Modeling and analysis of tethered satellite systems based on spinning deployment
Year: 2024
Type: conference-paper
Abstract: In recent years, with space science and technology development, tethered satellites have been widely recognized and valued. This paper analyzes a tether satellite system based on spinning deployment by dynamic modeling and numerical simulation to analyze the factors affecting its deployment stability. Firstly, the dynamic model of the tethered satellite system under the action of spinning centrifugal force is established using the dumbbell model. Then, numerical simulation is conducted to study the factors affecting the deployment stability of the tethered satellite system. Finally, a feasible and stable deployment control method is proposed based on actual working conditions.
Authors: Guotong Liu, Fengchen Fan, Yuanqing Miao, Tianyu Zhang, Yushu Bian
Institutions: Beihang University, China Academy of Space Technology
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: diamond
OpenAlex ID: W4404266851