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A review of hybrid-electric energy management and its inclusion in vehicle sizing

机译:混合电能管理及其在车辆定型中的应用综述

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摘要

Purpose - The purpose of this study is to examine state-of-the-art in hybrid-electric propulsion system modeling and suggest new methodologies for sizing such advanced concepts. Many entities are involved in the modelling and design of hybrid electric aircraft; however, the highly multidisciplinary nature of the problem means that most tools focus heavily on one discipline and over simplify others to keep the analysis reasonable in scope. Correctly sizing a hybrid-electric system requires knowledge of aircraft and engine performance along with a working knowledge of electrical and energy storage systems. The difficulty is compounded by the multi-timescale dynamic nature of the problem. Furthermore, the choice of energy management in a hybrid electric system presents multiple degrees of freedom, which means the aircraft sizing problem now becomes not just a root-finding exercise, but also a constrained optimization problem. Design/methodology/approach - The hybrid electric vehicle sizing problem can be sub-divided into three areas: modelling methods/fidelity, energy management and optimization technique. The literature is reviewed to find desirable characteristics and features of each area. Subsequently, a new process for sizing a new hybrid electric aircraft is proposed by synthesizing techniques from model predictive control and detailed conceptual design modelling. Elements from model predictive control and concurrent optimization are combined to formulate a new structure for the optimization of the sizing and energy management of future aircraft. Findings - While the example optimization formulation provided is specific to a hybrid electric concept, the proposed structure is general enough to be adapted to any vehicle concept which contains multiple degrees of control freedom that can be optimized continuously throughout a mission. Originality/value - The proposed technique is novel in its application of model predictive control to the conceptual design phase.
机译:目的-这项研究的目的是研究混合动力推进系统建模的最新技术,并提出用于确定此类高级概念的新方法。许多实体都参与了混合动力飞机的建模和设计。但是,问题的高度多学科性质意味着大多数工具都将重点放在一个学科上,而过于简化了其他学科以使分析在范围上保持合理。正确确定混合动力系统的大小需要飞机和发动机性能的知识,以及电力和能量存储系统的工作知识。问题的多时标动态性质使问题更加复杂。此外,混合动力系统中能量管理的选择具有多个自由度,这意味着飞机的选型问题现在不仅变成了寻根工作,而且还成为约束性的优化问题。设计/方法/方法-混合动力电动汽车的尺寸问题可细分为三个领域:建模方法/保真度,能源管理和优化技术。查阅文献以找到每个区域的理想特性。随后,通过综合模型预测控制和详细概念设计建模技术,提出了一种确定新型混合动力飞机尺寸的新方法。来自模型预测控制和并行优化的元素被组合在一起,从而为优化未来飞机的尺寸和能量管理提供了一种新的结构。发现-尽管提供的示例性优化公式特定于混合动力概念,但所提出的结构具有足够的通用性,可适应任何包含多个控制自由度的车辆概念,并且可以在整个任务中对其进行连续优化。原创性/价值-所提出的技术在模型预测控制应用于概念设计阶段方面是新颖的。

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