Mathematical Problems in Engineering / 2015 / Article / Fig 11

Research Article

Continuous Recursive Sliding Mode Control for Hypersonic Flight Vehicle with Extended Disturbance Observer

Figure 11

Response for altitude command with disturbance.
(a) Velocity
(b) Altitude
(c) Angle of attack
(d) Flight path angle
(e) Elevator deflection angle
(f) Throttle setting

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