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

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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Correspondence to Kun Li .

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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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