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Zhang H R, Wang Y, Hong D P. Research advances in Uncertainty Quantification and Design Optimization for Flight Vehicles. Advances in Mechanics, in press doi: 10.6052/1000-0992-25-032
Citation: Zhang H R, Wang Y, Hong D P. Research advances in Uncertainty Quantification and Design Optimization for Flight Vehicles. Advances in Mechanics, in press doi: 10.6052/1000-0992-25-032

Research advances in Uncertainty Quantification and Design Optimization for Flight Vehicles

doi: 10.6052/1000-0992-25-032 cstr: 32046.14.1000-0992-25-032
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  • Corresponding author: hloving@163.com
  • Received Date: 2026-01-02
  • Accepted Date: 2026-03-04
  • Available Online: 2026-05-06
  • Uncertainty Quantification (UQ) and Uncertainty-Based Design Optimization (UBDO), as an emerging design paradigm for flight vehicles, provides a systematic methodological framework for addressing the precise characterization, propagation, and design optimization of uncertainties. This paper reviews the core concepts and key technologies in this field. It summarizes the uncertainty challenges associated with critical systems and significant environmental conditions of flight vehicles. Based on the latest research progress, five key research directions are identified: (1) High-dimensional uncertainty quantification and efficient propagation: Constructing an adaptive high-dimensional UQ framework by integrating techniques such as dimensionality reduction, compressed sensing, and low-rank tensor decomposition to effectively address the "curse of dimensionality." (2) Hybrid uncertainty quantification and efficient propagation: A unified framework is established to accommodate various types of uncertainties—including probabilistic, interval, fuzzy, and evidence theory. The computational efficiency for complex, multi-source uncertainty problems is further enhanced by incorporating surrogate modeling and active learning strategies. (3) Multi-level and multi-fidelity UQ framework: Achieving dynamic and optimal allocation of computational resources across models of varying fidelities by integrating techniques like generalized approximate control variates and adaptive multi-index stochastic collocation. (4) Uncertainty-based design optimization algorithms and frameworks: Unifying probabilistic constraints and robustness metrics within a multi-objective optimization and decision-making framework under uncertainty, enabling trade-off optimization among performance, reliability, and robustness through single-loop and decoupled optimization strategies. (5) Uncertainty design and analysis based on artificial intelligence techniques: Centered on physics-informed neural networks, this direction incorporates physical knowledge and multi-source data to establish intelligent frameworks for uncertainty quantification and optimization.

     

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  • [1]
    陈鑫, 王刚, 叶正寅, 等. 2021. CFD不确定度量化方法研究综述. 空气动力学学报, 39(4): 1-13 (Chen X, Wang G, Ye Z Y, et al. 2021. A review of uncertainty quantification methods for Computational Fluid Dynamics. Acta Aerodynamica Sinica, 39(4): 1-13). doi: 10.7638/kqdlxxb-2021.0012

    Chen X, Wang G, Ye Z Y, et al. 2021. A review of uncertainty quantification methods for Computational Fluid Dynamics. Acta Aerodynamica Sinica, 39(4): 1-13 doi: 10.7638/kqdlxxb-2021.0012
    [2]
    陈小前, 姚雯, 欧阳琦. 2013. 飞行器不确定性多学科设计优化理论与应用. 科学出版社.
    [3]
    郭雷, 李文硕, 崔洋洋等. 2025. 动态闭环不确定性量化理论与智能无人系统应用. 中国科学: 技术科学, 55(1): 1-13 (Guo L, Li W S, Cui Y Y, et al. 2025. Dynamic closed-loop uncertainty quantification theory with intelligent unmanned systems applications. SCIENTIA SINICA Technologica, 55(1): 1-13). doi: 10.1360/SST-2024-0155

    Guo L, Li W S, Cui Y Y, et al. 2025. Dynamic closed-loop uncertainty quantification theory with intelligent unmanned systems applications. SCIENTIA SINICA Technologica, 55(1): 1-13. doi: 10.1360/SST-2024-0155
    [4]
    郭书祥, 吕震宙, 冯元生. 2001. 基于区间分析的结构非概率可靠性模型. 计算力学学报, 18(1): 56-60 (Guo S X, Lu Z Z, Feng Y S. 2001. A non-probabilistic model of structural reliability based on interval analysis. Chinese Journal of Computational Mechanics, 18(1): 56-60).

    Guo S X, Lu Z Z, Feng Y S. 2001. A non-probabilistic model of structural reliability based on interval analysis. Chinese Journal of Computational Mechanics, 18(1): 56-60.
    [5]
    何佳乐, 王玉惠, 张浩迪. 2023. 高超声速飞行器的非概率可靠性分析. 哈尔滨工业大学学报, 55(12): 1-8 (He J L, Wang Y H, Zhang H D. 2023. Non-probabilistic reliability analysis of hypersonic vehicle. Journal of Harbin Institute of Technology, 55(12): 1-8).

    He J L, Wang Y H, Zhang H D. 2023. Non-probabilistic reliability analysis of hypersonic vehicle. Journal of Harbin Institute of Technology, 55(12): 1-8.
    [6]
    刘继红, 李连升. 2018. 考虑多源不确定性的多学科可靠性设计优化. 华中科技大学出版社.
    [7]
    李阳天, 李海滨, 韦广梅, 等. 2020. 基于改进型多项式混沌展开的固体火箭发动机药柱低温点火不确定性量化分析. 兵工学报, 41(1): 40-48 (Li Y T, Li H B, Wei G M, et al. 2020. Uncertainty quantification analysis of solid rocket motor grain ignition at low temperature based on improved polynomial chaos expansion. Acta Armamentarii, 41(1): 40-48).

    Li Y T, Li H B, Wei G M, et al. 2020. Uncertainty quantification analysis of solid rocket motor grain ignition at low temperature based on improved polynomial chaos expansion. Acta Armamentarii, 41(1): 40-48.
    [8]
    聂兆伟, 王浩, 秦梦, 等. 2021. 高维不确定性条件下飞行器级间分离可靠性评估. 宇航学报, 42(12): 1525-1531 (Nie Z W, Wang H, Qin M, et al. 2021. Reliability assessment of flight vehicle stage separation considering high-dimensional uncertainties. Journal of Astronautics, 42(12): 1525-1531).

    Nie Z W, Wang H, Qin M, et al. 2021. Reliability assessment of flight vehicle stage separation considering high-dimensional uncertainties. Journal of Astronautics, 42(12): 1525-1531.
    [9]
    聂兆伟, 王浩, 秦梦, 等. 2022. 混合不确定条件下的飞行器级间分离可靠性分析. 国防科技大学学报, 44(3): 104-111 (Nie Z W, Wang H, Qin M, et al. 2022. Reliability analysis of flight vehicle stage separation under mixed uncertainties. Journal of National University of Defense Technology, 44(3): 104-111).

    Nie Z W, Wang H, Qin M, et al. 2022. Reliability analysis of flight vehicle stage separation under mixed uncertainties. Journal of National University of Defense Technology, 44(3): 104-111.
    [10]
    庞煜, 黄洪钟, 刘宇, 等. 2013. 多状态系统的可能可靠性分析. 西安交通大学学报, 47(3): 75-79 (Possibility theory based multi-state system reliability analysis. Journal of Xian Jiaotong University, 47(3): 75-79).

    Possibility theory based multi-state system reliability analysis. Journal of Xian Jiaotong University, 47(3): 75-79.
    [11]
    邱宇, 邱志平. 2023. 考虑多维相关性的飞行器结构载荷不确定性分析. 空天技术, 4: 66-74 (Qiu Y, Qiu Z P. 2023. Uncertainty analysis of aircraft structures load considering multi-dimensional correlation. Aerospace Technology, 4: 66-74).

    Qiu Y, Qiu Z P. 2023. Uncertainty analysis of aircraft structures load considering multi-dimensional correlation. Aerospace Technology, 4: 66-74.
    [12]
    邱志平, 胡永明. 2016. 椭球凸模型非概率可靠性度量和区间安全系数的关系. 计算力学学报, 33(4): 522-527 (Qiu Z P, Hu Y M. 2016. The relations of non-probabilistic reliability measures based on ellipsoidal convex model and interval safety factors. Chinese Journal of Computational Mechanics, 33(4): 522-527).

    Qiu Z P, Hu Y M. 2016. The relations of non-probabilistic reliability measures based on ellipsoidal convex model and interval safety factors. Chinese Journal of Computational Mechanics, 33(4): 522-527.
    [13]
    孙冲, 方群, 袁建平. 2012. 具有模型参数不确定性的高超声速飞行器动态特性分析及控制律设计. 西北工业大学学报, 30(4): 497-502 (Sun C, Fang Q, Yuan J P. 2012. A useful dynamic analysis of hypersonic vehicle and control law design using uncertainty parameter dynamics model. Journal of Northwestern Polytechnical University, 30(4): 497-502). doi: 10.3969/j.issn.1000-2758.2012.04.004

    Sun C, Fang Q, Yuan J P. 2012. A useful dynamic analysis of hypersonic vehicle and control law design using uncertainty parameter dynamics model. Journal of Northwestern Polytechnical University, 30(4): 497-502. doi: 10.3969/j.issn.1000-2758.2012.04.004
    [14]
    唐樟春, 吕震宙, 吕媛波. 2011. 随机变量概率信息不充分时的可靠性新模型. 工程力学, 28(4): 18-22 (Tang Z C, Lu Z Z, Lu Y B. 2011. A novel reliability model for random variables lacking sufficient probability information. Engineering Mechanics, 28(4): 18-22).

    Tang Z C, Lu Z Z, Lu Y B. 2011. A novel reliability model for random variables lacking sufficient probability information. Engineering Mechanics, 28(4): 18-22.
    [15]
    王攀, 吕震宙, 唐樟春. 2012. 模糊分布参数条件下结构系统的近似效应分析. 力学学报, 44(3): 546-556 (Wang P, Lu Z Z, Tang Z C. 2012. An approximate effect analysis of structural system with fuzzy distribution parameters. Chinese Journal of Theoretical and Applied Mechanics, 44(3): 546-556).

    Wang P, Lu Z Z, Tang Z C. 2012. An approximate effect analysis of structural system with fuzzy distribution parameters. Chinese Journal of Theoretical and Applied Mechanics, 44(3): 546-556.
    [16]
    熊芬芬, 杨树兴, 刘宇, 等. 2015. 工程概率不确定性分析方法. 科学出版社.
    [17]
    张海瑞, 王浩, 王尧, 等. 2019. 基于不确定性的飞行器分离可靠性建模与分析方法. 宇航学报, 40(4): 378-385 (Zhang H R, Wang H, Wang Y. 2019. Uncertainty-based reliability modeling and analysis method of flight vehicle separation. Journal of Astronautics, 40(4): 378-385).

    Zhang H R, Wang H, Wang Y. 2019. Uncertainty-based reliability modeling and analysis method of flight vehicle separation. Journal of Astronautics, 40(4): 378-385.
    [18]
    张海瑞. 2022. 飞行器总体不确定性分析与优化设计. 中国宇航出版社.
    [19]
    张涵信. 2008. 关于CFD计算结果的不确定度问题. 空气动力学学报, 26(1): 47-49 (Zhang H X. 2008. On the uncertainty about CFD results. Acta Aerodynamica Sinica, 26(1): 47-49).

    Zhang H X. 2008. On the uncertainty about CFD results. Acta Aerodynamica Sinica, 26(1): 47-49.
    [20]
    张涵信, 查俊. 2010. 关于CFD验证确认中的不确定度和真值估算. 空气动力学学报, 28(1): 39-45 (Zhang H X, Zha J. 2010. The uncertainty and truth-value assessment in the verification and validation of CFD. Acta Aerodynamica Sinica, 28(1): 39-45).

    Zhang H X, Zha J. 2010. The uncertainty and truth-value assessment in the verification and validation of CFD. Acta Aerodynamica Sinica, 28(1): 39-45
    [21]
    郑伶华, 陈强, 李彦斌, 等. 2023. 动态大气环境下高速飞行器气动噪声不确定性量化研究. 振动与冲击, 42(14): 306-313 (Zheng L H, Chen Q, Li Y B, et al. 2023. Uncertainty quantification for the aerodynamic noise of high-speed aircrafts in dynamic atmospheric environment. Journal of Vibration and Shock, 42(14): 306-313). doi: 10.13465/j.cnki.jvs.2023.14.036

    Zheng L H, Chen Q, Li Y B, et al. 2023. Uncertainty quantification for the aerodynamic noise of high-speed aircrafts in dynamic atmospheric environment. Journal of Vibration and Shock, 42(14): 306-313 doi: 10.13465/j.cnki.jvs.2023.14.036
    [22]
    张伟伟, 邬晓敬, 宋述芳. 2020. 气动外形优化设计中的不确定性及高维问题研究. 西北工业大学出版社.
    [23]
    Airbus Group Innovations. 2016. Current engineering practices in UQ&M in aeronautics and associated challenges.
    [24]
    Alonso J J, Fenrich R W, Menier V, et al. 2017. Scalable environment for quantification of uncertainty and optimization in industrial applications (SEQUOIA). AIAA SciTech 2017 Forum, 9-13 January 2017, Grapevine, USA.
    [25]
    Azarhoosh Z, Ilchi Ghazaan M. 2025. A review of recent advances in surrogate models for uncertainty quantification of high-dimensional engineering applications. Computer Methods in Applied Mechanics and Engineering, 433: 117508. doi: 10.1016/j.cma.2024.117508
    [26]
    Bichon B J, Eldred M S, Swiler L P, et al. 2008. Efficient global reliability analysis for nonlinear implicit performance functions. AIAA Journal, 46(10): 2459-2468. doi: 10.2514/1.34321
    [27]
    Beyer H G, Sendhoff B. 2007. Robust optimization-A comprehensive survey. Computer Methods in Applied Mechanics and Engineering, 196: 3190-3218. doi: 10.1016/j.cma.2007.03.003
    [28]
    Ben-Haim, Y. 1994. A non-probabilistic concept of reliability. Structural Safety, 14(4): 227-245. doi: 10.1016/0167-4730(94)90013-2
    [29]
    Cary A W, Schaefer J A, Duque E P N, et al. 2024. Overview of fluid dynamics uncertainty quantification challenge problem and results. AIAA SciTech 2024 Forum. 8-12 January 2024, Orlando, USA.
    [30]
    Chatterjee T, Chakraborty S, Chowdhury R. 2019. A critical review of surrogate assisted robust design optimization. Archives of Computational Methods in Engineering, 26: 245-274. doi: 10.1007/s11831-017-9240-5
    [31]
    Chen X, Zhou W, et al. 2020. The heat source layout optimization using deep learning surrogate modeling. Structural and Multidisciplinary Optimization, 62: 3127-3148. doi: 10.1007/s00158-020-02659-4
    [32]
    Chen X, Zhao X, Gong Z, et al. 2021. A deep neural network surrogate modeling benchmark for temperature field prediction of heat source layout. Science China Physics, Mechanics & Astronomy, 11: 78–107.
    [33]
    Dellino G, Meloni C. 2015. Uncertainty management in simulation-optimization of complex systems: algorithms and applications. Springer.
    [34]
    Duraisamy K, Iaccarino G, Xiao H. 2019. Turbulence modeling in the age of data. Annual Review of Fluid Mechanics, 51: 1-23.
    [35]
    DiGregorio N J, Wright A H. 2024. Efficient global optimization with gradient finish for design under uncertainty. AIAA SciTech 2024 Forum. 8-12 January 2024, Orlando, USA.
    [36]
    Dolgov S, Scheichl R. 2017. A hybrid alternating least squares-TT cross algorithm for parametric PDEs. SIAM/ASA Journal on Uncertainty Quantification, 7(1): 1-29. doi: 10.1137/17m1138881
    [37]
    Du X. 2008. Unified uncertainty analysis by the first order reliability method. Journal of Mechanical Design, 130: 091401. doi: 10.1115/1.2943295
    [38]
    Echard B, Gayton N, Lemaire M, et al. 2013. A combined importance sampling and kriging reliability method for small failure probabilities with time-demanding numerical models. Reliability Engineering & System Safety, 111: 232-240. doi: 10.1016/j.ress.2012.10.008
    [39]
    Elishakoff I, Colombi P. 1993. Combination of probabilistic and convex models of uncertainty when scarce knowledge is present on acoustic excitation parameters. Computer Methods in Applied Mechanics and Engineering, 104: 187-209. doi: 10.1016/0045-7825(93)90197-6
    [40]
    Francom D, Nachtsheim A. 2025. A review and comparison of different sensitivity analysis techniques in practice. arXiv preprint arXiv: 2506.11471v1 [stat. ME].
    [41]
    Gorodetsky A A, Geraci G, Eldred M S, et al. 2020. A generalized approximate control variate framework for multifidelity uncertainty quantification. Journal of Computational Physics, 408: 1-29. doi: 10.1016/j.jcp.2020.109257
    [42]
    Geraci G, Eldred M S, Gorodetsky A A, et al. 2018. Leveraging active direction for efficient multifidelity uncertainty quantification. 7th European Conference of Computational Fluid Dynamics, 11-15 June 2018, Glasgow, UK.
    [43]
    Geraci G, Eldred M S, Gorodetsky A A, et al. 2019. Recent advancements in Multilevel-Multifidelity techniques for forward UQ in the DARPA SEQUOIA project. AIAA Scitech 2019 Forum, 7-11 January 2019, San Diego, USA.
    [44]
    Geraci G, Menhorn F, Huan X, et al. 2019. Progress in scramjet design optimization under uncertainty using simulations of the HIFiRE direct connect rig. AIAA SciTech 2019 Forum, 7-11 January 2019, San Diego, USA.
    [45]
    Guo W L, Xu Y, Liu Q, et al. 2024. Reliability of hypersonic airfoil with freeplay and stochasticity via nonlinear energy sink. AIAA Journal, 62(9): 3258-3270. doi: 10.2514/1.J064048
    [46]
    Guo W L, Xu Y, Li Y G, et al. 2023. Dynamic responses of a conceptual two-dimensional airfoil in hypersonic flows with random perturbations. Journal of Fluids and Structures, 121: 103920. doi: 10.1016/j.jfluidstructs.2023.103920
    [47]
    Hirsch C, Wunsch D, Szumbarski J, et al. 2019. Uncertainty management for robust industrial design in aeronautics. Cham: Springer.
    [48]
    Hubbard E, Stephens J. 2017. Facility Measurement Uncertainty Analysis at NASA GRC. Supersonic Tunnel Association International (STAI) Meeting. NASA Report Number: GRC-E-DAA-TN31803.
    [49]
    Hu H D, Song Y P, Yu J Y, et al. 2024. Investigation on uncertainty quantification of transonic airfoil using compressive sensing greedy reconstruction algorithms. Aerospace Science and Technology, 147: 109000. doi: 10.1016/j.ast.2024.109000
    [50]
    Hu W, Cheng S, Yan J, et al. 2024. Reliability-based design optimization: a state-of-the-art review of its methodologies, applications, and challenges. Structural and Multidisciplinary Optimization, 67: 168. doi: 10.1007/s00158-024-03884-x
    [51]
    Huan X, Safta C, Vane Z P, et al. 2019. Uncertainty propagation using conditional random fields in large-eddy simulations of scramjet computations. AIAA SciTech 2019 Forum, 7-11 January 2019, San Diego, USA.
    [52]
    Iyengar N, Mavris D. 2023. High-dimensional uncertainty propagation in aerodynamics using polynomial chaos-Kriging. AIAA Aviation 2023 Forum, 12-16 June 2023, San Diego, CA.
    [53]
    Jiang C, Zheng J, Han X. 2017. Probability-interval hybrid uncertainty analysis for structures with both aleatory and epistemic uncertainties: a review. Structural and Multidisciplinary Optimization, 57: 2485-2502. doi: 10.1007/s00158-017-1864-4
    [54]
    Jakeman J D, Eldred M S, Geraci G, et al. 2020. Adaptive multi-index collocation for uncertainty quantification and sensitivity analysis. International Journal for Numerical Methods in Engineering, 121: 4471-4472. doi: 10.1002/nme.6450
    [55]
    Liu J X, Shi Y, Ding C, et al. 2024. Hybrid uncertainty propagation based on multi-fidelity surrogate model. Computers & Structures, 293: 107267. doi: 10.1016/j.compstruc.2023.107267
    [56]
    Lu Q H, Wang L, Li L S. 2022. Efficient uncertainty quantification of stochastic problems in CFD by combination of compressed sensing and POD-Kriging. Computer Methods in Applied Mechanics and Engineering, 396: 115118. doi: 10.1016/j.cma.2022.115118
    [57]
    Long X Y, Mao D L, Jiang C, et al. 2023. Unified uncertainty analysis under probability, evidence, fuzzy and interval uncertainties. Computer Methods in Applied Mechanics and Engineering, 355: 1-26. doi: 10.1007/978-981-19-9398-5_23
    [58]
    Liu Y S, Li L Y, Zhao S H, et al. 2021. A global surrogate model technique based on principal component analysis and Kriging for uncertainty propagation of dynamic systems. Reliability Engineering & System Safety, 207: 107365. doi: 10.1016/j.ress.2020.107365
    [59]
    Ma J Z, Li D Y, Wang R F, et al. 2025. Predicting tipping phenomenon in a conceptual airfoil structure under extreme flight environment. Journal of Sound and Vibration, 618: 119306. doi: 10.1016/j.jsv.2025.119306
    [60]
    Michek N E, Mehta P, Huebsch W W. 2024. Flight dynamic uncertainty quantification modeling using physics-informed neural networks. AIAA SciTech 2024 Forum. 8-12 January 2024, Orlando, USA.
    [61]
    Ma S J, Xu Y. 2025. Complex dynamics of a conceptual airfoil structure excited by the long-range correlation random load. The European Physical Journal Special Topics, 2025: 1-15. doi: 10.1140/epjs/s11734-025-02038-4
    [62]
    Meng Z, Zhao J Y, Chen G H, et al. 2022. Hybrid uncertainty propagation and reliability analysis using direct probability integral method and exponential convex model. Reliability Engineering and System Safety, 228: 108803. doi: 10.1016/j.ress.2022.108803
    [63]
    Navaneeth N, Chakraborty S. 2022. Surrogate assisted active subspace and active subspace assisted surrogate—A new paradigm for high dimensional structural reliability analysis. Computer Methods in Applied Mechanics and Engineering, 389: 114374. doi: 10.1016/j.cma.2021.114374
    [64]
    Oseledets I, Tyrtyshnikov E. 2010. TT-cross approximation for multidimensional arrays. Linear Algebra and its Applications, 432: 70-88. doi: 10.1016/j.laa.2009.07.024
    [65]
    Paudel A, Thapa M, Gupta S, et al. 2025. Polynomial chaos with modified Tikhonov regularization for uncertainty quantification. AIAA SciTech 2025 Forum. 6-10 January 2025, Orlando, USA.
    [66]
    Peherstorfer B, Willcox K, Gunzburger M. 2018. Survey of multifidelity methods in uncertainty propagation, inference, and optimization. SIAM Review, 60(3): 550-591. doi: 10.1137/16M1082469
    [67]
    Phillips B D, Schmidt J, Falck R D, et al. 2024. End-to-end uncertainty quantification with analytical derivatives for design under uncertainty. AIAA SciTech 2024 Forum. 8-12 January 2024, Orlando, USA.
    [68]
    Pereira D, Afonso F, Lau F. 2025. End-to-end deep-learning-based surrogate modeling for supersonic airfoil shape optimization. Aerospace, 12: 1-22. doi: 10.3390/aerospace12050389
    [69]
    Peng W, Zhang J, Zhou W, et al. 2021. IDRLnet: A physics-informed neural network library. arXiv preprint arXiv: 2107.04320v1.
    [70]
    Romeo S A S, Oz F, Kassem A, et al. 2024. Physics informed data fusion model for uncertainty quantification in atmospheric entry vehicle dynamic stability. AIAA Aviation Forum and Ascend 2024, 29 July-2 August 2024, Las Vegas, USA
    [71]
    Stephens J, Hubbard E, Walter J A, et al. 2016. Uncertainty Analysis of NASA Glenn's 8- by 6-Foot Supersonic Wind Tunnel. SciTech Meeting. San Diego, CA.
    [72]
    Slotnick J, Khodadoust A, Alonso J, et al. 2014. CFD vision 2030 study: a path to revolutionary computational aerosciences. No. NASA/CR-2014-218178.
    [73]
    Schaefer J A, Cary A W, Khurana M S. 2024. Surrogate model and discretization error impacts on the fluid dynamics uncertainty quantification challenge problem. AIAA SciTech 2024 Forum. 8-12 January 2024, Orlando, USA.
    [74]
    Sun J L, Zheng X H, Yao W, et al. 2025. Heat source layout optimization using automatic deep learning surrogate and multimodal neighborhood search algorithm. Annals of Operations Research, 348: 345-371. doi: 10.1007/s10479-023-05262-0
    [75]
    Schmidt J N, Phillips B D, Falck R D, et al. 2025. Design under uncertainty with design-dependent uncertain variables. AIAA SciTech 2025 Forum. 6-10 January 2025, Orlando, USA.
    [76]
    Shubham S, Kipouros T, Dash S, et al. 2024. Uncertainty propagation and management of mixed uncertainties for multi-fidelity multi-disciplinary analysis of propeller with different blade sweep. AIAA SciTech 2024 Forum. 8-12 January 2024, Orlando, USA.
    [77]
    Wong B Y J, Damodaran M, Khoo B C. 2024. Physics-informed machine learning using low-fidelity flowfields for inverse airfoil shape design. AIAA Journal, 62(8): 2846-2861 doi: 10.2514/1.j063570
    [78]
    Wang C, Fan H, Qiang X. 2023. A review of uncertainty-based multidisciplinary design optimization methods based on intelligent strategies. Symmetry, 15: 1875. doi: 10.3390/sym15101875
    [79]
    Wang C, Matthies H G. 2020. Random model with fuzzy distribution parameters for hybrid uncertainty propagation in engineering systems. Computer Methods in Applied Mechanics and Engineering, 1: 112673. doi: 10.1016/j.cma.2019.112673
    [80]
    Wang L, Liu Y R, Xu H Y. 2021. Review: Recent developments in dynamic load identification for aerospace vehicles considering multi-source uncertainties. Transactions of Nanjing University of Aeronautics and Astronautics, 38(2): 271-287.
    [81]
    Wang Z F, Wang L Q, Wang X Y, et al. 2023. Propagation algorithm for hybrid uncertainty parameters based on polynomial chaos expansion. International Journal for Numerical Methods in Engineering, 124: 4203-4223. doi: 10.1002/nme.7307
    [82]
    Xu Y, Yao W, Zheng X, et al. 2025. A generic quality and accuracy driven uncertainty quantification framework for reliability analysis. Reliability Engineering & System Safety, 262: 1-21. doi: 10.1016/j.ress.2025.111128
    [83]
    Xiang Z, He X, Zou Y, et al. 2024. An importance sampling method for structural reliability analysis based on interpretable deep generative network. Engineering with Computers, 40(1): 367-380. doi: 10.1007/s00366-023-01790-2
    [84]
    You L F, Zhang J G, Du X S, et al. 2020. A new structural reliability analysis method in presence of mixed uncertainty variables. Chinese Journal of Aeronautics, 33(6): 1673-1682. doi: 10.1016/j.cja.2019.12.008
    [85]
    Yao W, Chen X, Luo W, et al. 2011. Review of uncertainty-based multidisciplinary design optimization methods for aerospace vehicles. Progress in Aerospace Sciences, 47(6): 450-479. doi: 10.1016/j.paerosci.2011.05.001
    [86]
    Zhang H R, Wang H, Wang Y, et al. 2019. Incremental shifting vector and mixed uncertainty analysis method for reliability-based design optimization. Structural and Multidisciplinary Optimization, 59: 1597-1616. doi: 10.1007/s00158-018-2178-x
    [87]
    Zhang Y D, Liu Y S, Guo Q. 2021. A global sensitivity analysis approach for multiple failure modes based on convex-probability hybrid uncertainty. Engineering Computations, 3: 1263-1286.
    [88]
    Zang T A, Hemsch M J, Hilburger M W, et al. 2002. Needs and Opportunities for Uncertainty-Based Multidisciplinary Design Methods for Aerospace Vehicles. No. NASA-TM-2002-211462.
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