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Sufficient Conditions for Input-to-State Stability of Spacecraft Rendezvous Problems via Their Exact Discrete-Time Model

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Intelligent Robotics and Applications (ICIRA 2015)

Part of the book series: Lecture Notes in Computer Science ((LNAI,volume 9244))

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Abstract

This paper investigates the sampled-data control problem for spacecraft rendezvous with target spacecraft on an arbitrary elliptical orbit. The exact discrete-time dynamic model and its Euler approximation are established based on the Lawden equations. With bounded external disturbances attached on the discrete-time model, input-to-state stability (ISS) analysis is introduced to design a sampled-data controller, which can achieve the rendezvous mission. Finally, simulation results show that the proposed control laws are effective.

K. Li—This work was supported by the National Natural Science Foundation of China under Grant 61273090 and the National Basic Research Program of China under Grant 973-10001.

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Authors and Affiliations

  1. Department of Automation, University of Science and Technology of China, Hefei, Anhui, 230027, People’s Republic of China

    Kun Li, Haibo Ji & Shaomin He

Authors
  1. Kun Li
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  2. Haibo Ji
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  3. Shaomin He
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Corresponding author

Correspondence to Kun Li .

Editor information

Editors and Affiliations

  1. University of Portsmouth, Portsmouth, United Kingdom

    Honghai Liu

  2. Tokyo Metropolitan University, Tokyo, Japan

    Naoyuki Kubota

  3. Shanghai Jiao Tong University, Shanghai, China

    Xiangyang Zhu

  4. Karlsruhe Institute of Technology, Karlsruhe, Germany

    Rüdiger Dillmann

  5. University of Portsmouth, Portsmouth, United Kingdom

    Dalin Zhou

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Li, K., Ji, H., He, S. (2015). Sufficient Conditions for Input-to-State Stability of Spacecraft Rendezvous Problems via Their Exact Discrete-Time Model. In: Liu, H., Kubota, N., Zhu, X., Dillmann, R., Zhou, D. (eds) Intelligent Robotics and Applications. ICIRA 2015. Lecture Notes in Computer Science(), vol 9244. Springer, Cham. https://doi.org/10.1007/978-3-319-22879-2_6

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  • DOI: https://doi.org/10.1007/978-3-319-22879-2_6

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-22878-5

  • Online ISBN: 978-3-319-22879-2

  • eBook Packages: Computer ScienceComputer Science (R0)

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