2018
DOI: 10.1049/iet-cta.2017.0998
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Saturated adaptive sliding mode control for autonomous vessel landing of a quadrotor

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Cited by 42 publications
(28 citation statements)
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“…To achieve theV 3 negative definite, the control vector U 2 and the dynamics of ξ 2 are designed as (46) where k 5 , k 6 ∈ R + and ∆U 2 = sat(U 2 ) − U 2 . Assume that ∆U 2 satisfies ∆U 2 ≤ υ 2 with υ 2 ∈ R + .…”
Section: Robust Saturated Backstepping Tracking Controller Designmentioning
confidence: 99%
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“…To achieve theV 3 negative definite, the control vector U 2 and the dynamics of ξ 2 are designed as (46) where k 5 , k 6 ∈ R + and ∆U 2 = sat(U 2 ) − U 2 . Assume that ∆U 2 satisfies ∆U 2 ≤ υ 2 with υ 2 ∈ R + .…”
Section: Robust Saturated Backstepping Tracking Controller Designmentioning
confidence: 99%
“…Consider the quadrotor dynamics as described in Equation 2, for the given sufficiently smooth trajectory command P d and heading angle ψ d , if the controller gains k i (i = 1, ..., 6) and the observer bandwidth parameters ω 1 , ω 2 are chosen such that the matrix Π defined in the following is positive definite, then the ESO-based saturated trajectory tracking controller, including the virtual controllers (25), (33), (38), and (46) and the applied controllers (35) and (46), can guarantee the ultimate boundedness of all signals in the closed-loop and make the tracking errors arbitrarily small.…”
Section: Closed-loop System's Stability Analysismentioning
confidence: 99%
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