Integrated Guidance and Control for Hypersonic Morphing Missile Based on Variable Span Auxiliary Control

Table 2

The initial state of the missile and the latitude and longitude of the target point.

Name	Value	Name	Value	Name	Value
(m/s)	3000	(°)	2	(°)	0
(°)	0	(°)	0	(°)	0
(°)	0	(°)	0	(°)	1
()	0	(km)	0	(°)	1
()	0	(km)	30		0.40
()	0	(km)	0		0.55
(°)	60