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Research article

First published 2019-2

Dynamic sliding mode-based attitude stabilisation control of satellites with angular velocity and control constraints

Chunmei Yu, Xun Xie

Transactions of the Institute of Measurement and Control

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Research article

First published 2026-1

An anti-unwinding finite-time attitude tracking control method of rigid spacecraft considering angular velocity constraints and disturbances

Ji Wang, Xiangyu Wang

Proceedings of the Institution of Mechanical Engineers,Part I: Journal of Systems and Control Engineering

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Research article

First published 2019-2

A time suboptimal method for real-time spacecraft attitude agile maneuvering with angular velocity constraint

Yun-Hua Wu, Ya-Bo Hu, Bing Hua [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2020-11

Rigid-body attitude control guaranteeing finite-time convergence

Shenhao Li, Taotao Zhang

Measurement and Control

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Research article

First published 2021

Velocity-free attitude tracking for rigid spacecraft via bounded control

Jian Zhang, Wen-Jie Wu, Long Liu [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2025-6

Adaptive time-varying sliding mode attitude maneuver control for multirotary-joint solar power satellite under constraints

Song Xu, Naiming Qi, Mingying Huo [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2014-11

A novel high precision inertial measurement scheme and its optimization method for high-speed rotating ammunition

Qingya Wu, Qingzhong Jia, Jiayuan Shan [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2018-2

Finite-time attitude controller design via dual-loop control strategy

Chun W Yin, Ming S Hou, Ming X Li

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2009-3

Potential approach for constrained autonomous manoeuvres of a spacecraft equipped with a cluster of control moment gyroscopes

G Avanzini, G Radice, I Ali

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

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Research article

First published 2011-3

Adaptive quaternion-based output feedback control for flexible spacecraft attitude tracking with input constraints

B Xiao, Q Hu, G Ma

Proceedings of the Institution of Mechanical Engineers,Part I: Journal of Systems and Control Engineering

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