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Sliding-Mode-Based Attitude Tracking Control of Spacecraft Under Reaction Wheel Uncertainties

Wei Chen Qinglei Hu

自动化学报（英文版）2023，Vol.10Issue(6)：1475-1487,13.

自动化学报（英文版）2023，Vol.10Issue(6)：1475-1487,13.DOI:10.1109/JAS.2022.105665

Sliding-Mode-Based Attitude Tracking Control of Spacecraft Under Reaction Wheel Uncertainties

Wei Chen ¹Qinglei Hu²

作者信息

1. School of Automation Science and Electrical Engineering,Beihang University,Beijing 100191,China
2. School of Automation Science and Electrical Engineering,Beihang University,Beijing 100191,China||Beihang Hangzhou Innovation Institute Yuhang,Hangzhou 310023,China
折叠

摘要

关键词

Actuator failures/actuator misalignment angles/finite time/sliding mode control(SMC)/spacecraft attitude tracking

Key words

Actuator failures/actuator misalignment angles/finite time/sliding mode control(SMC)/spacecraft attitude tracking

引用本文复制引用

Wei Chen,Qinglei Hu..Sliding-Mode-Based Attitude Tracking Control of Spacecraft Under Reaction Wheel Uncertainties[J].自动化学报（英文版）,2023,10(6):1475-1487,13.

基金项目

This work was supported in part by the National Natural Science Foundation of China(61960206011,62227812),the Beijing Natural Science Foundation(JQ19017),the National Key Basic Research Program"Gravitational Wave Detection"Project(2021YFC2202600),and the Beijing Advanced Discipline Center for Unmanned Aircraft System. （61960206011,62227812）

自动化学报（英文版）

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