多转子
控制理论(社会学)
有效载荷(计算)
职位(财务)
卡尔曼滤波器
估计员
计算机科学
扰动(地质)
控制工程
模型预测控制
工程类
控制(管理)
人工智能
航空航天工程
数学
古生物学
经济
网络数据包
财务
统计
生物
计算机网络
作者
Daniel Hentzen,Thomas Stastny,Roland Siegwart,Roland Brockers
标识
DOI:10.1109/iros40897.2019.8968471
摘要
Many multirotor Unmanned Aerial Systems applications have a critical need for precise position control in environments with strong dynamic external disturbances such as wind gusts or ground and wall effects. Moreover, to maximize flight time, small multirotor platforms have to operate within strict constraints on payload and thus computational performance. In this paper, we present the design and experimental comparison of Model Predictive and PID multirotor position controllers augmented with a disturbance estimator to reject strong wind gusts up to 12 m/s and ground effect. For disturbance estimation, we compare Extended and Unscented Kalman filtering. In extensive in- and outdoor flight tests, we evaluate the suitability of the developed control and estimation algorithms to run on a computationally constrained platform. This allows to draw a conclusion on whether potential performance improvements justify the increased computational complexity of MPC for multirotor position control and UKF for disturbance estimation.
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