Generalized Guidance Scheme for Low-Thrust Orbit Transfer

Table 3

The second simulation conditions.

	Initial values	Desired values
Semimajor axis ()	12878.14 km	20000 km
Eccentricity ()	0.4270803	0.6614378
Inclination angle ()	20°	45°
Longitude of the ascending node ()	90°	180°
Argument of perigee ()	0°	270°