Work

Fully-actuated System Approach-based Spacecraft Attitude Control under Tube-based Framework

Year: 2024

Type: conference-paper

Source: International Conference on Mechatronics, Robotics and Automation (ICMRA)

DOI: 10.1109/icmra62519.2024.10809175

Authors: Kerun Liu, Shiyi Li, Ming Liu

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

OpenAlex ID: W4405846005

FWCI:

Cites: 22

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Related to: 10