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Archive of Applied Mechanics
Erschienen in: Archive of Applied Mechanics 12/2021

04.09.2021 | Original

Analysis of nominal halo orbits in the Sun–Earth system

verfasst von: Elbaz I. Abouelmagd, Ashok Kumar Pal, Juan Luis García Guirao

Erschienen in: Archive of Applied Mechanics | Ausgabe 12/2021

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Abstract

In this paper, the effect of radiation pressure force on formation of the nominal halo orbit around the collinear point \(L_1\) is estimated in the framework of Sun–Earth system. Using Lindstedt–Poincaré technique, the periodic solutions up to third-order approximation are computed. Further, the Fourier series solutions of nominal halo orbit are also evaluated. With considering the radiation pressure force effect, the proposed analysis in this work can be used to design a trajectory for spacecraft moving in more realistic system.
Vorheriger Artikel Elastoplastic nonlinear analysis of functionally graded beams utilizing the symplectic method
Nächster Artikel Buckling analysis of nanobeams with deformable boundaries via doublet mechanics

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Metadaten
Titel
Analysis of nominal halo orbits in the Sun–Earth system
verfasst von
Elbaz I. Abouelmagd
Ashok Kumar Pal
Juan Luis García Guirao
Publikationsdatum
04.09.2021
Verlag
Springer Berlin Heidelberg
Erschienen in
Archive of Applied Mechanics / Ausgabe 12/2021
Print ISSN: 0939-1533
Elektronische ISSN: 1432-0681
DOI
https://doi.org/10.1007/s00419-021-02031-y

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