FLORA 发表于 2025-3-27 00:42:40
http://reply.papertrans.cn/99/9806/980557/980557_31.pngEncoding 发表于 2025-3-27 02:08:48
http://reply.papertrans.cn/99/9806/980557/980557_32.pngTrypsin 发表于 2025-3-27 05:26:38
Trust Region Filter-SQP Method for Multi-Fidelity Wing Aerostructural Optimization, construct the quadratic programming subproblem. The high fidelity model is used to compute the objective function and the constraints used to generate the filter. The results of the high fidelity analysis are also used to calibrate the results of the lower fidelity tool during the optimization. ThiLipoma 发表于 2025-3-27 11:56:49
http://reply.papertrans.cn/99/9806/980557/980557_34.png烦忧 发表于 2025-3-27 16:39:06
Data Analytic UQ Cascade,ion and probability density function quantiles of the optimization parameters permits to define the notion of directional extreme scenarios (DES) without sampling of large dimension design spaces. One goes beyond DES with ensemble Kalman filters (EnKF) after the multi-point optimization algorithm isciliary-body 发表于 2025-3-27 18:25:40
http://reply.papertrans.cn/99/9806/980557/980557_36.png犬儒主义者 发表于 2025-3-28 00:46:29
http://reply.papertrans.cn/99/9806/980557/980557_37.pngchiropractor 发表于 2025-3-28 03:41:38
A New, General Neighboring Optimal Guidance for Aerospace Vehicles,ime-domain neighboring optimal guidance algorithm is applied to two typical aerospace maneuvers: (1) minimum-time climbing path of a Boeing 727 aircraft and (2) interception of fixed and moving targets. Perturbations arising from nonnominal propulsive thrust or atmospheric density and from errors in敌意 发表于 2025-3-28 09:09:45
http://reply.papertrans.cn/99/9806/980557/980557_39.pngCUMB 发表于 2025-3-28 14:27:17
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