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Optimal H_∞ robust output feedback control for satellite formation in arbitrary elliptical reference orbits

机译:任意椭圆参考轨道上卫星编队的最优H_∞鲁棒输出反馈控制

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摘要

A two degree-of-freedom signal-based optimal H_∞ robust output feedback controller is designed for satellite formation in an arbitrary elliptical reference orbit. Based on high-fidelity linearized dynamics of relative motion, uncertainties introduced by non-zero eccentricity and gravitational J2 perturbation are separated to construct a robust control model. Furthermore, a distributed robust control model is derived by modifying the perturbed robust control model of each satellite with the eigenvalues of the Laplacian matrix of the communication graph, which represent uncertainty in the communication topology. A signal-based optimal H_∞ robust controller is then designed primarily. Considering that the uncertainties involved in the distributed robust control model have a completely diagonal structure, the corresponding analyses are made through structured singular value theory to reduce the conservativeness. Based on simulation results, further designs including increasing the degrees of freedom of the controller, modifying the performance and control weighted functions, adding a post high-pass filter according to the dynamic characteristics, and reducing the control model are made to improve the control performance. Nonlinear simulations demonstrate that the resultant optimal H_∞ robust output feedback controller satisfies the robust performance requirements under uncertainties caused by non-zero eccentricity, J2 perturbation, and varying communication topology, and that 5 m accuracy in terms of stable desired formation configuration can be achieved by the presented optimal H_∞ robust controller. In addition to considering the widely discussed uncertainties caused by the orbit of each satellite in a formation, the optimal H_∞ robust output feedback control model presented in the current work considers the uncertainties caused by varying communication topology in the satellite formation that works in a cooperative way. Other new improvements include adopting a new method to more accurately describe and analyze the effects of the higher-order J2 perturbation, combining all the uncertainties into a diagonal structure, and utilizing a structured singular value to synthesize and analyze the controller.
机译:设计了基于两自由度信号的最优H_∞鲁棒输出反馈控制器,用于在任意椭圆参考轨道上进行卫星编队。基于相对运动的高保真线性化动力学,将非零偏心率和重力J2扰动引入的不确定性分开,以构建鲁棒控制模型。此外,通过用通信图的拉普拉斯矩阵的特征值修改每颗卫星的扰动鲁棒控制模型来导出分布式鲁棒控制模型,该特征值表示通信拓扑中的不确定性。然后主要设计基于信号的最优H_∞鲁棒控制器。考虑到分布式鲁棒控制模型所涉及的不确定性具有完全对角线的结构,通过结构奇异值理论进行了相应的分析,以减少保守性。根据仿真结果,进一步设计包括增加控制器的自由度,修改性能和控制加权功能,根据动态特性添加后置高通滤波器以及简化控制模型以提高控制性能。 。非线性仿真表明,所得的最优H_∞鲁棒输出反馈控制器满足了在非零偏心率,J2扰动和变化的通信拓扑所造成的不确定性下的鲁棒性能要求,并且在稳定的所需地层配置方面可以实现5 m的精度通过提出的最优H_∞鲁棒控制器。除了考虑由编队中每颗卫星的轨道引起的广泛讨论的不确定性外,当前工作中提出的最优H_∞鲁棒输出反馈控制模型还考虑了协同工作的卫星编队中变化的通信拓扑结构引起的不确定性道路。其他新改进包括采用一种新方法来更准确地描述和分析高阶J2摄动的影响,将所有不确定性组合到对角线结构中以及利用结构化奇异值来合成和分析控制器。

著录项

  • 来源
    《Advances in space research》 |2014年第6期|969-989|共21页
  • 作者单位

    Harbin Institute of Technology, Harbin 150001, People's Republic of China,Yonsei University Observatory, Yonsei University, Seoul 120-749, Republic of Korea;

    Astrodynamics and Control Laboratory, Department of Astronomy & Yonsei University Observatory, Yonsei University, Seoul 120-749, Republic of Korea;

    Astrodynamics and Control Laboratory, Department of Astronomy & Yonsei University Observatory, Yonsei University, Seoul 120-749, Republic of Korea;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Satellite formation flying; Optimal H_∞ robust control; Output feedback control; Graph theory;

    机译:卫星编队飞行;最优H_∞鲁棒控制;输出反馈控制;图论;

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