A Rapid Penetration Trajectory Optimization Method for Hypersonic Vehicles

Table 4

Miss distances in the two scenarios of the terminal maximum overload maneuver or no maneuver.

Penetration angle	Miss distance (no maneuver)	Miss distance (maneuver)
10	0.15	0.26
15	0.30	0.78
20	2.89	74.36
25	253.25	757.9
30	1705.34	1827.27