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).
| | Parameter | Value |
| | 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 , /° | , |
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