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Space Tether Deployment Control with Explicit Tension Constraint and Saturation Function

机译:具有显式张力约束和饱和功能的空间系绳展开控制

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摘要

This Note presents a nonlinear tension control law for the deployment of space tethers, where the positive tension constraint is explicitly accommodated by a special form of saturation function. The feedbackin the proposed controller is given analytically in terms of tether length and deployment rate, without the need of full state information. Compared with the recently developed fractional-order tension control scheme, the proposed controller achieves faster tether deployment with better stability. A large set of simulations is conducted to evaluate the performance of the controller and the impact of initial conditions of tether deployment on the convergence characteristics of the system trajectories. The statistical results show that the restriction on the initial conditions for the tether deployment to converge to the desired equilibrium point is quite loose under the proposed control law, which leaves a large margin for practical implementation.
机译:本说明提出了一种用于空间系链部署的非线性张力控制定律,其中正张力约束明确地由一种特殊形式的饱和函数来提供。建议的控制器中的反馈通过系链长度和展开速率进行分析,而无需完整的状态信息。与最近开发的分数阶张力控制方案相比,所提出的控制器实现了更快的系绳部署和更好的稳定性。进行了大量的仿真来评估控制器的性能以及系绳展开的初始条件对系统轨迹的收敛特性的影响。统计结果表明,在拟议的控制律下,束缚展开以收敛到所需平衡点的初始条件的限制非常宽松,为实际实施留有很大余地。

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  • 来源
    《Journal of guidance, control, and dynamics》 |2016年第4期|915-920|共6页
  • 作者单位

    Nanjing University of Aeronautics and Astronautics, 210016 Jiangsu, People's Republic of China;

    York University, Toronto, Ontario M3J 1P3, Canada;

    Nanjing University of Aeronautics and Astronautics, 210016 Jiangsu, People's Republic of China;

    Nanjing University of Aeronautics and Astronautics, 210016 Jiangsu, People's Republic of China;

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