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首页> 外文期刊>Journal of Spacecraft and Rockets >Practical Operation Strategy for Deorbit of an Electrodynamic Tethered System
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Practical Operation Strategy for Deorbit of an Electrodynamic Tethered System

机译:电动系留系统脱轨的实用操作策略

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This paper presents an operation strategy employing electric current switching for deorbit of an electrodynamic tethered system. The electric current in the tether experiences some unexpected changes due to its plasma environment and thermal conditions. Libration control through current switching, in which only the on/off status of the current is determined, can avoid such changes and unexpected instability. A simple control law to determine current switching to stabilize both in-plane and out-of-plane libration is presented. A new stability function is also presented to facilitate evaluating the stability of a tethered system on an elliptic orbit. The effectiveness of the libration control strategy and the stability function is demonstrated through several numerical simulations. It is clearly indicated that the stability function and a switching control toward a periodic solution facilitate an appropriate stability evaluation and an efficient libration control. The control strategy is considered to be easily materialized in actual electrodynamic tethered systems, and enables a more rapid and secure deorbit.
机译:本文提出了一种采用电流切换的电动系留系统定轨的操作策略。由于其等离子体环境和热条件,系绳中的电流会发生一些意想不到的变化。通过仅确定电流的开/关状态的电流切换进行的振动控制可以避免这种变化和意外的不稳定。提出了确定电流开关以稳定平面内和平面外释放的简单控制律。还提出了一种新的稳定性函数,以方便评估椭圆轨道上的系留系统的稳定性。通过几个数值模拟证明了解放控制策略和稳定函数的有效性。清楚地表明,稳定性函数和朝向周期解的切换控制有助于适当的稳定性评估和有效的解放控制。该控制策略被认为可以在实际的电动系留系统中轻松实现,并且可以实现更快,更安全的脱轨。

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