Boost-Phase Trajectory Planning with the Nonregular Reachable Area Constraints

Table 4

Relationship between boost terminal states and reachable area boundary parameters.

States	States change	Variation of boundary curve parameters
Height (km)	0
	10.4
	17.3
	23.25
Velocity (m/s)	0
	69.2
	142
	216.3
Flight path angle (°)	4.25
	6.5
	7.8
	8.9