基于递归高斯过程自适应控制的机载风能系统闭环侧风飞行实时实验优化

Joe Deese, C. Vermillion
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引用次数: 2

摘要

机载风能(AWE)系统产生的功率可以通过在受控侧风飞行模式下移动系统而显着增加。本文采用基于递归高斯过程(RGP)的自适应控制,对AWE系统的侧风飞行模式进行了实时优化。基于rgp的自适应控制融合了机器学习工具和实时自适应控制原理。传统上,高斯过程(GP)建模需要一个包含所有先前测试过的数据点及其相关性能值的完整数据库。通过利用递归更新法则,这里使用的基于rgp的建模避免了维护完整数据库的需要。基于rgp的建模基于瞬时性能反馈在控制参数设计空间上估计预测均值和方差模型。候选设计空间通过在最大不确定性的位置选择点来探索。被确定为在统计上劣于感知最佳的设计点将从候选设计空间中被拒绝。在这项工作中,基于rgp的自适应应用于AWE系统实验侧风飞行的实验室规模平台。实验侧风飞行结果表明,与传统的固定飞行相比,功率增加了60%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Real-Time Experimental Optimization of Closed-Loop Crosswind Flight of Airborne Wind Energy Systems via Recursive Gaussian Process-based Adaptive Control
Power generated by airborne wind energy (AWE) systems can be dramatically increased by moving the system in controlled crosswind flight patterns. In this paper, the crosswind flight pattern of an AWE system is optimized in real time using recursive Gaussian process (RGP)-based adaptive control. RGP-based adaptive control fuses machine learning tools with real-time adaptive control principles. Traditionally, Gaussian process (GP) modeling requires a complete database of all the previously tested data points and their associated performance values. By utilizing a recursive update law, the RGP-based modeling used here avoids the need to maintain a complete database. The RGP-based modeling estimates a predictive mean and variance model over the control parameter design space based on instantaneous performance feedback. The candidate design space is explored by selecting points at locations of maximum uncertainty. Design points that are determined to be statistically inferior to the perceived optimum are rejected from the candidate design space. In this work, the RGP-based adaptation is applied to a lab-scale platform for experimental crosswind flight of AWE systems. Experimental crosswind flight results presented here demonstrate a 60% increase in power augmentation over traditional stationary flight.
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