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Xiao-Feng Liu

Researcher at Shanghai Jiao Tong University

Publications -  35
Citations -  343

Xiao-Feng Liu is an academic researcher from Shanghai Jiao Tong University. The author has contributed to research in topics: Control theory & Computer science. The author has an hindex of 7, co-authored 27 publications receiving 189 citations.

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Dynamics modeling and control of a 6-DOF space robot with flexible panels for capturing a free floating target

TL;DR: In this paper, the authors investigated the spatial dynamics and control of a 6-DOF space robot with flexible panels and spatial impact problem is considered, and the computed torque control method is used to design active controller to suppress the spacecraft drift caused by the impact.
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Dynamics and control of capture of a floating rigid body by a spacecraft robotic arm

TL;DR: In this paper, the dynamics and control of capturing a floating rigid body using a space robot are investigated, and the dynamic model of the system is established by the single direction recursive construction method and the Jourdain's velocity variation principle.
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Dynamics and control of space robot considering joint friction

TL;DR: In this article, the Coulomb friction model, the Stribeck friction model and the LuGre friction model are adopted to describe the joint friction and the calculation method for joint friction is discussed in detail, and the relationship between ideal constraint force and Lagrange multipliers is derived.
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Dynamics analysis of flexible space robot with joint friction

TL;DR: In this paper, the Coulomb friction model and LuGre friction model are adopted to describe the joint friction of a flexible space robot with a single-directional recursive construction method.
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Deployment dynamics and control of large-scale flexible solar array system with deployable mast

TL;DR: Simulation results indicate that the proposed model is effective to describe the deployment dynamics of the large-scale flexible solar arrays and the proposed controller is practical to eliminate the drift of spacecraft mainbody.