Re, Fabrizio (2011) Modelica Landing Gear Modelling and On-Ground Trajectory Tracking with Sliding Mode Control. In: Advances in Aerospace Guidance, Navigation and Control Springer. pp. 103-115. ISBN 978-3-642-19816-8.
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A control system for an aircraft taxiing on ground based on sliding mode has been developed. The controller is capable of tracking the trajectory assigned in terms of longitudinal velocity and yaw rate and to drive an aircraft equipped with electric motors in the main gear as well as conventional brakes and nose gear steering. In addition, it can successfully handle saturation of the actuators. The algorithm is shown to be robust against parameter uncertainties (e.g. aircraft mass) as well as low friction coefficients at the interface tyre-ground. In order to test the tracking controller, an accurate virtual aircraft model has been designed in Modelica, with particular attention to the landing gears.
|Document Type:||Book Section|
|Title:||Modelica Landing Gear Modelling and On-Ground Trajectory Tracking with Sliding Mode Control|
|Journal or Publication Title:||Advances in Aerospace Guidance, Navigation and Control|
|In ISI Web of Science:||No|
|Page Range:||pp. 103-115|
|Keywords:||Modelica landing gear modelling, aircraft ground dynamics, sliding mode control|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Systems & Cabin|
|Institutes and Institutions:||Institute of Robotics and Mechatronics > System Dynamics and Control (former Control Design Engineering)|
|Deposited By:||Fabrizio Re|
|Deposited On:||06 May 2011 09:52|
|Last Modified:||30 Jan 2012 11:48|
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