Mathematical Problems in Engineering / 2015 / Article / Fig 10

Research Article

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

Figure 10

Response for velocity step 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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