Midcourse Guidance Law Based on High Target Acquisition Probability Considering Angular Constraint and Line-of-Sight Angle Rate Control

Table 9

Simulation of the different positions.

Missile initial positions (, , )	Value
(, , )/m	(2000, 3000, 0)
(, , )/m	(1000, 3000, −350)
(, , )/m	(2000, 1000, −650)
(, , )/m	(2000, 5000, 500)
The end position of the midcourse guidance (, , )/m	(8921, 1740, 0)
Terminal angular constraint , /°	,
Terminal LOS angle rate (°/s)	2