Reinforcement Learning for Computational Guidance of Launch Vehicle Upper Stage

Table 4

Results of experiment 2.

Parameter	Target orbit	Tracking reference trajectory	RL-guidance	Tracking reference trajectory with expanding flight time
Semimajor (m)	6588753	5953963	6588753	6588753
Eccentricity	0.0052	0.1046	0.0054	0.0102
Inclination (°)	20.009	19.991	20.009	20.019
Altitude of perigee (km)	176	-1047	175	143