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A Three-step Decomposition Method for Solving the Minimum-Fuel Geostationary Station Keeping of Satellites Equipped with Electric Propulsion

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Academic year: 2021

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Figure

Figure 2: Station Keeping window.
Figure 4: Parametrization of the j th thrust of the thruster i.
Figure 5: Effect of the threshold parameter ς on the half-width du- du-ration of the thrusts.
Figure 6: Continuous control profile at the end of step (A).
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