基于DDIM混合加速采样的飞行器布局生成式设计方法

DDIM-based hybrid accelerated sampling method for generative design of aircraft configuration

  • 摘要: 针对基于点云扩散模型的飞行器三维气动布局设计中采样迭代次数多、计算耗时长的问题,本研究引入了去噪隐式扩散模型(DDIM, denoising diffusion implicit models)的快速采样方法,并进一步提出了“确定性-随机性”混合采样策略,不仅提升了生成效率,同时保证了生成质量与多学科设计约束的满足。该策略通过分析隐空间点云特征梯度的时间演化动态识别关键时间步,并利用分类器自适应调控不同关键性区域的噪声强度参数。实验结果表明:DDIM能显著加速采样,当采样步数从1000步缩减至50步时,生成耗时降低57.5%(30.32 s降至12.89 s),气动性能相对误差仅从3.62%增至8.52%;所提出的混合采样策略在50步条件下,生成耗时为13 s,生成多样性达标率为76.6%,气动性能误差<10%的达标率为73.3%,综合性能显著优于单一静态噪声强度采样。本研究为提高飞行器设计效率和降低设计成本奠定了基础。

     

    Abstract: Traditional aircraft configuration design faces significant efficiency challenges. This study addresses the critical bottleneck of slow sampling in point cloud diffusion models for generating 3D aerodynamic configuration under multidisciplinary constraints. We introduce the Denoising Diffusion Implicit Model (DDIM) acceleration strategy, leveraging its non-Markovian skip-step mechanism to drastically reduce the required sampling iterations without model retraining. To further optimize the balance between speed, accuracy, and diversity, we propose a novel "deterministic-stochastic" hybrid sampling strategy. This approach dynamically identifies critical timesteps by analyzing the temporal evolution of latent point cloud feature gradients and employs a trained classifier to adaptively modulate the noise strength parameter (η) across regions of varying criticality. Experimental validation demonstrates that DDIM achieves substantial acceleration: reducing steps from 1000 to 50 slashes generation time by 57.5% (from 30.32 s to 12.89 s) while only increasing the average aerodynamic performance relative error from 3.62% to 8.52% under fixed design conditions. Crucially, the hybrid strategy operating at 50 steps delivers generation within 13s, achieves a 76.6% satisfaction rate for Coverage (COV, Chamfer Distance) <10%, and attains a 73.3% satisfaction rate for aerodynamic performance error <10%, outperforming static noise sampling. This work successfully integrates DDIM acceleration with dynamic noise regulation into a point cloud diffusion framework for aircraft configuration generation, effectively overcoming the sampling efficiency hurdle and enabling the rapid production of diverse, constraint-satisfying designs. Future efforts will focus on automating the optimization of the classifier and noise control parameters.

     

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