Modeling of the Space Shuttle Main Engine Using Feed-forward Neural Networks

N. Saravanan, A. Duyar, T. Guo, W. C. Merrill
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引用次数: 16

Abstract

This paper presents the modeling of the Space Shuttle Main Engine (SSME) using a feed-forward neural network. The input and output data for modeling are obtained from a non-linear performance simulation developed by Rockwell International. The SSME is modeled as a system with two inputs and four outputs. The back-propagation algorithm is used to train the neural network by minimizing the squares of the residuals. The inputs to the network are the delayed values of the selected inputs and outputs of the non-linear simulation. The results obtained from the neural network model are compared with the results obtained from the non-linear simulation. It is shown that a single neural network can be used to model the dynamics of the space shuttle main engine. This neural network model can be used for control design purposes as well as for model-based fault detection studies.
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基于前馈神经网络的航天飞机主发动机建模
本文采用前馈神经网络对航天飞机主发动机(SSME)进行建模。建模的输入和输出数据来自罗克韦尔国际公司开发的非线性性能仿真。SSME被建模为具有两个输入和四个输出的系统。采用反向传播算法通过最小化残差的平方来训练神经网络。网络的输入是非线性仿真选择的输入和输出的延迟值。将神经网络模型得到的结果与非线性仿真结果进行了比较。结果表明,单个神经网络可以用于航天飞机主发动机的动力学建模。该神经网络模型既可用于控制设计,也可用于基于模型的故障检测研究。
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