Integrated Guidance and Control Method for the Interception of Maneuvering Hypersonic Vehicle Based on High Order Sliding Mode Approach

Table 4

Average miss distances of 50 simulations.

Target maneuvering timing	HOSM-IGC	HOSM-IGC	HOSM-IGC	OSMG
tgo = 1 second	4.3539	3.224	2.8936	3.6116
tgo = 2 seconds	2.5424	1.8665	0.9322	3.5534
tgo = 3 seconds	0.8124	0.8265	0.7538	1.1959