Supervised Energy Management in Advanced Aircraft Applications

A. Cavallo, Giacomo Canciello, A. Russo
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引用次数: 7

Abstract

A control strategy is proposed for energy management onboard the innovative More Electric Aircraft (MEA) concept. The objective is to reduce generator sizing (and weight onboard) by using battery packs as extra-energy sources. The flow of energy is regulated by a Buck-Boost Converter Unit (BBCU), suitably driven. The controller is composed of a two-layers architecture, where the bottom layer is devoted to current-tracking purposes, while the upper level takes care of the safe switching between the different control objectives. Rigorous stability tools are presented for both controllers, based on the Theory of Sliding Mode Control and of Common Lyapunov Functions. Detailed simulation with switching power electronic components show the effectiveness of the proposed approach.
先进飞机应用中的监督能源管理
提出了一种用于新型多电动飞机(MEA)能量管理的控制策略。目标是通过使用电池组作为额外的能源来减少发电机的尺寸(和重量)。能量流由Buck-Boost转换器单元(BBCU)调节,适当驱动。该控制器由两层结构组成,其中底层用于电流跟踪,而上层负责不同控制目标之间的安全切换。基于滑模控制理论和常用李雅普诺夫函数,给出了两种控制器的严格稳定性工具。对开关电力电子器件进行了详细的仿真,验证了该方法的有效性。
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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