Research Article
Trajectory Optimization for High-Speed and Long-Range Interceptor Based on Improved Adaptive hp Pseudospectral Method
Figure 6
Midcourse 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 |