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RESEARCH ON LONG-TERM ORBIT PROPAGATION FOR SPACE DEBRIS IN LEO

机译:狮子座空间碎片长期轨道传播的研究

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摘要

Space debris long-term orbit propagation is one of thernmain problems for the space debris environment models.rnThe evolution of space debris in low Earth orbit (LEO)rnis determined by a complex interplay of differentrnperturbations. The aim of this paper is to investigate thernlong-term effects of the most dominating perturbations:rnEarth geopotential effects, atmospheric drag, luni-solarrnperturbations and solar radiation pressure. Thernatmospheric drag is the major non-gravitationalrnperturbation in LEO. This article provides an averagernmethod of numerical integration on one revolution forrnrotating and stationary atmosphere, and then one canrnmake use of various atmospheric densities to calculaternthe orbital evolution. Using this method, we havernanalyzed the effects of rotating and stationaryrnatmospheric drag perturbation on orbital lifetime. Thernresults show the effects of solar activity andrngeomagnetic index on orbital evolution are obvious. Thernlifetime difference in rotating atmosphere is mostlyrndepending on inclinations of space debris.
机译:空间碎片的长期轨道传播是空间碎片环境模型的主要问题之一。低地球轨道(LEO)rnis中空间碎片的演化是由不同扰动的复杂相互作用决定的。本文的目的是研究最主要的扰动的长期影响:地球的地势效应,大气阻力,单日太阳能扰动和太阳辐射压力。大气阻力是LEO的主要非引力扰动。本文提供了一种在旋转和静止大气旋转一圈时的平均数值积分方法,然后可以利用各种大气密度来计算轨道演化。使用这种方法,我们已经分析了旋转和静止的大气阻力扰动对轨道寿命的影响。结果表明太阳活动和地磁指数对轨道演化的影响是明显的。旋转大气的寿命差异主要取决于空间碎片的倾角。

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  • 会议地点 Darmstadt(DE)
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    Hypervelocity Impact Research Center. P.O. Box 3020, Science Park, Harbin Institute of Technology,2 Yikuang Street, Nangang District, Harbin, P.R.China, 150080, Email: pengkeke2000@163.com;

    Hypervelocity Impact Research Center. P.O. Box 3020, Science Park, Harbin Institute of Technology,2 Yikuang Street, Nangang District, Harbin, P.R.China, 150080;

    Hypervelocity Impact Research Center. P.O. Box 3020, Science Park, Harbin Institute of Technology,2 Yikuang Street, Nangang District, Harbin, P.R.China, 150080;

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