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Publishing Language: Chinese

Key technologies and prospects for separation dynamics of stacked satellite systems

Dongping JIN1,2Dingfeng DING1,2Lin WU1,2Hao WEN1,2Xiaotong ZHANG3Jialiang SUN1,2( )
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing 210016, China
Shanghai Institute of Satellite Engineering, Shanghai 201109, China
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Abstract

Recent years have witnessed the rapid development of satellite internet constellation via low-orbit communication satellites in the main aerospace industries of various countries. For efficient construction of the satellite internet constellation, researchers from the main aerospace industries focus on the technologies of multi-satellite launch of stacked satellite system, as well as autonomous separation and reconfiguration on orbit. Therefore, this paper reviews the application requirements and launch merits of stacked satellites, and introduces the development of the launched stacked satellites all over the world. For the challenges of on orbit separation, this paper also presents the configuration design of the stacked satellites and the optimization design of separation mechanisms. For the separation dynamics of the stacked satellites, the paper outlines the dynamic modeling and simulation methods for the system before separation, the rigid multibody system during separation, and most importantly, the contact detection algorithms during separation. For the ground experiment validations, the paper briefly exhibits the experiment platform and results for separations of two satellites between layers and in the same layer. Finally, the key technologies of stacked satellites separation dynamics are summarized, and several frontier directions for further study are highlighed.

CLC number: V11;O313 Document code: A Article ID: 1000-6893(2025)05-531342-26

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
JIN D, DING D, WU L, et al. Key technologies and prospects for separation dynamics of stacked satellite systems. Acta Aeronautica et Astronautica Sinica, 2025, 46(5). https://doi.org/10.7527/S1000-6893.2024.31342

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Received: 30 September 2024
Revised: 09 October 2024
Accepted: 16 October 2024
Published: 30 October 2024
© 2025 The Journal of Acta Aeronautica et Astronautica Sinica