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