEE/CAA J. of Autom. Sinica, vol. 2, no. 2, pp. 186-197, 2015.

Output Feedback Dynamic Surface Controller Design for Airbreathing Hypersonic Flight Vehicle

Funds:

This work was supported by Natural National Science Foundation of China (61273083, 61374012).

  • This paper addresses issues related to nonlinear robust output feedback controller design for a nonlinear model of airbreathing hypersonic vehicle. The control objective is to realize robust tracking of velocity and altitude in the presence of immeasurable states, uncertainties and varying flight conditions. A novel reduced order fuzzy observer is proposed to estimate the immeasurable states. Based on the information of observer and the measured states, a new robust output feedback controller combining dynamic surface theory and fuzzy logic system is proposed for airbreathing hypersonic vehicle. The closedloop system is proved to be semi-globally uniformly ultimately bounded (SUUB), and the tracking error can be made small enough by choosing proper gains of the controller, filter and observer. Simulation results from the full nonlinear vehicle model illustrate the effectiveness and good performance of the proposed control scheme.

     

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