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On‐line RNN compensated second order nonsingular terminal sliding mode control for hypersonic vehicle

Ruimin Zhang (School of Automation, Southeast University, Nanjing, China and School of Mathematics and Statistics, Henan University of Science and Technology, Luoyang, China)
Li Wang (School of Automation, Southeast University, Nanjing, China)
Yingjiang Zhou (School of Automation, Southeast University, Nanjing, China)

International Journal of Intelligent Computing and Cybernetics

ISSN: 1756-378X

Article publication date: 1 June 2012

319

Abstract

Purpose

The purpose of this paper is to design a robust control scheme to achieve robust tracking of velocity and altitude commands for a general hypersonic vehicle (HSV) in the presence of parameter variations and external disturbances.

Design/methodology/approach

The robust control scheme is composed of nonsingular terminal sliding mode control (NTSMC), super twisting control algorithm (STC) and recurrent neural network (RNN). First, by combing a novel NTSMC and STC algorithm, a second order NTSMC approach for HSV is proposed to provide fast, continuous and high precision tracking control. Second to relax the requirements for the bounds of the lumped uncertainties in control design, a RNN disturbance observer is presented to increase the robustness of the control system. The weights of RNN are updated by adaptive laws based on Lyapunov theorem, thus the closed‐loop stability can be guaranteed.

Findings

Simulation results demonstrate that the proposed method is effective, leading to promising performance.

Originality/value

The main contributions of this work are: first, both parameter variations and external disturbances are considered in control design for the longitudinal dynamic model of HSV; and second, the proposed controller can remove chattering and achieve more favorable tracking performances than conventional sliding mode control.

Keywords

Citation

Zhang, R., Wang, L. and Zhou, Y. (2012), "On‐line RNN compensated second order nonsingular terminal sliding mode control for hypersonic vehicle", International Journal of Intelligent Computing and Cybernetics, Vol. 5 No. 2, pp. 186-205. https://doi.org/10.1108/17563781211231534

Publisher

:

Emerald Group Publishing Limited

Copyright © 2012, Emerald Group Publishing Limited

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