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• W2532479877 abstract "We study the control plane motion of an axisymmetric satellite with a movable mass on its axis of symmetry in circular orbit under the influence of a gravity torque. The problem of the gravitational stabilization to in-plane perturbations of two diametrically opposite relative equilibrium positions of the satellite in a circular orbit using the swing-by technique is solved. A restricted law with continuous derivative for controlling the movable mass is proposed. We solve the problem of reorientation of the satellite by moving it from one stable equilibrium position to the other. The theoretical results are illustrated by graphical representation of the numerical simulation." @default.
• W2532479877 created "2016-10-28" @default.
• W2532479877 creator A5072500715 @default.
• W2532479877 date "2016-04-01" @default.
• W2532479877 modified "2023-09-26" @default.
• W2532479877 title "The bounded control gravitational stabilization problem for satellites with movable mass" @default.
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• W2532479877 doi "https://doi.org/10.1109/codit.2016.7593614" @default.
• W2532479877 hasPublicationYear "2016" @default.
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