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Digital LQR control scheme to maintain the separation distance of the NASA benchmark tetrahedron constellation

机译:数字LQR控制方案可保持NASA基准四面体星座的分隔距离

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摘要

In previous papers, the authors developed an active control scheme based on the linear quadratic regulator (LQR) to maintain the separation distance constraints of the NASA benchmark tetrahedron constellation. Two different active control schemes were used to maintain the separation distance constraints, but one control scheme applied to every eccentricity of the NASA benchmark problem. Through this paper, the digital LQR strategy will be developed with this active control scheme to maintain the separation distance conditions of the tetrahedron constellation. The motion of a pair of satellites in an elliptical orbit about the Earth is defined by the linearized Tschauner-Hempel (TH) equations. These equations will be defined discretely in the true anomaly angle for the development of the digital control scheme. In summary, the digital LQR approach will be implemented and studied to determine how this active control scheme maintains the separation distance constraints for different specific sizes of the NASA benchmark tetrahedron constellation.
机译:在先前的论文中,作者开发了一种基于线性二次调节器(LQR)的主动控制方案,以维持NASA基准四面体星座的分离距离约束。两种不同的主动控制方案被用来维持间隔距离约束,但是一种控制方案被应用于NASA基准问题的每个偏心率。通过本文,将采用这种主动控制方案来开发数字LQR策略,以保持四面体星座的分离距离条件。一对椭圆轨道绕地球轨道的一对卫星的运动由线性化的Tschauner-Hempel(TH)方程定义。这些方程将在真实异常角度中离散定义,以开发数字控制方案。总而言之,将实施和研究数字LQR方法,以确定这种主动控制方案如何针对NASA基准四面体星座的不同特定大小来保持间隔距离约束。

著录项

  • 来源
    《Acta astronautica》 |2009年第8期|1058-1067|共10页
  • 作者单位

    Department of Mechanical Engineering, Howard University, Washington, DC 20059, USA EV41, Guidance, Navigation & Control Systems Design & Analysis Branch, NASA Marshall Space Flight Center, Huntsville, AL 35812, USA;

    Department of Mechanical Engineering, Howard University, Washington, DC 20059, USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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