Research Article
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 , /° | , |
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