resonant orbital dynamics in leo region: space debris in focus

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ID: 225682
2014
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Abstract
The increasing number of objects orbiting the earth justifies the great attention and interest in the observation, spacecraft protection, and collision avoidance. These studies involve different disturbances and resonances in the orbital motions of these objects distributed by the distinct altitudes. In this work, objects in resonant orbital motions are studied in low earth orbits. Using the two-line elements (TLE) of the NORAD, resonant angles and resonant periods associated with real motions are described, providing more accurate information to develop an analytical model that describes a certain resonance. The time behaviors of the semimajor axis, eccentricity, and inclination of some space debris are studied. Possible irregular motions are observed by the frequency analysis and by the presence of different resonant angles describing the orbital dynamics of these objects.
Reference Key
sampaio2014mathematicalresonant Use this key to autocite in the manuscript while using SciMatic Manuscript Manager or Thesis Manager
Authors ;J. C. Sampaio;E. Wnuk;R. Vilhena de Moraes;S. S. Fernandes
Journal journal of power sources
Year 2014
DOI
10.1155/2014/929810
URL
http://dx.doi.org/10.1155/2014/929810
Keywords
civil engineering (general)mathematics engineering (general)

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