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SciProfiles: 1137752
Scopus Author ID: 55017803100

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Education and qualifications (1)

York University: Toronto, ON, CA

2017-10 to 2018-10 | Visiting Student (Department of Earth and Space Science and Engineering)
Education
Source: Self-asserted source
Chuang Liu

Works (41)

Parallel layered scheme-based integrated orbit-attitude-vibration coupled dynamics and control for large-scale spacecraft

ISA Transactions
2025-03 | Journal article
DOI: 10.1016/j.isatra.2024.12.033
Contributors: Bailiang Lyu; Xiaokui Yue; Chuang Liu
Source: check_circle
Crossref

Integrated Predictor-Observer Feedback Control for Vibration Mitigation of Large-Scale Spacecraft With Unbounded Input Time Delay

IEEE Transactions on Aerospace and Electronic Systems
2024 | Journal article
DOI: 10.1109/TAES.2024.3505851
Contributors: Bailiang Lyu; Chuang Liu; Xiaokui Yue
Source: check_circle
Crossref

Reinforcement learning-based decision-making for spacecraft pursuit-evasion game in elliptical orbits

Control Engineering Practice
2024-12 | Journal article
DOI: 10.1016/j.conengprac.2024.106072
Contributors: Weizhuo Yu; Chuang Liu; Xiaokui Yue
Source: check_circle
Crossref

Improved sliding mode tracking control for spacecraft electromagnetic separation supporting on-orbit assembly

Advances in Space Research
2024-05 | Journal article
DOI: 10.1016/j.asr.2024.01.034
Contributors: Chuang Liu; Yiqing Ma; Xiaokui Yue; Keke Shi
Source: check_circle
Crossref

Non-fragile negative imaginary output feedback control for attitude stabilization of flexible spacecraft

Acta Astronautica
2023-07 | Journal article
DOI: 10.1016/j.actaastro.2023.04.002
Contributors: Ziyu Yang; Chuang Liu; Xiaokui Yue; Ming Guo
Source: check_circle
Crossref

Hybrid nonfragile intermediate observer-based T-S fuzzy attitude control for flexible spacecraft with input saturation

Aerospace Science and Technology
2022-09 | Journal article
DOI: 10.1016/j.ast.2022.107753
Contributors: Bailiang Lyu; Chuang Liu; Xiaokui Yue
Source: check_circle
Crossref

Constrained multi‐observer‐based fault‐tolerant disturbance‐rejection control for rigid spacecraft

International Journal of Robust and Nonlinear Control
2022-09-25 | Journal article
DOI: 10.1002/rnc.6270
Contributors: Bailiang Lyu; Xiaokui Yue; Chuang Liu
Source: check_circle
Crossref

Active Disturbance Rejection Control for Delayed Electromagnetic Docking of Spacecraft in Elliptical Orbits

IEEE Transactions on Aerospace and Electronic Systems
2022-06 | Journal article
DOI: 10.1109/TAES.2021.3130830
Contributors: Chuang Liu; Xiaokui Yue; Jianqiao Zhang; Keke Shi
Source: check_circle
Crossref

Finite-time controller design with adaptive fixed-time anti-saturation compensator for hypersonic vehicle

ISA Transactions
2022-03 | Journal article
DOI: 10.1016/j.isatra.2021.04.038
Contributors: Yibo Ding; Xiaokui Yue; Chuang Liu; Honghua Dai; Guangshan Chen
Source: check_circle
Crossref

Coupled orbit-attitude dynamics and trajectory tracking control for spacecraft electromagnetic docking

Applied Mathematical Modelling
2022-01 | Journal article
DOI: 10.1016/j.apm.2021.08.030
Contributors: Keke Shi; Chuang Liu; Zhaowei Sun; Xiaokui Yue
Source: check_circle
Crossref

Are nonfragile controllers always better than fragile controllers in attitude control performance of post-capture flexible spacecraft?

Aerospace Science and Technology
2021-11 | Journal article
DOI: 10.1016/j.ast.2021.107053
Contributors: Chuang Liu; Xiaokui Yue; Ziyu Yang
Source: check_circle
Crossref

Finite-time distributed hierarchical control for satellite cluster with collision avoidance

Aerospace Science and Technology
2021-07 | Journal article
DOI: 10.1016/j.ast.2021.106750
Contributors: Siyuan Li; Chuang Liu; Zhaowei Sun
Source: check_circle
Crossref

Fuzzy-logic-based adaptive event-triggered sliding mode control for spacecraft attitude tracking

Aerospace Science and Technology
2021-01 | Journal article
DOI: 10.1016/j.ast.2020.106394
Contributors: Lei Xing; Jianqiao Zhang; Chuang Liu; Xiao Zhang
Source: check_circle
Crossref

Additional Cover

International Journal of Robust and Nonlinear Control
2020-09-10 | Journal article
DOI: 10.1002/rnc.5187
Contributors: Chuang Liu; Keke Shi; Xiaokui Yue; Zhaowei Sun
Source: check_circle
Crossref

Inertia‐free saturated output feedback attitude stabilization for uncertain spacecraft

International Journal of Robust and Nonlinear Control
2020-09-10 | Journal article
DOI: 10.1002/rnc.5044
Contributors: Chuang Liu; Keke Shi; Xiaokui Yue; Zhaowei Sun
Source: check_circle
Crossref
grade
Preferred source (of 2)‎

Disturbance observer-based attitude stabilization for rigid spacecraft with input MRCs

Advances in Space Research
2020-08 | Journal article
DOI: 10.1016/j.asr.2020.04.016
Contributors: Keke Shi; Chuang Liu; Zhaowei Sun; Xiaokui Yue
Source: check_circle
Crossref
grade
Preferred source (of 2)‎

Observer-based control for spacecraft electromagnetic docking

Aerospace Science and Technology
2020-04 | Journal article
DOI: 10.1016/j.ast.2020.105759
Part of ISSN: 1270-9638
Source: Self-asserted source
Chuang Liu
grade
Preferred source (of 2)‎

Inertia‐free attitude stabilization for flexible spacecraft with active vibration suppression

International Journal of Robust and Nonlinear Control
2019-12 | Journal article
DOI: 10.1002/rnc.4742
Contributors: Chuang Liu; Xiaokui Yue; Keke Shi; Zhaowei Sun
Source: check_circle
Crossref
grade
Preferred source (of 2)‎

Constrained fuel-free control for spacecraft electromagnetic docking in elliptical orbits

Acta Astronautica
2019-09 | Journal article
DOI: 10.1016/j.actaastro.2019.05.016
Contributors: Keke Shi; Chuang Liu; Zhaowei Sun
Source: check_circle
Crossref
grade
Preferred source (of 2)‎

Robust H∞ controller design for attitude stabilization of flexible spacecraft with input constraints

Advances in Space Research
2019-03 | Journal article
DOI: 10.1016/j.asr.2018.10.043
Contributors: Chuang Liu; Keke Shi; Zhaowei Sun
Source: check_circle
Crossref
grade
Preferred source (of 2)‎

Extended state observer based robust adaptive control on SE(3) for coupled spacecraft tracking maneuver with actuator saturation and misalignment

Acta Astronautica
2018 | Journal article
DOI: 10.1016/j.actaastro.2017.11.034
EID:

2-s2.0-85036655609
Contributors: Zhang, J.; Ye, D.; Sun, Z.; Liu, C.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Observer-based fault-tolerant attitude control for spacecraft with input delay

Journal of Guidance, Control, and Dynamics
2018 | Journal article
DOI: 10.2514/1.G003555
EID:

2-s2.0-85052848957
Contributors: Liu, C.; Vukovich, G.; Sun, Z.; Shi, K.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Robust fault tolerant nonfragile H <inf>∞</inf> attitude control for spacecraft via stochastically intermediate observer

Advances in Space Research
2018 | Journal article
DOI: 10.1016/j.asr.2018.07.026
EID:

2-s2.0-85051127612
Contributors: Liu, C.; Vukovich, G.; Shi, K.; Sun, Z.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Robust non-fragile state feedback attitude control for uncertain spacecraft with input saturation

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
2018 | Journal article
DOI: 10.1177/0954410016679194
EID:

2-s2.0-85041468635
Contributors: Liu, C.; Sun, Z.; Shi, K.; Wang, F.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Spacecraft chaotic attitude control with certain actuator failure based on integral sliding mode

Journal of Engineering Research
2018 | Journal article
EID:

2-s2.0-85053699690
Contributors: Liu, C.; Shi, K.; Sun, Z.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Spacecraft chaotic attitude control with certain actuator failure based on integral sliding mode

Journal of Engineering Research (Kuwait)
2018 | Journal article
EID:

2-s2.0-85074934392

Part of ISBN:

23071885
Contributors: Liu, C.; Shi, K.; Sun, Z.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

A novel robust non-fragile control approach for a class of uncertain linear systems with input constraints

2018-10-04 | Journal article
DOI: 10.1177/0142331218799835
Source: Self-asserted source
Chuang Liu
grade
Preferred source (of 2)‎

Dynamics modeling and simulation of space electromagnetic docking for CubeSat

2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
2017 | Conference paper
DOI: 10.1109/ICMAE.2017.8038716
EID:

2-s2.0-85032335069
Contributors: Shi, K.; Sun, Z.; Liu, C.; Ye, D.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Robust adaptive variable structure tracking control for spacecraft chaotic attitude motion

IEEE Access
2017 | Journal article
DOI: 10.1109/ACCESS.2017.2788860
EID:

2-s2.0-85040041151
Contributors: Liu, C.; Sun, Z.; Ye, D.; Shi, K.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier
grade
Preferred source (of 2)‎

Robust high-precision attitude control for flexible spacecraft with improved mixed H<inf>2</inf>/H<inf>∞</inf> control strategy under poles assignment constraint

Acta Astronautica
2017 | Journal article
DOI: 10.1016/j.actaastro.2017.03.009
EID:

2-s2.0-85015721238
Contributors: Liu, C.; Ye, D.; Shi, K.; Sun, Z.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Underactuated spacecraft chaotic attitude control based on exponential reaching law

2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
2017 | Conference paper
DOI: 10.1109/ICMAE.2017.8038718
EID:

2-s2.0-85032362345
Contributors: Sun, Z.; Liu, C.; Shi, K.; Zhang, J.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Robust dynamic output feedback control for attitude stabilization of spacecraft with nonlinear perturbations

Aerospace Science and Technology
2017-05 | Journal article
DOI: 10.1016/j.ast.2017.01.016
Contributors: Chuang Liu; Zhaowei Sun; Keke Shi; Feng Wang
Source: check_circle
Crossref
grade
Preferred source (of 2)‎

Mixed H<inf>2</inf>/H<inf>∞</inf> control approach and its application in satellite attitude control system

International Journal of Engineering Research in Africa
2016 | Journal article
DOI: 10.4028/www.scientific.net/JERA.25.89
EID:

2-s2.0-84982295573
Contributors: Liu, C.; Sun, Z.; Shi, K.; Wang, F.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Mixed H<inf>2</inf>/H<inf>∞</inf> state feedback attitude control of microsatellite based on extended LMI method

Journal of Harbin Institute of Technology (New Series)
2016 | Journal article
DOI: 10.11916/j.issn.1005-9113.2016.05.003
EID:

2-s2.0-85011700161
Contributors: Shi, K.; Liu, C.; Wang, F.; Sun, Z.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Design of microsatellite attitude control with multiplicative perturbation of controller

Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015
2015 | Conference paper
DOI: 10.1109/CCDC.2015.7161742
EID:

2-s2.0-84945572630
Contributors: Shi, K.; Sun, Z.; Liu, C.; Wang, F.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

In-orbit estimation of inertia parameters of target satellite after capturing the tracking satellite

Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
2015 | Conference paper
DOI: 10.1109/WCICA.2014.7053375
EID:

2-s2.0-84932189203
Contributors: Liu, C.; Wang, F.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Mass and mass center identification of target satellite after rendezvous and docking

Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
2015 | Conference paper
DOI: 10.1109/WCICA.2014.7053711
EID:

2-s2.0-84932153716
Contributors: Liu, C.; Shi, K.; Wang, F.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Mixed H<inf>2</inf>/H<inf>∞</inf> approach of full order state observer design for satellite attitude control system

Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015
2015 | Conference paper
DOI: 10.1109/CCDC.2015.7162720
EID:

2-s2.0-84945561744
Contributors: Shi, K.; Liu, C.; Sun, Z.; Wang, F.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

The design of guidance law and error analysis in deceleration process of lunar soft landing

Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014
2015 | Conference paper
DOI: 10.1109/ICMC.2014.7231748
EID:

2-s2.0-84953731417
Contributors: Zhang, Z.; Liu, C.; Ye, D.; Sun, Z.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Simulations for orbital maintenance of low-angle satellite based on STK

Energy Education Science and Technology Part A: Energy Science and Research
2014 | Journal article
EID:

2-s2.0-84931266501
Contributors: Liu, C.; Wang, F.; Shi, K.; Guo, J.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Optimizing design of auxiliary support for solar panel of agile satellite

Guangxue Jingmi Gongcheng/Optics and Precision Engineering
2013 | Journal article
DOI: 10.3788/OPE.20132113.0108
EID:

2-s2.0-84899085658
Contributors: Wang, F.; Guo, J.-S.; Liu, C.
Source: Self-asserted source
Chuang Liu via Scopus - Elsevier

Peer review (40 reviews for 14 publications/grants)

Review activity for Acta astronautica. (2)
Review activity for Advances in space research (13)
Review activity for Aerospace science and technology. (6)
Review activity for AIP advances. (3)
Review activity for Chinese Journal of Aeronautics. (1)
Review activity for European journal of control. (1)
Review activity for Frontiers of Information Technology & Electronic Engineering. (1)
Review activity for Information sciences. (1)
Review activity for International journal of dynamics and control. (1)
Review activity for ISA transactions. (7)
Review activity for Mathematics and computers in simulation. (1)
Review activity for Nonlinear dynamics. (1)
Review activity for Soft computing. (1)
Review activity for Systems & control letters. (1)
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