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).

(a)

(b)

(c)

(d)

(e)

(f)