This paper derives predictive reduced-order models for rocket engine combustion dynamics via Operator Inference, a scientific machine learning approach that blends data-driven learning with physics-based modeling. The non-intrusive nature of the approach enables variable transformations that expose system structure. The specific contribution of this paper is to advance the formulation robustness and algorithmic scalability of the Operator Inference approach. Regularization is introduced to the formulation to avoid over-fitting. The task of determining an optimal regularization is posed as an optimization problem that balances training error and stability of long-time integration dynamics. A scalable algorithm and open-source implementation are presented, then demonstrated for a single-injector rocket combustion example. This example exhibits rich dynamics that are difficult to capture with state-of-the-art reduced models. With appropriate regularization and an informed selection of learning variables, the reduced-order models exhibit high accuracy in re-predicting the training regime and acceptable accuracy in predicting future dynamics, while achieving close to a million times speedup in computational cost. When compared to a state-of-the-art model reduction method, the Operator Inference models provide the same or better accuracy at approximately one thousandth of the computational cost.
翻译:本文通过运算符推断得出火箭发动机燃烧动态的预测减序模型,这是将数据驱动的学习与基于物理的模型相结合的一种科学机器学习方法。该方法的非侵入性性质使各种变异的变异能够暴露系统结构。本文件的具体贡献是推进操作员推算法的稳健性和算法缩缩缩性。为避免过度配置而引入了常规化。确定最佳正规化的任务是一个优化问题,它平衡了培训错误和长期集成动态的稳定性。介绍了可缩放算法和开源执行,然后演示了单一喷射器火箭燃烧实例。这个例子显示了难以用最先进的降级模型捕捉到的丰富动态。在适当规范化和知情选择学习变量的情况下,减序模型显示了重新定位培训制度和预测未来动态的可接受准确性方面的高度准确性,同时在计算成本上达到近100万倍的速率。与最先进的降低成本模型相比,操作员推断模型提供了大约一千倍的精确度。