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COMPACT AERO-THERMO MODEL BASED ENGINE MATERIAL TEMPERATURE CONTROL

机译:基于紧凑型航空热力学模型的发动机材料温度控制

摘要

Systems and methods for controlling a fluid based engineering system are disclosed. The systems and methods may include a model processor for generating a model output, the model processor including a set state module for setting dynamic states of the model processor, the dynamic states input to an open loop model based on the model operating mode. The model processor may further include an estimate state module for determining an estimated state of the model based on a prior state model output and the current state model of the open loop model the estimate state module using online linearization and gain calculation to determine estimator gain for determining the estimated state of the model.
机译:公开了用于控制基于流体的工程系统的系统和方法。该系统和方法可以包括用于生成模型输出的模型处理器,该模型处理器包括用于设置模型处理器的动态状态的设置状态模块,该动态状态基于模型操作模式输入到开环模型。模型处理器可以进一步包括估计状态模块,用于基于先前状态模型输出和开环模型的当前状态模型来确定模型的估计状态,该估计状态模块使用在线线性化和增益计算来确定用于确定模型的估计状态。

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