2011
DOI: 10.1109/tac.2010.2081770
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Modular Adaptive Control of Uncertain Euler–Lagrange Systems With Additive Disturbances

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Cited by 83 publications
(42 citation statements)
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“…Inequality (27) shows V (t) V (0) in N 1 , hence, all the the signals e 1 , e 2 , ρ,Θ on the right-hand side of function (24) are bounded in N 1 . From the definition of e 1 , e 2 , ρ, Θ, we knowė 1 = e 2 − α 1 e 1 ,ė 2 = ρ − α 2 e 2 ,Θ = Θ −Θ, therefore, we can further getė 1 ,ė 2 ,Θ ∈ L ∞ in N 1 .…”
Section: Theoremmentioning
confidence: 98%
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“…Inequality (27) shows V (t) V (0) in N 1 , hence, all the the signals e 1 , e 2 , ρ,Θ on the right-hand side of function (24) are bounded in N 1 . From the definition of e 1 , e 2 , ρ, Θ, we knowė 1 = e 2 − α 1 e 1 ,ė 2 = ρ − α 2 e 2 ,Θ = Θ −Θ, therefore, we can further getė 1 ,ė 2 ,Θ ∈ L ∞ in N 1 .…”
Section: Theoremmentioning
confidence: 98%
“…To achieve the desired control objective, the following filtered tracking errors [25,27], denoted by e 2 , ρ ∈ R n−m , are defined as…”
Section: Error System Developmentmentioning
confidence: 99%
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“…The unknown disturbance represents unsteady nonlinear aerodynamic effects. A NN is used as a feedforward control term to compensate for the unknown nonlinear disturbance and a RISE feedback term [16][17][18] ensures asymptotic tracking of a desired state trajectory. A RISE-like controller was also recently developed in Ref.…”
Section: Introductionmentioning
confidence: 99%
“…A brief survey of nonlinear damping-based modular adaptive control results is provided in [7]. Another approach was investigated in [16] by designing a robust control law using the RISE (robust integral of the sign of the error [17]) feedback method, such that a generic form of an update law in terms of tracking errors could be used.…”
Section: Introductionmentioning
confidence: 99%