Research Article

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

Table 6

Conditions for the simulations (fixed target).

ParameterValue

Missile midcourse navigation initial position (, , )/m(1000, 1000, 0)
Missile midcourse velocity (m/s)278
The end position of the midcourse guidance (, , )/m(7291, 687, 0)
Target position (, , )/m(8287, 0, 0)
Terminal angular constraint , ,