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

Table 8

Conditions for the simulations (NSMG and BPN).

Parameter	Value
Missile position (, , ) (m)	(3000, 3500, −500)
Missile velocity (m/s)	370
The end position of the midcourse guidance (, , ) (m)	(8921, 1740, 0)
Target position (, , )/m	(10360, 0, 0)
Terminal LOS angle rate (°/s)	2
Terminal angular constraint , /°	,