Determination of thrusts to generate artificial equilibrium points in binary systems with applications to a planar solar sail
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Undergraduate course
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Acesso aberto
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Abstract
In this work, the artificial equilibrium points for a general two-body system are derived, visualized, and summarized as functions of the direction of the thrust, for several directions. The results for the Sun-Earth system are also presented. Planar solar sail applications are also considered.
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Keywords
Artificial equilibrium point, Astrodynamics, Nonlinear systems, Restricted three-body problem, Solar sail
Language
English
Citation
Nonlinear Dynamics, v. 95, n. 2, p. 919-942, 2019.
