de Almeida, A. K.Prado, A. F.B.A.Yokoyama, T. [UNESP]2019-10-062019-10-062019-01-30Nonlinear Dynamics, v. 95, n. 2, p. 919-942, 2019.1573-269X0924-090Xhttp://hdl.handle.net/11449/187026In 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.919-942engArtificial equilibrium pointAstrodynamicsNonlinear systemsRestricted three-body problemSolar sailDetermination of thrusts to generate artificial equilibrium points in binary systems with applications to a planar solar sailArtigo10.1007/s11071-018-4605-3Acesso aberto2-s2.0-85055951018