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Development of a simulation platform of all-electric aircraft on-board systems for energy management studies

机译：开发用于能源管理研究的全电动飞机机载系统仿真平台

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This paper deals with the development of a simulation platform for the dynamic analysis of systems characterised by different physical domains. The research has been carried out\udin the context of the EC-funded Clean Sky Joint Technology Initiative (Green Regional Aircraft/All-Electric Aircraft domain). In particular, the objective of the research is focused\udon the on-board systems of new All-Electric Aircraft, where a crucial design point is related to the electrical energy management. In the “all-electric” concept, where pneumatic and\udhydraulic power systems are eliminated to improve aviation costs and environmental impact, the dynamics of electrical power absorptions is to be characterised and managed to avoid\udexcessive peaks with respect to generators capabilities. The paper describes the architecture of a Matlab/Simulink simulation platform developed in order to design and validate of the\udelectrical energy management logics, which lead up to 32% reduction of the maximum power request for the case study considered. Thanks to an approach based on a mixing of cosimulation\udand S-function compiling, the platform integrates models coming from different environments (AMESim, Dymola/Modelica), and developed by various partners/specialists.
机译：本文讨论了用于对具有不同物理域特征的系统进行动态分析的仿真平台的开发。该研究是在欧盟资助的“清洁天空联合技术计划”（绿色支线飞机/全电动飞机领域）的背景下进行的。特别地，研究的目标集中在新型全电动飞机的机载系统上，其中关键的设计点与电能管理有关。在“全电动”概念中，为了避免航空成本和环境影响，取消了气动和\ /液压动力系统，应对电功率吸收的动态进行表征和管理，以免在发电机性能方面出现\不必要的峰值。本文描述了为设计和验证电力电能管理逻辑而开发的Matlab / Simulink仿真平台的体系结构，对于所考虑的案例研究，该逻辑可将最大功率要求降低32％。由于采用了基于联合仿真\ ud和S函数编译的混合方法，该平台集成了来自不同环境（AMESim，Dymola / Modelica）的模型，并由各种合作伙伴/专家开发。

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