Research Article

Adaptive High Order Sliding Mode Controller Design for Hypersonic Vehicle with Flexible Body Dynamics

Figure 1

Vehicle states: (a) velocity change, (b) altitude change, (c) angle of attack, (d) velocity error information, (e) altitude error information, and (f) flight path angle.
357685.fig.001a
(a)
357685.fig.001b
(b)
357685.fig.001c
(c)
357685.fig.001d
(d)
357685.fig.001e
(e)
357685.fig.001f
(f)