Functional feedback in an extremum seeking loop

R. Banavar, D. Chichka, J. Speyer
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引用次数: 10

Abstract

We analyze the effect of functional feedback in an extremum seeking loop. Our study is motivated by a formation flight problem where the trailing aircraft experiences an outward rolling moment as the vortex effects of the leading aircraft come into play. Viewed as the extremized functional, this rolling moment feeds itself back to the lateral dynamics of the aircraft. In the initial half of the paper we impose restrictions on the curvature of the extremized functional and examine the effect under the assumption of a dynamic time-scale separation between the tracking loops of the linear dynamical system and the extremum seeking loop; in the latter half we remove both these assumptions and instead impose assumed functional forms on the extremized functional.
极值搜索回路中的功能反馈
分析了函数反馈在极值寻优回路中的作用。我们研究的动机是一个编队飞行问题,在这个问题中,随着领先飞机的旋涡效应的发挥,尾随飞机经历了一个向外滚动的力矩。作为一种极端的功能,这种滚动力矩反馈给飞机的横向动力学。在本文的前半部分中,我们对极值泛函的曲率施加了限制,并在线性动力系统的跟踪回路与极值寻求回路之间存在动态时标分离的假设下检验了这种影响;在后半部分,我们去掉了这两个假设,取而代之的是在极值泛函上施加假设的函数形式。
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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