Towards a multi-fidelity & multi-objective Bayesian optimization efficient algorithm

被引:8
作者
Charayron, Remy [1 ,2 ]
Lefebvre, Thierry [1 ]
Bartoli, Nathalie [1 ]
Morlier, Joseph [2 ]
机构
[1] Univ Toulouse, ONERA DTIS, 2 Ave Edouard Belin, F-31400 Toulouse, France
[2] Univ Toulouse, CNRS, ICA, ISAE SUPAERO,MINES ALBI,UPS,INSA, 3 Rue Caroline Aigle, F-31400 Toulouse, France
关键词
Bayesian optimization; Multi-fidelity; Multi-objective; Multi-disciplinary optimization; Kriging; Fixed-wing drone; GLOBAL OPTIMIZATION; DESIGN; ENDURANCE; SYSTEM; MODEL;
D O I
10.1016/j.ast.2023.108673
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Black-box optimization methods like Bayesian optimization are often employed in cases where the underlying objective functions and their gradient are complex, expensive to evaluate, or unavailable in closed form, making it difficult or impossible to use traditional optimization techniques. Fixed-wing drone design problems often face this kind of situations. Moreover in the literature multi-fidelity strategies allow to consistently reduce the optimization cost for mono-objective problems. The purpose of this paper is to propose a multi-fidelity Bayesian optimization method that suits to multi-objective problem solving. In this approach, low-fidelity and high-fidelity objective functions are used to build co-Kriging surrogate models which are then optimized using a Bayesian framework. By combining multiple fidelity levels and objectives, this approach efficiently explores the solution space and identifies the set of Pareto-optimal solutions. First, four analytical problems were solved to assess the methodology. The approach was then used to solve a more realistic problem involving the design of a fixed-wing drone for a specific mission. Compared to the mono-fidelity strategy, the multi-fidelity one significantly improved optimization performance. On the drone test case, using a fixed budget, it allows to divide the inverted generational distance metric by 6.87 on average.
引用
收藏
页数:16
相关论文
共 78 条
[1]  
[Anonymous], 2016, 17 AIAA ISSMO MULT A
[2]  
[Anonymous], MECH PROPERTIES CARB
[3]  
[Anonymous], 2013, INT C MACHINE LEARNI
[4]  
[Anonymous], 2017, 18 AIAA ISSMO MULT A
[5]   Multi-Fidelity Multi-Objective Efficient Global Optimization Applied to Airfoil Design Problems [J].
Ariyarit, Atthaphon ;
Kanazaki, Masahiro .
APPLIED SCIENCES-BASEL, 2017, 7 (12)
[6]   Cross Validation and Maximum Likelihood estimations of hyper-parameters of Gaussian processes with model misspecification [J].
Bachoc, Francois .
COMPUTATIONAL STATISTICS & DATA ANALYSIS, 2013, 66 :55-69
[7]  
Baek SS, 2013, IEEE INT C INT ROBOT, P2955, DOI 10.1109/IROS.2013.6696775
[8]   Adaptive modeling strategy for constrained global optimization with application to aerodynamic wing design [J].
Bartoli, N. ;
Lefebvre, T. ;
Dubreuil, S. ;
Olivanti, R. ;
Priem, R. ;
Bons, N. ;
Martins, J. R. R. A. ;
Morlier, J. .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 90 :85-102
[9]  
Belakaria S., 2020, P AAAI C ARTIFICIAL, V34, P10035, DOI DOI 10.1609/AAAI.V34I06.6560
[10]  
Bouhlel M.A., 2022, Surrogate modelling toolbox