Rotation matrix-based finite-time attitude coordinated control for spacecraft

Chao Tan,Guodong Xu,Limin Dong,Yaen Xie,Yushan He,Yong Hao,Fei Han

Advances in Space Research（2022）

引用 6|浏览8

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摘要

•Rotation matrix-based finite-time attitude coordinated control is studied;•An attitude controller is synthesized by the utilization of terminal sliding mode;•A novel sliding mode surface has been developed for finite-time convergence;

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关键词

Rotation matrix,Finite-time coordinate control,Spacecraft formation flying,Terminal sliding mode

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