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Trajectory Design and Optimization for LEO Satellites in Formation to Observe GEO Satellites’ Beams

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Figure

Figure 1. The diagram of the projection of the GEO satellites’ beamstwo-dimensional view and (b) Refers to the three-dimensional view
Figure 3. The procedure of the methods employed for solving the problem A of CTOC9.
Figure 4. The procedure of the IEMM algorithm. The solid arrows and circles refer to the recorded sequences, and the dotted arrows and circles refer to the abandoned sequences
Figure 5. The procedure of the MICM algorithm.
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