Research on Three-Dimensional Integrated Guidance and Control Design with Multiple Constraints

Table 1

The initial condition for missile and target.

Symbol	Value	Symbol	Value	Symbol	Value
	0 m		5000 m		8 deg
	5000 m		1000 m		4 deg
	0 m		2000 m		8 deg
	600 m/s		50 m/s		20 deg/s
	15 deg		0 deg		-20 deg/s
	-5 deg		0 deg		-30 deg/s