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

Table 7

Conditions for the simulations (moving target).

Parameter	Value
Missile midcourse navigation initial position (, , )/m	(3000, 3500, −500)
Missile midcourse velocity (m/s)	370
The end position of the midcourse guidance (, , )/m	(8921, 1740, 0)
Target initial position (, , )/m	(10360, 0, 0)
Target velocity (,,), m/s	(10, 0, 0)
Terminal angular constraint ,	,
Terminal LOS angle rate (°/s)	0.2
Proportional coefficient of PNG,