Attitude-Orbit Coupling Control Based on the Fully-Actuated Systems Approach Utilizing Dual Quaternion
Year: 2025
Type: conference-paper
Authors: Xuesong Li, Yingjing Qian
Institution: Beijing University of Technology
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4414170218
