Boost-Phase Trajectory Planning with the Nonregular Reachable Area Constraints

Table 9

Comparison results.

Item		hpPM	NSGA II
Terminal deviations	Height (m)	0.0	76.0
	Velocity (m/s)	0.0	9.6
	Flight path angle (°)	0.0
	Heading angle (°)
Performance index	Maximum range (km)	988.5	987.1
Path constraints	Maximum attack angle (°)	20.0	20.0
	Maximum change rate of attack angle (°/s)	5.8	34.2
	Maximum sideslip angle (°)	10.0	7.3
	Maximum change rate of sideslip angle (°/s)	1.4
Timeliness	Calculation time (s)	2.8	318.3