Abstract
The libration motion of conductive tether in the electrodynamic tether system has been demonstrated to be inherently unstable. However, the relationship between the instability of libration motion and the tether current, orbital inclination and attitude of libration motion has not been thoroughly investigated. The novelty of this paper lies in the determination of the critical ranges of attitude and ε that lead to rapid tumbling of libration motion, and the study of how the instability of libration motion varies with attitude and ε, where ε accounts for the effects of tether current and orbital inclination. Some numerical simulations were conducted to demonstrate that, as attitude and ε increase, the instability of libration motion gradually becomes more pronounced, especially when the attitude angle or ε exceeds the respective critical range, in which case the libration will become unstable even with implementation of control strategy. The critical range of tether current, which leads to rapid tumbling of the libration motion, can be determined based on the range of ε, and this range of current can serve as a basis for designing the current regulation range, thereby preventing rapid tumbling that may result from improperly designed or regulated current values. The critical range of attitude angle can be utilized to monitor attitude motion and to avoid quick tumbling caused by excessive attitude angle.
Original language | English |
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Pages (from-to) | 13771-13784 |
Number of pages | 14 |
Journal | Nonlinear Dynamics |
Volume | 112 |
Issue number | 16 |
DOIs | |
Publication status | Published - Aug 2024 |
Keywords
- Dynamic instability
- Electrodynamic tether
- Nonlinear dynamics
- Space debris