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Optimal control of a space-borne laser system for a 100 m asteroid deflection under uncertainties

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Figure

Figure 1. Example of surface points producing thrustdirected along the y-axis
Table 1. Assumed Physical Properties of an S-TypeAsteroid
Table 1. The same arguments apply to the case of the thermalconductivity, which can undergo huge variations between thedifferent materials or simply because of the porous nature of
Figure 6. Achieved deflection with fixed thrust withfocus (case 2)
+4

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