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This paper presents the control of an electropneumatic system used for moving steering mechanism. This aeronautic application needs a high-precision position control and high bandwidth. The structure of the experimental setup and the benchmark on which controllers are evaluated have been designed in order to precisely check the use of such actuator in aeronautics. Two kinds of controllers are designed: a linear one based on gain scheduling feedback, and two high order sliding mode controllers ensuring finite-time convergence, high accuracy and robustness. Experimental results display feasibility and high performance of each controller and a comparison study is done. [ABSTRACT FROM AUTHOR]

This article deals with the well known problem of robust visual servoing (VS), which is formulated by the use of the general task function approach. Robustness is provided with respect to calibration parametric errors not only in terms of stability, but also in terms of tracking errors boundness. As a result, the proposed approach allows the user to choose a bound on the tracking error so as to guarantee the visibility of the target during the task execution. Most importantly, the error boundness is obtained while avoiding the use of large gains. Rather, one uses bounded gains, together with the modulation of the desired velocity along the desired path. An application of this general approach is developed and experimentally validated. [ABSTRACT FROM AUTHOR]