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Finite-Time Adaptive Attitude Stabilization for Spacecraft Based on Modified Power Reaching Law

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Neural Information Processing (ICONIP 2017)

Part of the book series: Lecture Notes in Computer Science ((LNTCS,volume 10639))

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Abstract

In this paper, a finite-time adaptive sliding mode control scheme is proposed for the attitude stabilization of spacecrafts with lumped uncertainties. By introducing an exponential function in the reaching law design, an improved reaching law is developed such that the faster convergence of sliding mainfold can be achieved. Then, an adaptive controller is proposed based on the modified reaching law to guarantee the finite time attitude stabilization of spacecrafts by adaptive estimating the bounds of uncertainties. Besides, the chattering problem is reduced by using a power rate term in the controller design. Simulations are given to illustrate the effectiveness and superior performance of the proposed method.

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Acknowledgments

This work is supported by the National Natural Science Foundation of China under Grant No.61473262, No.6157332 and No.61403343, Zhejiang Provincial Natural Science Foundation under Grant No. Y17F030063.

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Authors and Affiliations

  1. Data-Driven Intelligent Systems Laboratory, College of Information Engineering, Zhejiang University of Technology, Hangzhou, 310023, China

    Meiling Tao, Qiang Chen, Xiongxiong He & Hualiang Zhuang

Authors
  1. Meiling Tao
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  2. Qiang Chen
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  3. Xiongxiong He
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  4. Hualiang Zhuang
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Corresponding author

Correspondence to Xiongxiong He .

Editor information

Editors and Affiliations

  1. Guangdong University of Technology, Guangzhou, China

    Derong Liu

  2. Guangdong University of Technology, Guangzhou, China

    Shengli Xie

  3. South China University of Technology, Guangzhou, China

    Yuanqing Li

  4. Institute of Automation, Chinese Academy of Sciences, Beijing, China

    Dongbin Zhao

  5. King Fahd University of Petroleum and Minerals, Dhahran, Saudi Arabia

    El-Sayed M. El-Alfy

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Tao, M., Chen, Q., He, X., Zhuang, H. (2017). Finite-Time Adaptive Attitude Stabilization for Spacecraft Based on Modified Power Reaching Law. In: Liu, D., Xie, S., Li, Y., Zhao, D., El-Alfy, ES. (eds) Neural Information Processing. ICONIP 2017. Lecture Notes in Computer Science(), vol 10639. Springer, Cham. https://doi.org/10.1007/978-3-319-70136-3_42

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  • DOI: https://doi.org/10.1007/978-3-319-70136-3_42

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-70135-6

  • Online ISBN: 978-3-319-70136-3

  • eBook Packages: Computer ScienceComputer Science (R0)

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