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

Table 1

Disturbance factors and their distribution.

Disturbance factor	Range	Distribution type	Unit
Muzzle velocity deviation	±2	Normal distribution	m/s
Initial flight path angle deviation	±0.3	Normal distribution	deg
Initial flight path deflection angle deviation	±0.3	Normal distribution	deg
Initial angular velocity	±0.5	Normal distribution	rad/s
Wind in direction	±5	Normal distribution	m/s
Time of boost deviation	±0.5	Normal distribution	s
Thrust deviation	±20	Normal distribution	N