Wind field estimation for autonomous dynamic soaring

J. Langelaan, J. Spletzer, Corey Montella, J. Grenestedt
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引用次数: 53

Abstract

A method for distributed parameter estimation of a previously unknown wind field is described. The application is dynamic soaring for small unmanned air vehicles, which severely constrains available computing while simultaneously requiring updates that are fast compared with a typical dynamic soaring cycle. A polynomial parameterization of the wind field is used, allowing implementation of a linear Kalman filter for parameter estimation. Results of Monte Carlo simulations show the effectiveness of the approach. In addition, in-flight measurements of wind speeds are compared with data obtained from video tracking of balloon launches to assess the accuracy of wind field estimates obtained using commercial autopilot modules.
自主动力翱翔的风场估计
描述了一种未知风场的分布参数估计方法。该应用是小型无人飞行器的动态飙升,这严重限制了可用的计算,同时要求与典型的动态飙升周期相比,更新速度要快。使用了风场的多项式参数化,允许实现线性卡尔曼滤波器进行参数估计。蒙特卡罗仿真结果表明了该方法的有效性。此外,将飞行中的风速测量值与气球发射的视频跟踪数据进行比较,以评估使用商用自动驾驶模块获得的风场估计的准确性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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