Generalized Guidance Scheme for Low-Thrust Orbit Transfer

Table 4

The third simulation conditions.

	Initial values	Desired values
Semimajor axis ()	7278.14 km	7478.14 km
Eccentricity ()	0.0137398	0.0133723
Inclination angle ()	15°	45°
Longitude of the ascending node ()	25°	0°
Argument of perigee ()	45°	0°