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- W2334971339 abstract "In order to maintain satellite missions long-term on-orbit servicing is necessary. One component of on-orbit servicing is on-orbit inspection. This study presents an original scenario for the use of Coulomb forcing for the purpose of on-orbit inspection. Within the framework of this study Coulomb force assisted deployment, guidance and docking of a deputy satellite is investigated. This deputy satellite is intended for use in carrying out external inspection of a main satellite. This paper specifically focuses on two-axis attitude control of a deputy satellite using Coulomb forces. The deputy satellite relative plane of motion is out of the orbital plane. Control logic is presented and numerical simulation results confirm that both relative attitude and positional control can be achieved under the assumed system conditions. The positional errors can be kept within several tens of millimeters whilst the angular errors can be kept within several degrees even in the worst case." @default.
- W2334971339 created "2016-06-24" @default.
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- W2334971339 date "2011-06-14" @default.
- W2334971339 modified "2023-09-24" @default.
- W2334971339 title "Two-Axis Attitude Control of a Deputy Satellite during Out-of-Plane Guidance in a Coulomb Formation" @default.
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- W2334971339 doi "https://doi.org/10.2514/6.2011-6707" @default.
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