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Autor:
Li, Linxiao, Li, Aijun, Lu, Hongshi, Wang, Changqing, Zabolotnov, Yuriy Mikhailovich, Guo, Yong
Publikováno v:
Astrodynamics; Jun2024, Vol. 8 Issue 2, p247-259, 13p
Publikováno v:
Journal of Spacecraft and Rockets. 60:59-67
Spinning tether systems are considered a good platform for payload transportation and active removal of space debris. Such maneuvers require rendezvous with targeted objects. Due to the inevitable maneuvering error, rendezvous usually happens not at
Publikováno v:
2019 International Conference on Advanced Mechatronic Systems (ICAMechS).
The paper analyzes the deployment dynamics of a low-orbital tethered system. The low-orbital tethered system consists of a spacecraft and an atmospheric sounder that are connected by a tether. The tether is deployed from the spacecraft by means of a