New Design Method of Solid Propellant Grain Using Machine Learning

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초록

The correlation between solid propellant grain configuration and burning surface area profile is a complicated nonlinear problem. Nonlinear optimization has been adopted to design grain configurations that satisfied the objective area profiles. However, as conventional design methods are impractical, with limited performance, it is necessary to investigate alternatives. Useful information for grain design can be obtained by analyzing the aforementioned correlation. However, this aspect has not been studied owing to the requirement of large amounts of data and analysis techniques. In this study, machine learning was used to develop a new design method. The objective of machine learning was to train a model to classify classes of data. The database stores various sets of configuration variables and their classes. The proposed Gaussian kernel-based support vector machine model predicts the class of newly designed grains. The results verified that the model accurately predicted the class of the set of configuration variables and can be used to modify the set of configuration variables to satisfy the requirement. Thus, it was confirmed that machine learning is an appropriate approach to grain design; however, further research is needed to analyze its practicality.

키워드

solid rocket motorgrain designmachine learningsupport vector machineOPTIMIZATION
제목
New Design Method of Solid Propellant Grain Using Machine Learning
저자
Oh, Seok-HwanLee, Hyoung JinRoh, Tae-Seong
DOI
10.3390/pr9060910
발행일
2021-06
유형
Article
저널명
PROCESSES
9
6