立方体卫星轨道元的微扰效应

2017 International Conference on Advanced Technologies for Signal and Image Processing (ATSIP) Pub Date : 2017-05-22 DOI:10.1109/ATSIP.2017.8075534

A. Hanafi, M. Karim, El-Kaber Hachem, T. Rachidi, M. Sahmoudi

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引用次数: 7

摘要

本文的主要目的是利用Cowell方法对低地球轨道上立方体卫星轨道元素的摄动进行评估。干扰力驱使卫星(卫星的轨道)远离开普勒轨道，因此产生了开普勒轨道元素随时间的变化。本文在介绍了作用在近地轨道卫星上的摄动力的基础上，提出了轨道元与状态矢量的转换方法，最后对立方体卫星的轨道元摄动进行了评估。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Perturbation effects in orbital elements of CubeSats

The main objective of this paper is to evaluate the perturbations in CubeSat's orbital elements in low Earth orbits (LEO) using the Cowell's method. The disturbing forces are driving the satellite (the satellite's trajectory) away from Keplerian orbit, therefore produce a change in Keplerian orbital elements over time. In this paper, after introducing the perturbing forces acting on a satellite in LEO, the methods of converting the orbital elements into state vector and the opposite are being presented, and in the end, the perturbations in orbital elements of CubeSats in LEO are evaluated.

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来源期刊

2017 International Conference on Advanced Technologies for Signal and Image Processing (ATSIP)

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