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

Table 4

Parameter optimization value of the IGC method for the invariable span missile.

Name	Value	Name	Value	Name	Value
	3.22		10.21		2.14
	0.71		2.14		2.41
	0.23		1.75		5.60
	0.51		0.41		0.74
	0.13		0.56		0.44
	0.21		40.21		0.45
	0.35		0.75		75.30
					0.12