Gradient-based constrained optimization using a database of linear reduced-order models

被引:56
作者
Choi, Youngsoo [1 ]
Boncoraglio, Gabriele [2 ]
Anderson, Spenser [2 ]
Amsallem, David [3 ,5 ]
Farhat, Charbel [2 ,3 ,4 ]
机构
[1] Lawrence Livermore Natl Lab, Computat Engn Div, Livermore, CA 94550 USA
[2] Stanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
[3] Stanford Univ, Dept Mech Engn, Stanford, CA 94305 USA
[4] Stanford Univ, Inst Computat & Math Engn, Stanford, CA 94305 USA
[5] Facebook, Menlo Pk, CA 94025 USA
关键词
Constrained optimization; Flutter; Gradient-based optimization; Interpolation on a matrix manifold; Model reduction; Parameter sampling; REAL-TIME SOLUTION; DYNAMICS; APPROXIMATIONS; INTERPOLATION; FORMULATION; ALGORITHM; SYSTEMS;
D O I
10.1016/j.jcp.2020.109787
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
A methodology grounded in model reduction is presented for accelerating the gradient-based solution of a family of linear or nonlinear constrained optimization problems where the constraints include at least one linear Partial Differential Equation (PDE). A key component of this methodology is the construction, during an offline phase, of a database of pointwise, linear, Projection-based Reduced-Order Models (PROM)s associated with a design parameter space and the linear PDE(s). A parameter sampling procedure based on an appropriate saturation assumption is proposed to maximize the efficiency of such a database of PROMs. A real-time method is also presented for interpolating at any queried but unsampled parameter vector in the design parameter space the relevant sensitivities of a PROM. The practical feasibility, computational advantages, and performance of the proposed methodology are demonstrated for several realistic, nonlinear, aerodynamic shape optimization problems governed by linear aeroelastic constraints. (C) 2020 Elsevier Inc. All rights reserved.
引用
收藏
页数:24
相关论文
共 42 条
[1]   A posteriori error estimators for linear reduced-order models using Krylov-based integrators [J].
Amsallem, D. ;
Hetmaniuk, U. .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 2015, 102 (05) :1238-1261
[2]  
Amsallem D., 2015, ARXIV150607441PHYSIC, P1
[3]   Interpolation method for adapting reduced-order models and application to aeroelasticity [J].
Amsallem, David ;
Farhat, Charbel .
AIAA JOURNAL, 2008, 46 (07) :1803-1813
[4]   Real-time solution of linear computational problems using databases of parametric reduced-order models with arbitrary underlying meshes [J].
Amsallem, David ;
Tezaur, Radek ;
Farhat, Charbel .
JOURNAL OF COMPUTATIONAL PHYSICS, 2016, 326 :373-397
[5]   Design optimization using hyper-reduced-order models [J].
Amsallem, David ;
Zahr, Matthew ;
Choi, Youngsoo ;
Farhat, Charbel .
STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, 2015, 51 (04) :919-940
[6]   On the Stability of Reduced-Order Linearized Computational Fluid Dynamics Models Based on POD and Galerkin Projection: Descriptor vs Non-Descriptor Forms [J].
Amsallem, David ;
Farhat, Charbel .
REDUCED ORDER METHODS FOR MODELING AND COMPUTATIONAL REDUCTION, 2014, 9 :215-233
[7]   Nonlinear model order reduction based on local reduced-order bases [J].
Amsallem, David ;
Zahr, Matthew J. ;
Farhat, Charbel .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 2012, 92 (10) :891-916
[8]   AN ONLINE METHOD FOR INTERPOLATING LINEAR PARAMETRIC REDUCED-ORDER MODELS [J].
Amsallem, David ;
Farhat, Charbel .
SIAM JOURNAL ON SCIENTIFIC COMPUTING, 2011, 33 (05) :2169-2198
[9]   Toward Real-Time Computational-Fluid-Dynamics-Based Aeroelastic Computations Using a Database of Reduced-Order Information [J].
Amsallem, David ;
Cortial, Julien ;
Farhat, Charbel .
AIAA JOURNAL, 2010, 48 (09) :2029-2037
[10]   A method for interpolating on manifolds structural dynamics reduced-order models [J].
Amsallem, David ;
Cortial, Julien ;
Carlberg, Kevin ;
Farhat, Charbel .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 2009, 80 (09) :1241-1258