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Neural Network-Based Study on the Correlation between Exhaust Plume Images and Combustion Chamber Pressures of the Throttleable Hybrid Rocket Motor

机译:基于神经网络的排气羽状图像与舒适性混合火箭火箭电机的燃烧室压力相关性研究

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The relation between exhaust plume images and combustion chamber pressures of the throttleable hybrid rocket motor has not gained much attention. A neural network method is proposed to explore the correlation between exhaust plume images and combustion chamber pressures. Based on the idea of classification, we classified the combustion chamber pressures according to a piecewise function. The image of each frame of the input video was matched with each stage of the combustion chamber pressure to establish their corresponding relation with the machine learning method. In the training process, the pressure data were used as labels to match the corresponding exhaust plume images. In the testing process, after the input of the video, the combustion chamber pressures were automatically obtained according to the images. The results show that the exhaust plume images of different combustion chamber pressures present significant differences. Besides, with the images of exhaust plume as input, the test results of the neural network method show an 86.40% accuracy in the identification of the combustion chamber pressures.
机译:排气羽流图像与舒适的混合火箭火箭电机的燃烧室压力之间的关系并未获得很多关注。提出了一种神经网络方法来探讨排气羽图像与燃烧室压力之间的相关性。基于分类的思想,我们根据分段功能分类燃烧室压力。输入视频的每个帧的图像与燃烧室压力的每个级匹配,以与机器学习方法建立它们的对应关系。在训练过程中,压力数据用作标签以匹配相应的排气羽图像。在测试过程中,在输入视频之后,根据图像自动获得燃烧室压力。结果表明,不同燃烧室压力的排气羽状图像具有显着差异。此外,随着排气羽流的图像作为输入,神经网络方法的测试结果在识别燃烧室压力方面显示了86.40%的精度。

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