Generalized Guidance Scheme for Low-Thrust Orbit Transfer

Table 2

The first simulation conditions.

	Initial values	Desired values
Semimajor axis ()	20000 km	20000 km
Eccentricity ()	0.3	0.3
Inclination angle ()	45°	45°
Longitude of the ascending node ()	205°	25°
Argument of perigee ()	225°	45°