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- W2955406425 abstract "This paper studies the spinning stability of a triangular tethered satellite formation that flies on a low earth orbit. The spinning around the center of mass at a constant angular rate gives rise to a periodic motion in the non-inertial orbital frame. Floquet theory is used to analyze the stability of the periodic motion. A dynamic similarity between the on-orbit dynamics and ground experimental models is built to construct an equivalent ground experiment to verify the stability analysis. The analytical and experimental results show that a stable periodic motion can be guaranteed if the spinning angular rate of the system exceeds a critical value." @default.
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- W2955406425 date "2019-09-01" @default.
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- W2955406425 title "Stability and ground experiments of a spinning triangular tethered satellite formation on a low earth orbit" @default.
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- W2955406425 doi "https://doi.org/10.1016/j.ast.2019.06.012" @default.
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