Research Article
Trajectory Optimization for High-Speed and Long-Range Interceptor Based on Improved Adaptive hp Pseudospectral Method
Table 3
Terminal state of missile in the midcourse flight.
| Method | Terminal position (km) | Pitch angle (deg) | Yaw angle (deg) |
| Improved hp | (708.90, 27.47, 11.98) | 1.59 | -14.18 | hp | (708.85, 27.53, 12.18) | 1.55 | -14.05 |
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