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DEEP-LEARNING ALGORITHM-BASED SELF-ADAPTIVE CORRECTION METHOD FOR FULL-ENVELOPE MODEL OF AERO-ENGINE

机译:基于深度学习算法的航空发动机全包络模型自校正方法

摘要

A deep-learning algorithm-based self-adaptive correction method for a full-envelope model of an aero-engine, wherein same falls within the field of the modeling and simulation of aero-engines. A recurrent neural network-based dynamic parallel compensator is used to compensate for an original non-linear model error within a full-envelope range in a state where the performance of an aero-engine is not impaired; and at the same time, a genetic algorithm-based corrector is used to self-adaptively adjust a correction factor of a health parameter to be corrected in an original non-linear component-level model, wherein the health parameter to be corrected is determined by means of an integrated evaluation-based multi-index decision-making algorithm, and the sum of an output of the corrected non-linear component-level model and an output of the compensator is consistent with running trial output data of the aero-engine, thereby improving the full-envelope modeling precision of the aero-engine. By means of the method, strong support is provided for the design of an aero-engine control system and a fault diagnosis system, thereby facilitating the improvement of the reliability of aero-engine hardware in loop and semi-physical experiment verification.
机译:一种基于深度学习算法的航空发动机全包络模型自适应校正方法,该方法属于航空发动机建模与仿真领域。基于递归神经网络的动态并行补偿器用于在不损害航空发动机性能的状态下,在全包络范围内补偿原始非线性模型误差。同时,基于遗传算法的校正器用于自适应调整原始非线性分量级模型中待校正健康参数的校正因子,其中待校正健康参数由一种基于评估的综合多指标决策算法,校正后的非线性组件级模型的输出与补偿器的输出之和与航空发动机的运行试验输出数据一致,从而提高了航空发动机的全包络建模精度。通过该方法,为航空发动机控制系统和故障诊断系统的设计提供了有力的支持,从而有利于提高航空发动机硬件在回路和半物理实验验证中的可靠性。

著录项

  • 公开/公告号WO2019144337A1

    专利类型

  • 公开/公告日2019-08-01

    原文格式PDF

  • 申请/专利权人 DALIAN UNIVERSITY OF TECHNOLOGY;

    申请/专利号WO2018CN74084

  • 发明设计人 MA YANHUA;DU XIAN;SUN XIMING;

    申请日2018-01-25

  • 分类号G06F17/50;

  • 国家 WO

  • 入库时间 2022-08-21 11:53:47

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