Adaptive sliding mode control for spacecraft rendezvous in near-circular orbits with time-varying saturation constraint

Neng Wan; Desineni S Naidu; Ming Liu; Ligang Wu; Weiran Yao

doi:10.23919/ACC.2017.7963861

Adaptive sliding mode control for spacecraft rendezvous in near-circular orbits with time-varying saturation constraint

Neng Wan
, Desineni S Naidu
, Ming Liu
, Ligang Wu
, Weiran Yao

Electrical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

10 Scopus citations

Abstract

An adaptive sliding mode control scheme is proposed for spacecraft rendezvous constrained by the external perturbations, the non-circularity of reference orbit, and the time-varying saturation, which can be induced by the temporal characteristics and the accidental faults of actuators. With some reasonable assumptions, we prove that the adaptive control scheme can achieve asymptotic stability without using the effectiveness information of actuators. Compared with the existing results, numerical experiment with longer initial distances, lower saturation bounds, and better performance is achieved within a nonlinear two-body system.

Original language	English (US)
Title of host publication	2017 American Control Conference, ACC 2017
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	5812-5817
Number of pages	6
ISBN (Electronic)	9781509059928
DOIs	https://doi.org/10.23919/ACC.2017.7963861
State	Published - Jun 29 2017
Event	2017 American Control Conference, ACC 2017 - Seattle, United States Duration: May 24 2017 → May 26 2017

Publication series

Name	Proceedings of the American Control Conference
ISSN (Print)	0743-1619

Other

Other	2017 American Control Conference, ACC 2017
Country/Territory	United States
City	Seattle
Period	5/24/17 → 5/26/17

Bibliographical note

Publisher Copyright:
© 2017 American Automatic Control Council (AACC).

Publisher link

10.23919/ACC.2017.7963861

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Wan, N., Naidu, D. S., Liu, M., Wu, L., & Yao, W. (2017). Adaptive sliding mode control for spacecraft rendezvous in near-circular orbits with time-varying saturation constraint. In 2017 American Control Conference, ACC 2017 (pp. 5812-5817). Article 7963861 (Proceedings of the American Control Conference). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.23919/ACC.2017.7963861

Adaptive sliding mode control for spacecraft rendezvous in near-circular orbits with time-varying saturation constraint. / Wan, Neng; Naidu, Desineni S; Liu, Ming et al.
2017 American Control Conference, ACC 2017. Institute of Electrical and Electronics Engineers Inc., 2017. p. 5812-5817 7963861 (Proceedings of the American Control Conference).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Wan, N, Naidu, DS, Liu, M, Wu, L & Yao, W 2017, Adaptive sliding mode control for spacecraft rendezvous in near-circular orbits with time-varying saturation constraint. in 2017 American Control Conference, ACC 2017., 7963861, Proceedings of the American Control Conference, Institute of Electrical and Electronics Engineers Inc., pp. 5812-5817, 2017 American Control Conference, ACC 2017, Seattle, United States, 5/24/17. https://doi.org/10.23919/ACC.2017.7963861

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AU - Yao, Weiran

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N2 - An adaptive sliding mode control scheme is proposed for spacecraft rendezvous constrained by the external perturbations, the non-circularity of reference orbit, and the time-varying saturation, which can be induced by the temporal characteristics and the accidental faults of actuators. With some reasonable assumptions, we prove that the adaptive control scheme can achieve asymptotic stability without using the effectiveness information of actuators. Compared with the existing results, numerical experiment with longer initial distances, lower saturation bounds, and better performance is achieved within a nonlinear two-body system.

AB - An adaptive sliding mode control scheme is proposed for spacecraft rendezvous constrained by the external perturbations, the non-circularity of reference orbit, and the time-varying saturation, which can be induced by the temporal characteristics and the accidental faults of actuators. With some reasonable assumptions, we prove that the adaptive control scheme can achieve asymptotic stability without using the effectiveness information of actuators. Compared with the existing results, numerical experiment with longer initial distances, lower saturation bounds, and better performance is achieved within a nonlinear two-body system.

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ER -

Adaptive sliding mode control for spacecraft rendezvous in near-circular orbits with time-varying saturation constraint

Abstract

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