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W2806746768 abstract "The pitch motion of a spacecraft in the planar elliptic restricted three-body system is studied. Previous studies laid the foundation for spacecraft stability analysis with a small perturbation to the zero pitch motion. In this study, a cell mapping approach that combines analytical and numerical techniques is used to study the global behavior of the full nonlinear spacecraft attitude in which coupling between orbital dynamics and attitude occurs. The effect of gravity gradient torques, orbital eccentricity, and the spacecraft configuration at different Lagrangian points is analyzed. Multiple-period periodic solutions and invariant surfaces are presented for different cases. Reference trajectories around the Lagrangian points are also considered to study coupled dynamics." @default.
W2806746768 created "2018-06-13" @default.
W2806746768 creator A5019872190 @default.
W2806746768 creator A5070062398 @default.
W2806746768 date "2016-09-09" @default.
W2806746768 modified "2023-09-30" @default.
W2806746768 title "Periodic Orbit-Attitude Solutions in the Planar Elliptic Restricted Three-Body Problem" @default.
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W2806746768 doi "https://doi.org/10.2514/6.2016-5685" @default.
W2806746768 hasPublicationYear "2016" @default.
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