Work

Unwinding-Free Performance of a Sliding-Mode Spacecraft Pose Controller Designed by Fully Actuated System Approaches

Year: 2025

Type: conference-paper

Source: Conference on Fully Actuated System Theory and Applications (FASTA)

DOI: 10.1109/fasta65681.2025.11138587

Authors: Fu-Zheng Xiao, Yong-Heng Yu, Li-Qun Chen

Institution: Harbin Institute of Technology

Language: English

Topic: Spacecraft Dynamics and Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: National Natural Science Foundation of China

Award: G6512881685

OpenAlex ID: W4414170307

FWCI:

Cites: 21

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