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COMPACT AERO-THERMO MODEL BASED ENGINE MATERIAL TEMPERATURE CONTROL
COMPACT AERO-THERMO MODEL BASED ENGINE MATERIAL TEMPERATURE CONTROL
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机译:基于紧凑型航空热力学模型的发动机材料温度控制
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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.
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