2007
DOI: 10.1109/tcst.2007.899718
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Stabilization of a PVTOL Aircraft and an Inertia Wheel Pendulum Using Saturation Technique

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Cited by 83 publications
(43 citation statements)
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“…6, pp. 1143-1150, Nov. 2007 A. Zavala-Rio, I. Fantoni, and R. Lozano, "Global stabilization of a PVTOL aircraft model with bounded inputs," Int. J.…”
Section: Referencesmentioning
confidence: 99%
“…6, pp. 1143-1150, Nov. 2007 A. Zavala-Rio, I. Fantoni, and R. Lozano, "Global stabilization of a PVTOL aircraft model with bounded inputs," Int. J.…”
Section: Referencesmentioning
confidence: 99%
“…Proposition 1 If H1) is satisfied, then there always exists a small parameter, such that control (5) stabilizes system (4).…”
Section: Partial Saturation Controlmentioning
confidence: 99%
“…Noticing that an ISS system possesses the "bounded input bounded state" property [10], and the (x 3 , x 4 ) subsystem is ISS with respect to the "input" −sat λ (x 2 ) − sat λ 2 (x 1 ), so x 3 and x 4 and in turn f i ( · ) (i = 1, 2) are bounded. Then, doing integral calculations in a bottom-up manner shows that the claim holds true.…”
Section: Partial Saturation Controlmentioning
confidence: 99%
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