Research Article
Loosely Formation-Displaced Geostationary Orbit Optimization with Complex Hybrid Sail Propulsion
Figure 6
Strict formation on ideal displaced GEO: mass of pure SEP (a) leader, (b) follower 1, and (c) follower 2 and mass of hybrid sail (d) leader, (e) follower 1, and (f) follower 2 in the frame (A).
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