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This article focuses on the nonlinear control issue of miniature Unmanned Aerial Vehicles(UAVs). A complete nonlinear model for miniature fixed-wing UAVs is structured and simplified as an affine nonlinear system aiming at the fast dynamic loop of key attitude control. We adopt the state feedback method to dynamic inversion controller design. To compensate the external disturbance and modeling error,...
This paper is concerned with the control of a class of continuous-time nonlinear dynamic systems preceded by unknown non-symmetrical, non-equal slope dead-zones. By exploring the properties of the dead-zone model intuitively and mathematically, an adaptive sliding mode inverse control scheme is developed by constructing a dead-zone inverse for compensation. The proposed approach ensures global stability...
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