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Dynamic Surface Control of Hypersonic Aircraft with Parameter Estimation

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Foundations and Applications of Intelligent Systems

Part of the book series: Advances in Intelligent Systems and Computing ((AISC,volume 213))

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Abstract

This paper investigates the adaptive controller for the longitudinal dynamics of a generic hypersonic aircraft. The control-oriented model is adopted for design. The subsystem is transformed into the linearly parameterized form. Based on the parameter projection estimation, the dynamic inverse control is proposed via back-stepping. The dynamic surface method is employed to provide the derivative information of the virtual control. The proposed methodology addresses the issue of controller design with respect to parametric model uncertainty. Simulation results show that the proposed approach achieves good tracking performance in the presence of uncertain parameters.

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Acknowledgments

This work was supported by the DSO National Laboratories of Singapore through a Strategic Project Grant (Project No: DSOCL10004), National Science Foundation of China (Grant No:61134004), NWPU Basic Research Funding (Grant No: JC20120236), and Deutsche Forschungsgemeinschaft (DFG) Grant No. WU 744/1-1.

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Authors and Affiliations

  1. School of Automation, Northwestern Polytechnical University, Xi’An, China

    Bin Xu

  2. Department of Computer Science and Technology, Tsinghua University, Beijing, China

    Fuchun Sun & Shixing Wang

  3. Department of Mathematics and Computer Science, Free University of Berlin, Berlin, Germany

    Hao Wu

Authors
  1. Bin Xu
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  2. Fuchun Sun
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  3. Shixing Wang
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  4. Hao Wu
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Corresponding author

Correspondence to Bin Xu .

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Editors and Affiliations

  1. Department of Computer Science and Technology, Tsinghua University, Beijing, People's Republic of China

    Fuchun Sun

  2. School of Information Science and Technology, Southwest Jiaotong University, Chengdu, People's Republic of China

    Tianrui Li

  3. Department of Computer Science and Techn, Tsinghua University, Beijing, People's Republic of China

    Hongbo Li

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Xu, B., Sun, F., Wang, S., Wu, H. (2014). Dynamic Surface Control of Hypersonic Aircraft with Parameter Estimation. In: Sun, F., Li, T., Li, H. (eds) Foundations and Applications of Intelligent Systems. Advances in Intelligent Systems and Computing, vol 213. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-37829-4_56

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  • DOI: https://doi.org/10.1007/978-3-642-37829-4_56

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-37828-7

  • Online ISBN: 978-3-642-37829-4

  • eBook Packages: EngineeringEngineering (R0)

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