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Integrated electro-hydraulic system modeling and analysis

机译:集成式电动液压系统建模与分析

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摘要

The technical approach for the development of the computer model of an integrated electro-hydraulic system is presented. As an example, the development of the computer model of the Space Shuttle Electric Auxiliary Power Unit (EAPU) is discussed. The integrated model consists of power source, electric power distribution and control (EPD&C), and mechanical and hydraulic loads. The modeling and analysis results, model interface issues, EPD&C interactions with the power sources, and EPD&C interaction with the electro-hydraulic load are discussed . The selected computer tool facilitates the development of "submodel" corresponding to the subsystem in the integrated system. This modeling approach and the models developed for EAPU can be generalized and adapted for the detailed modeling, simulation, and analysis of other aerospace and commercial electro-mechanical systems
机译:提出了开发集成式电动液压系统计算机模型的技术方法。例如,讨论了航天飞机电动辅助动力装置(EAPU)的计算机模型的开发。集成模型包括电源,配电和控制(EPD&C)以及机械和液压负载。讨论了建模和分析结果,模型接口问题,EPD&C与电源的相互作用以及EPD&C与电液负载的相互作用。所选计算机工具有助于开发与集成系统中的子系统相对应的“子模型”。可以推广这种建模方法和为EAPU开发的模型,并适用于其他航空航天和商用机电系统的详细建模,仿真和分析

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