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Swarm heuristic for identifying preferred solutions in surrogate-based multi-objective engineering design

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posted on 2024-11-23, 07:42 authored by Robert Carrese, András Sobester, Hadi Winarto, Xiaodong LiXiaodong Li
Exploring the entire Pareto frontier of high-fidelity multidisciplinary problems can be prohibitive due to the excessive number of expensive evaluations required. The use of surrogate models offers promise toward managing such problems, which are restricted by a computational budget. In this paper, the kriging-assisted user-preference multi-objective particle swarm heuristic is presented, in which less accurate but inexpensive surrogate models are used cooperatively with the precise but expensive objective functions to alleviate the computational burden. A userpreference module is integrated into the optimization framework, which guides the swarm toward preferred regions of the Pareto frontier, thereby focusing all computing effort on identifying only solutions of interest to the designer. While providing a logical criterion to prescreen candidates for precise evaluation, the additional guidance provided by user-preferences guarantees an accelerated convergence rate. To depict the proficiency of the proposed framework, a suite of test problems, including the multidisciplinary cross-sectional design of a semimonocoque fuselage enclosing a pressurized cabin and payload bay, is presented.Aparametric model is described that is capable of generating a broad range of double-lobe fuselage designs. The superiority of the kriging-assisted user-preference multi-objective particle swarm optimization algorithm over more traditional search methods to efficiently manage high-fidelity discontinuous design problems is highlighted.

History

Related Materials

  1. 1.
    DOI - Is published in 10.2514/1.J050819
  2. 2.
    ISSN - Is published in 00011452

Journal

AIAA Journal

Volume

49

Issue

7

Start page

1437

End page

1449

Total pages

13

Publisher

American Institute of Aeronautics and Astronautics

Place published

United States

Language

English

Copyright

© 2011 by the American Institute of Aeronautics and Astronautics, Inc.

Former Identifier

2006027784

Esploro creation date

2020-06-22

Fedora creation date

2012-02-03

Open access

  • Yes

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