Time-Delayed Feedback Control in Astrodynamics
Time-Delayed Feedback Control in Astrodynamics
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DOI：
10.2514/1.43672
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发表时间：
2009-11
影响因子：
2.6
通讯作者：
J. Biggs;C. McInnes
中科院分区：
文献类型：
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作者：
J. Biggs;C. McInnes
本文提出了时滞反馈控制(TDFC)，目的是将非线性系统的轨迹自主驱动到周期轨道。由于周期轨道的产生是非动力学中许多问题的主要组成部分，我们提出这种方法作为这类应用中的一个有用工具。为了激励这种方法的使用，我们将它应用于天体动力学文献中的一些众所周知的问题。首先，将TDFC应用于椭圆轨道上非对称卫星混沌姿态运动的控制。其次，我们将TDFC应用于航天器在大椭圆度物体(如小行星)的周期轨道上的保持问题，最后，我们应用TDFC来消除低地球轨道上的两颗卫星之间的漂移，以确保它们的相对运动是有界的。
In this paper we present time-delayed feedback control (TDFC) for the purpose of autonomously driving trajectories of nonlinear systems into periodic orbits. As the generation of periodic orbits is a major component of many problems in astodynamics we propose this method as a useful tool in such applications. To motivate the use of this method we apply it to a number of well known problems in the astrodynamics literature. Firstly, TDFC is applied to control in the chaotic attitude motion of an asymmetric satellite in an elliptical orbit. Secondly, we apply TDFC to the problem of maintaining a spacecraft in a periodic orbit about a body with large ellipticity (such as an asteroid) and finally, we apply TDFC to eliminate the drift between two satellites in low Earth orbits to ensure their relative motion is bounded.