Abstract
For the hypersonic vehicle with external disturbance, input saturation, model parameter uncertainties and prescribed performance constraint, the tracking control strategy is studied in the thesis. Firstly, a prescribed performance function is introduced into the control design by transforming auxiliary variable errors, which guarantees tracking performance of the control system. On the basis of second-order system model of hypersonic vehicle, an adaptive anti-saturation terminal sliding mode (TSM) controller with prescribed performance is presented by using the adaptive control theory and TSM control. The stability theory of the control law is presented by Lyapunov stability theory and the numerical simulations are conducted to indicate the effectiveness of the proposed control scheme.
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Publisher’s Note Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Recommended by Associate Editor Jiuxiang Dong under the direction of Editor Guang-Hong Yan. This work was supported by the National Natural Science Foundation of China under Grant 61703126, the Research projects of Shenzhen Institute of Information Technology under Grant ZY201714.
Bao-Wen Chen received his Ph.D. degree in Control Theory and Application from Harbin Institute of Technology in 2009. He is currently an associate professor of Computer Science and Technology at Shenzhen Institute of Information Technology. His main research interests include spacecraft guidance and control, intelligent control, and artificial intelligence.
Li-Guo Tan received his Ph.D. degree in Aircraft Navigation and Control from Bauman Moscow State Technical University in 2016. He is currently an assistant researcher of Research Center of Basic Space Science at HarbinInstitute of Technology. His main research interests include UAV control, navigation and guidance, path planning, and multi-sensor information fusion.
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Chen, BW., Tan, LG. Adaptive Anti-saturation Tracking Control with Prescribed Performance for Hypersonic Vehicle. Int. J. Control Autom. Syst. 18, 394–404 (2020). https://doi.org/10.1007/s12555-019-0007-7
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DOI: https://doi.org/10.1007/s12555-019-0007-7