Mathematical Problems in Engineering / 2015 / Article / Fig 12

Research Article

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

Figure 12

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

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