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MODEL-BASED AIRCRAFT BRAKE TEMPERATURE ESTIMATION

机译:基于模型的飞机制动温度估计

摘要

A method (200) for estimating the temperature of a component being monitored is described herein, comprising: inputting data (210) related to the component being monitored into a brake thermal model (215); using said brake thermal model (215) to predict a temperature (220) of the component based on said input data (210); inputting a) actual temperature sensor measurement data of said component and b) said predicted temperature (220) into an estimation algorithm, wherein said estimation algorithm (230) combines said a) actual temperature sensor data and b) predicted temperature and generates an estimated brake temperature of said component based on said combined inputs. A computer-implemented system is also described.
机译:本文描述了一种用于估计被监视的分量的温度的方法(200),包括:输入与被监视为制动热模型(215)的部件相关的数据(210); 使用所述制动热模型(215)来预测基于所述输入数据(210)的组件的温度(220); 将所述组件的实际温度传感器测量数据输入,B)所述预测温度(220)进入估计算法,其中所述估计算法(230)组合所述a)实际温度传感器数据和b)预测温度并产生估计的制动器 基于所述组合输入的所述组分的温度。 还描述了一种计算机实现的系统。

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