Please use this identifier to cite or link to this item: http://dspace.univ-usto.dz/handle/123456789/211
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dc.contributor.authorLitim, Mustapha-
dc.contributor.authorA. Omari-
dc.date.accessioned2015-05-26T14:47:56Z-
dc.date.available2015-05-26T14:47:56Z-
dc.date.issued2015-05-26-
dc.identifier.urihttp://dspace.univ-usto.dz/handle/123456789/211-
dc.description.abstractThis paper presents a sliding mode control of a flight simulator Gough-Stewart type. The control is based on the inverse dynamic model of the robot in task space. Kinematic analysis is also discussed. High performance tracking control of a 6 DOF Stewart platform normally requires full knowledge of the system dynamics. In this paper, some important properties of the dynamics of the Stewart platform are considered to develop a sliding mode controller which can drive the upper platform angular and translation positions to the desired trajectories. Stability analysis based on Lyapunov theory is performed to ensure that the designed controller is stable. Numerical simulation is completed to show the effectiveness of the control system even in the case of large parameter variations.en_US
dc.language.isoenen_US
dc.publisherUniversity of sciences and technology in Oranen_US
dc.subjectFlight simulatoren_US
dc.subjectGough-Stewart platformen_US
dc.subjectsliding mode controlen_US
dc.subjectLyapunov stabilityen_US
dc.titleNonlinear Robust Sliding Mode Control of Flight Simulator (6-3) Gough-Stewart Type in Task spaceen_US
dc.typeArticleen_US
Appears in Collections:Thèses doctorat

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