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

Research output: Chapter in Book/Report/Conference proceedingConference contribution

5 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 languageEnglish (US)
Title of host publication2017 American Control Conference, ACC 2017
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages5812-5817
Number of pages6
ISBN (Electronic)9781509059928
DOIs
StatePublished - Jun 29 2017
Event2017 American Control Conference, ACC 2017 - Seattle, United States
Duration: May 24 2017May 26 2017

Publication series

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

Other

Other2017 American Control Conference, ACC 2017
CountryUnited States
CitySeattle
Period5/24/175/26/17

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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). [7963861] (Proceedings of the American Control Conference). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.23919/ACC.2017.7963861