research-article

Super-twisting Sliding Mode Observer Based Finite-Time Attitude Control of Combined Spacecraft

Authors:

Han Gao,

Liye Zu,

Yueyong Lv,

Chuanjiang LiAuthors Info & Claims

ICCAE '17: Proceedings of the 9th International Conference on Computer and Automation Engineering

Pages 222 - 226

https://doi.org/10.1145/3057039.3057048

Published: 18 February 2017 Publication History

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Abstract

A novel finite-time controller integrated with disturbance observer is proposed for a combined spacecraft in the presence of inertia uncertainty and external disturbance. As a stepping-stone, a super-twisting sliding mode disturbance observer(STDO) is designed firstly such that the reconstruction of lumped disturbances is accomplished in finite time and the observer error is convergence. Then, with the reconstructed information, a finite-time controller synthesized with the backstepping method, and command filter is used to avoid the too cumbersome analytic derivation, then the closed-loop system/state is proved to be finite-time stable. Numerical simulation results for the combined spacecraft show good performances, which validate the effectiveness and feasibility of the proposed scheme.

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Cited By

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Huang HSun GZhang DHuang GXu XZhang B(2021)Adaptive Attitude Control for a Kind of Heavy-Lift Launch Vehicle Based on Super-Twisting Algorithm2021 China Automation Congress (CAC)10.1109/CAC53003.2021.9728461(3288-3293)Online publication date: 22-Oct-2021
https://doi.org/10.1109/CAC53003.2021.9728461

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Published In

ICCAE '17: Proceedings of the 9th International Conference on Computer and Automation Engineering

February 2017

365 pages

ISBN:9781450348096

DOI:10.1145/3057039

Permission to make digital or hard copies of all or part of this work for personal or classroom use is granted without fee provided that copies are not made or distributed for profit or commercial advantage and that copies bear this notice and the full citation on the first page. Copyrights for components of this work owned by others than ACM must be honored. Abstracting with credit is permitted. To copy otherwise, or republish, to post on servers or to redistribute to lists, requires prior specific permission and/or a fee. Request permissions from [email protected]

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Macquarie U., Austarlia

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Association for Computing Machinery

New York, NY, United States

Publication History

Published: 18 February 2017

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National Nature Science Foundation

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ICCAE '17

ICCAE '17: 9th International Conference on Computer and Automation Engineering

February 18 - 21, 2017

Sydney, Australia

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Huang HSun GZhang DHuang GXu XZhang B(2021)Adaptive Attitude Control for a Kind of Heavy-Lift Launch Vehicle Based on Super-Twisting Algorithm2021 China Automation Congress (CAC)10.1109/CAC53003.2021.9728461(3288-3293)Online publication date: 22-Oct-2021
https://doi.org/10.1109/CAC53003.2021.9728461

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