编队装配问题轨道要素的确定

2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720) Pub Date : 2004-03-13 DOI:10.1109/AERO.2004.1368059

S. Balaji, A. Tatnall

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引用次数: 0

摘要

本文利用欧拉变换矩阵，导出了紧密放置编队中希尔坐标系中航天器的坐标与其实际轨道元之间的一般关系。然后，在结果的帮助下，我们将轨道元素表示为相对于地球上的参考航天器的相对坐标的函数。对编队卫星轨道要素的了解有助于提前计划必要的机动，以建立所需的构型模式。

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Determination of orbital elements for the formation assembly problem

In this paper, we derive general relationships between the coordinates of the spacecraft in the Hill frame and their actual orbital elements for a closely placed formation with the help of Euler transformation matrices. Then, with the help of the results, we represent the orbital elements as a function of relative coordinates with respect to a reference spacecraft for an Earth-based scenario. The knowledge of orbital elements of the satellites in a formation help to plan ahead the necessary maneuvers to establish a desired configuration pattern.

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2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720)

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