Loosely Formation-Displaced Geostationary Orbit Optimization with Complex Hybrid Sail Propulsion

Table 1

Spacecraft parameters.

Parameters	Leader	Follower 1	Follower 2
Initial mass (kg)	1000	900	800
Initial propellant mass (kg)	700	500	550
(s)	3200	3200	3200
	0.2	0.1	0.1