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

Table 6

Results of Monte Carlo simulation experiments.

Terms		Variable span	Invariable span
CEP		51.31	77.20
		50.61	74.76
		55.23	80.29
		6.2196	9.9341
		1.4145	1.4006
		0.0344	0.0478
		0.0056	0.0066
		0.0370	0.0476
		0.0076	0.0103