Trajectory Optimization for High-Speed and Long-Range Interceptor Based on Improved Adaptive hp Pseudospectral Method

Figure 5

Programmed guidance stage trajectory optimization results.

(a) Trajectory of the missile

(b) Velocity vs. time

(c) Mass of missile

(d) Flight path angle and heading angle

(e) Control vs. time

(f) Process constraint

(g) Various grids of improved hp

(h) Various grids of hp