Research Article

Adaptive Neural Control of Hypersonic Vehicles with Actuator Constraints

Figure 3

Simulation result of Case 2.
(a) Velocity tracking
(b) Velocity tracking error
(c) The responses of flexible states
(d) Altitude tracking
(e) Altitude tracking error
(f) The responses of flexible states
(g) Flight-path angle
(h) Fuel equivalence ratio
(i) Elevator angular deflection