International Journal of Aerospace Engineering / 2019 / Article / Fig 4

Research Article

Active Disturbance Rejection Control for Air-Breathing Hypersonic Vehicles Based on Prescribed Performance Function

Figure 4

Simulation results for Scenario 2.
(a) Velocity tracking performance
(b) Velocity tracking error
(c) Altitude tracking performance
(d) Altitude tracking error
(e) Flight-path angle
(f) Estimation of and
(g)
(h)
(i) Elastic state
(j) Elastic state
(k) Fuel equivalence ratio
(l) Elevator angular deflection

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