Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/85154
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dc.contributor.authorHu, Qingleien
dc.contributor.authorWang, Danweien
dc.contributor.authorXie, Wenboen
dc.contributor.authorZhang, Jianen
dc.date.accessioned2017-08-30T07:42:20Zen
dc.date.accessioned2019-12-06T15:58:15Z-
dc.date.available2017-08-30T07:42:20Zen
dc.date.available2019-12-06T15:58:15Z-
dc.date.issued2017en
dc.identifier.citationZhang, J., Hu, Q., Wang, D., & Xie, W. (2017). Robust attitude coordinated control for spacecraft formation with communication delays. Chinese Journal of Aeronautics, 30(3), 1071-1085.en
dc.identifier.issn1000-9361en
dc.identifier.urihttps://hdl.handle.net/10356/85154-
dc.identifier.urihttp://hdl.handle.net/10220/43650en
dc.description.abstractIn this paper, attitude coordinated tracking control algorithms for multiple spacecraft formation are investigated with consideration of parametric uncertainties, external disturbances, communication delays and actuator saturation. Initially, a sliding mode delay-dependent attitude coordinated controller is proposed under bounded external disturbances. However, neither inertia uncertainty nor actuator constraint has been taken into account. Then, a robust saturated delay-dependent attitude coordinated control law is further derived, where uncertainties and external disturbances are handled by Chebyshev neural networks (CNN). In addition, command filter technique is introduced to facilitate the backstepping design procedure, through which actuator saturation problem is solved. Thus the spacecraft in the formation are able to track the reference attitude trajectory even in the presence of time-varying communication delays. Rigorous analysis is presented by using Lyapunov-Krasovskii approach to demonstrate the stability of the closed-loop system under both control algorithms. Finally, the numerical examples are carried out to illustrate the efficiency of the theoretical results.en
dc.format.extent15 p.en
dc.language.isoenen
dc.relation.ispartofseriesChinese Journal of Aeronauticsen
dc.rights© 2017 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).en
dc.subjectAttitude controlen
dc.subjectActuator saturationen
dc.titleRobust attitude coordinated control for spacecraft formation with communication delaysen
dc.typeJournal Articleen
dc.contributor.schoolSchool of Electrical and Electronic Engineeringen
dc.identifier.doihttp://dx.doi.org/10.1016/j.cja.2017.01.014en
dc.description.versionPublished versionen
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