用量子算法提升飞机机身装配精度,减少实验次数。
Quantum Safe-Set Bayesian Optimization for Quality Improvement in Fuselage Assembly
- 结合量子奥数与贝叶斯优化,用更少查询获得精准环境响应
- 实验显示相同查询下误差和不确定性显著低于传统方法
- 适合追求高精度、低样本需求的智能制造场景
智能制造在飞机机身装配中通过创新的形状调整技术,有效减小了各段之间的尺寸间隙。现有方法虽有成效,但存在样本效率低的问题,源于经典蒙特卡洛方法在从分布中估计均值时的局限性。相比之下,量子算法可在相同精度下使用更少样本完成估计。受此启发,本文提出量子贝叶斯优化(QBO)框架,用于装配过程中的精确形状控制,以提升制造实践中的样本效率。该方法利用基于有限元分析(FEA)或代理模型的量子奥数,以较少查询获取更准确的环境响应。QBO采用上置信界(UCB)作为采集函数,策略性选择最可能最大化目标函数的输入值。理论上证明其可大幅减少样本量并保持相近优化效果。案例研究中,采用力控执行器调整一个机身段,以减小与邻接段的间隙。实验结果表明,相较于经典方法,QBO在相同仿真查询下实现了显著更低的尺寸误差与不确定性。
原文摘要 · Abstract (English)
Recent efforts in smart manufacturing have enhanced aerospace fuselage assembly processes, particularly by innovating shape adjustment techniques to minimize dimensional gaps between assembled sections. Existing approaches have shown promising results but face the issue of low sample efficiency from the manufacturing systems. It arises from the limitation of the classical Monte Carlo method when uncovering the mean response from a distribution. In contrast, recent work has shown that quantum algorithms can achieve the same level of estimation accuracy with significantly fewer samples than the classical Monte Carlo method from distributions. Therefore, we can adopt the estimation of the quantum algorithm to obtain the estimation from real physical systems (distributions). Motivated by this advantage, we propose a Quantum Bayesian Optimization (QBO) framework for precise shape control during assembly to improve the sample efficiency in manufacturing practice. Specifically, this approach utilizes a quantum oracle, based on finite element analysis (FEA)-based models or surrogate models, to acquire a more accurate estimation of the environment response with fewer queries for a certain input. QBO employs an Upper Confidence Bound (UCB) as the acquisition function to strategically select input values that are most likely to maximize the objective function. It has been theoretically proven to require much fewer samples while maintaining comparable optimization results. In the case study, force-controlled actuators are applied to one fuselage section to adjust its shape and reduce the gap to the adjoining section. Experimental results demonstrate that QBO achieves significantly lower dimensional error and uncertainty compared to classical methods, particularly using the same queries from the simulation.
Thank you to arXiv for use of its open access interoperability. PaperDance 不是 arXiv 官方产品;中文卡片由大模型生成,请以原文为准。