Proceedings of the 2000. IEEE International Conference on Control Applications. Conference Proceedings (Cat. No.00CH37162)
DOI: 10.1109/cca.2000.897513
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The control of the hovercraft system: a flatness based approach

Abstract: A simplified model of the hovercraft system, used in the literature to illustrate nonlinear control options in underactuated systems, is shown to be diflerentially flat. The flat outputs are given by the position coordinates with respect to the fixed earth frame. This fact is here exploited for the design of a dynamic feedback controller for the global asymptotic stabilization of the system's trajectory tracking error with respect to off-line planned position trajectories.

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Cited by 23 publications
(7 citation statements)
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“…This controller was validated experimentally on a robot called MVWT (the Caltech Multi-Vehicle Wireless Testbed) [10] and [5]. Other methods are used like in [17] where the flat property of the hovercraft model is proved. Nonetheless it appears that some singularities of the control law have to be avoided.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…This controller was validated experimentally on a robot called MVWT (the Caltech Multi-Vehicle Wireless Testbed) [10] and [5]. Other methods are used like in [17] where the flat property of the hovercraft model is proved. Nonetheless it appears that some singularities of the control law have to be avoided.…”
Section: Introductionmentioning
confidence: 99%
“…Based on this work, a robust second order sliding mode control is developed in [18]. Trajectory tracking for the terrestrial quadrotor detailed in [19] is made using the flat property of the system just like in [17].…”
Section: Introductionmentioning
confidence: 99%
“…The system model can be explicitly analyzed and designed using flatness property. 30 The flatness property was shown in many nonlinear systems: hovercrafts, 31 helicopters 32 and piezoelectric actuators. 33 Kim et al 28 proposed flatness-based nonlinear control for electro-hydraulic position servo system.…”
Section: Introductionmentioning
confidence: 99%
“…The controller is designed with expected state variables that are derived from system dynamics model. Controllers of many nonlinear systems were designed based on the flatness property: helicopters (Koo and Sastry, 1999), hovercrafts (Sira-Ramrez and Ibanez, 2000) and piezoelectric actuators (Rodriguez-Fortun et al, 2013). Electrohydraulic servo systems have also been shown to be flat (Kim et al, 2013).…”
Section: Introductionmentioning
confidence: 99%