Abstract
In this paper, the problem of autopilot design for missile system with mismatched disturbances is considered via a sliding mode control method and finite time disturbance observer. Firstly, a finite time disturbance observer is designed to estimate the mismatched disturbances. Secondly, based on disturbance estimation values and traditional sliding mode surface, a novel sliding mode surface is constructed. Thirdly, a composite continuous anti-disturbance autopilot is developed, which can guarantee system output converge to reference signal. Finally, a simulation result is presented to demonstrate the effectiveness of the proposed scheme.
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Acknowledgements
This work was supported in part by the National Natural Science Foundation of China(Nos. 61203064,61403227).
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Liu, X., Sun, H., Shan, J. (2016). Composite Continuous Anti-disturbance Autopilot Design for Missile System with Mismatched Disturbances. In: Jia, Y., Du, J., Li, H., Zhang, W. (eds) Proceedings of the 2015 Chinese Intelligent Systems Conference. Lecture Notes in Electrical Engineering. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-48386-2_46
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DOI: https://doi.org/10.1007/978-3-662-48386-2_46
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