1993 American Control Conference 1993
DOI: 10.23919/acc.1993.4793048
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Fuzzy Control of Wing Rock for Slender Delta wings

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Cited by 12 publications
(4 citation statements)
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“…For the demonstration, a wing-rock model for delta-wing aircraft is used (Tarn and Hsu, 1993). The continuous-time dynamics of the wing-rock model can be written as and Hsu, 1993), and therefore, the optimization variable space is U := U N . The horizon and time step are set as N = 5 and ∆t = 0.1s, respectively.…”
Section: Case 2: Learning-based Nonlinear Model Predictive Controlmentioning
confidence: 99%
“…For the demonstration, a wing-rock model for delta-wing aircraft is used (Tarn and Hsu, 1993). The continuous-time dynamics of the wing-rock model can be written as and Hsu, 1993), and therefore, the optimization variable space is U := U N . The horizon and time step are set as N = 5 and ∆t = 0.1s, respectively.…”
Section: Case 2: Learning-based Nonlinear Model Predictive Controlmentioning
confidence: 99%
“…The assumption of (S2) assures that the FLC represented by This assumption of (D2) is not heavily restrictive in that this skew symmetry can be found in the vast majority of FLC's proposed to date [6], [11], [16]- [19]. Especially, the fuzzy sliding mode controllers (FSMC) satisfy the above skew-symmetric condition [20]- [22] D3)…”
Section: For the Dynamic Casementioning
confidence: 99%
“…The plant to be controlled in this example is an Electrocraft Corporation E530 motor system governed by the following equation: (19) where the variables and the parameters are as follows:…”
Section: B Examplementioning
confidence: 99%
“…In Ref. [4], fuzzy logicbased roll controllers have been designed to control wingrock motion of a free-to-roll stinged delta wing. In Ref.…”
Section: Introductionmentioning
confidence: 99%