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Model predictive quadrotor control: attitude, altitude and position experimental studies

机译:模型预测四旋翼控制:姿态,高度和位置实验研究

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摘要

This study addresses the control problem of an unmanned quadrotor in an indoor environment where there is lack of absolute localisation data. Based on an attached inertia measurement unit, a sonar and an optic-flow sensor, the state vector is estimated using sensor fusion algorithms. A novel switching model predictive controller is designed in order to achieve precise trajectory control, under the presence of forcible wind gusts. The quadrotor??s attitude, altitude and horizontal linearised dynamics result in a set of piecewise affine models, enabling the controller to account for a larger part of the quadrotor's flight envelope while modelling the effects of atmospheric disturbances as additive-affine terms in the system. The proposed controller algorithm accounts for the state and actuation constraints of the system. The controller is implemented on a quadrotor prototype in indoor position tracking, hovering and attitude manoeuvres experiments. The experimental results indicate the overall system??s efficiency in position/altitude/attitude set-point manoeuvres.
机译:这项研究解决了在缺乏绝对定位数据的室内环境中无人四旋翼飞机的控制问题。基于附加的惯性测量单元,声纳和光学流量传感器,使用传感器融合算法估算状态向量。设计了一种新颖的切换模型预测控制器,以便在强风的影响下实现精确的轨迹控制。四旋翼的姿态,高度和水平线性化动力学产生了一组分段仿射模型,使控制器能够在将大气扰动的影响建模为系统中的附加仿射项的同时考虑到四旋翼飞行包线的较大部分。所提出的控制器算法考虑了系统的状态和致动约束。该控制器在室内位置跟踪,悬停和姿态操纵实验的四旋翼原型机上实现。实验结果表明整个系统在位置/高度/姿态设定点操作中的效率。

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