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

Table 5

Initial conditions.

Variable	Description	Value
(, )	Missile initial position	(0 km, 17.5 km)
(, )	Target initial position	(60 km, 19.5 km)
	Missile initial velocity	1200 (m/s)
	Target initial velocity	2000 (m/s)
	Missile initial flight path angle	0 (deg)
	Target initial flight path angle	0 (deg)
	Compensatory gain	3
	Saturation parameter	0.001