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Coordinated formation control strategy of the rotating hub-spoke tethered formation system

机译:轮毂-辐条式束缚编队系统的协调编队控制策略

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摘要

The hub-spoke tethered formation system (HS-TFS) is attractive in many space applications, such as multi-point measurements, providing flexible frame for solar sail and other membrane or net structures. To utilize the specific advantages of the system, such as reduction of fuel consumption, promotion of the formation stability, the HS-TFS is usually designed as a rotating system. However, the rotating motion will increase the complexity of the formation control of the HS-TFS. In this paper, the formation control of the rotating HS-TFS is investigated. First, an analytical model based on several reasonable assumptions is introduced to describe the dynamics of the rotating HS-TFS. Based on this model, two coordinated formation control strategies are proposed and described in detail, in which the tension forces of the tethers, propulsions of the sub-spacecraft, and the torque of the master-spacecraft are used as control inputs. Then a closed-loop control system is constructed to validate the proposed coordinated formation control strategies. Finally detailed numerical simulations are implemented based on the closed-loop control system. The simulation results show that the proposed coordinated control strategies are capable of assigning the operating time of the torque of the master-spacecraft and improving the efficiency of the formation control of the rotating HS-TFS.
机译:轮辐式束缚编队系统(HS-TFS)在许多空间应用中都很有吸引力,例如多点测量,可为太阳帆和其他膜或网状结构提供灵活的框架。为了利用系统的特定优势,例如减少燃油消耗,提高地层稳定性,HS-TFS通常设计为旋转系统。但是,旋转运动将增加HS-TFS的编队控制的复杂性。本文研究了旋转HS-TFS的形成控制。首先,引入了基于几个合理假设的分析模型来描述旋转HS-TFS的动力学。在此模型的基础上,提出并详细描述了两种协调编队控制策略,其中系绳的拉力,子航天器的推进力和主航天器的扭矩用作控制输入。然后构造一个闭环控制系统来验证所提出的协调编队控制策略。最后,基于闭环控制系统进行了详细的数值模拟。仿真结果表明,所提出的协调控制策略能够分配主航天器扭矩的工作时间,并提高了HS-TFS旋转编队控制的效率。

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