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Self-organising low Earth orbit constellations for Earth observation

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Figure

Figure 1. Depiction of satellite constellation design.
Figure 2.Visualisation of the relationship between the PQW reference frame, andthe ECEF reference frame.
Figure 3. Typical time evolution of coupled selection equations for 5 competing modes, i “ 1, 2, ..., 5.
Figure 4. Time evolutions of coupled selection equation variables - the radius of eachsphere represents strength of pairing between the associated targets and satellites.Top left after 0 time steps, top right after 40 time steps, bottom left after 90 time steps,and bottom right after 140 time steps.
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