Abstract
This paper presents a robust continuous terminal sliding mode attitude tracking control approach for a near-space hypersonic vehicle(NSHV) in the presence of parameter uncertainties and external disturbances. Firstly, a novel nonsingular terminal sliding surface is developed. Then, a continuous terminal sliding mode control law is proposed, which is chattering-free. Afterward, considering the presence of parameter uncertainties and external disturbances, a high order sliding mode disturbance observer is introduced to estimate the lumped disturbance to improve the control performance. Finally, numerical simulations applied to the NSHV illustrate the effectiveness of the proposed approach.
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© 2013 Springer-Verlag Berlin Heidelberg
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Zhang, R., Sun, C., Zhang, J., Qian, C. (2013). Robust Continuous Terminal Sliding Mode Control Design for a Near-Space Hypersonic Vehicle. In: Sun, C., Fang, F., Zhou, ZH., Yang, W., Liu, ZY. (eds) Intelligence Science and Big Data Engineering. IScIDE 2013. Lecture Notes in Computer Science, vol 8261. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-42057-3_87
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DOI: https://doi.org/10.1007/978-3-642-42057-3_87
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-42056-6
Online ISBN: 978-3-642-42057-3
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