Nondeterministic Kriging for Engineering Design Exploration
In this paper, the nondeterministic kriging (NDK) method is proposed, aiming for the applications of engineering design exploration, especially when only a limited number of random samples is available from either nondeterministic simulations or physical experiments under uncertainty. To handle nond...
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Veröffentlicht in: | AIAA journal 2019-04, Vol.57 (4), p.1659-1670 |
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description | In this paper, the nondeterministic kriging (NDK) method is proposed, aiming for the applications of engineering design exploration, especially when only a limited number of random samples is available from either nondeterministic simulations or physical experiments under uncertainty. To handle nondeterministic data, the proposed NDK method uses separate aleatory and epistemic uncertainty processes. In a general situation in which resources are limited in generating random samples, an aleatory variance is assessed via a local regression kernel process. It is often found that a prediction model built with a conventional kriging suffers from the overfitting issue, which becomes worse with noisy and random data. The proposed NDK method can provide physically meaningful insights into both the main trend and the prediction uncertainty of system behaviors by capturing uncertainty in the sample data and suppressing the numerical instability. The predicted uncertainty from the proposed approach can be represented in terms of distinguishable aleatory and epistemic uncertainties, which will be useful in a decision-making process for an adaptive model building and design exploration. The potential benefits of using the proposed NDK method are demonstrated with multiple numerical examples, including mathematical and aircraft concept design problems. |
doi_str_mv | 10.2514/1.J057364 |
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To handle nondeterministic data, the proposed NDK method uses separate aleatory and epistemic uncertainty processes. In a general situation in which resources are limited in generating random samples, an aleatory variance is assessed via a local regression kernel process. It is often found that a prediction model built with a conventional kriging suffers from the overfitting issue, which becomes worse with noisy and random data. The proposed NDK method can provide physically meaningful insights into both the main trend and the prediction uncertainty of system behaviors by capturing uncertainty in the sample data and suppressing the numerical instability. The predicted uncertainty from the proposed approach can be represented in terms of distinguishable aleatory and epistemic uncertainties, which will be useful in a decision-making process for an adaptive model building and design exploration. The potential benefits of using the proposed NDK method are demonstrated with multiple numerical examples, including mathematical and aircraft concept design problems.</description><identifier>ISSN: 0001-1452</identifier><identifier>EISSN: 1533-385X</identifier><identifier>DOI: 10.2514/1.J057364</identifier><language>eng</language><publisher>Virginia: American Institute of Aeronautics and Astronautics</publisher><subject>Aircraft design ; Building design ; Computer simulation ; Decision making ; Design engineering ; Kriging interpolation ; Mathematical models ; Numerical prediction ; Stability ; Uncertainty</subject><ispartof>AIAA journal, 2019-04, Vol.57 (4), p.1659-1670</ispartof><rights>Copyright © 2019 by the American Institute of Aeronautics and Astronautics, Inc. The U.S. Government has a royalty-free license to exercise all rights under the copyright claimed herein for Governmental purposes. All other rights are reserved by the copyright owner. All requests for copying and permission to reprint should be submitted to CCC at ; employ the eISSN to initiate your request. See also AIAA Rights and Permissions .</rights><rights>Copyright © 2019 by the American Institute of Aeronautics and Astronautics, Inc. The U.S. Government has a royalty-free license to exercise all rights under the copyright claimed herein for Governmental purposes. All other rights are reserved by the copyright owner. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. 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The potential benefits of using the proposed NDK method are demonstrated with multiple numerical examples, including mathematical and aircraft concept design problems.</description><subject>Aircraft design</subject><subject>Building design</subject><subject>Computer simulation</subject><subject>Decision making</subject><subject>Design engineering</subject><subject>Kriging interpolation</subject><subject>Mathematical models</subject><subject>Numerical prediction</subject><subject>Stability</subject><subject>Uncertainty</subject><issn>0001-1452</issn><issn>1533-385X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><recordid>eNplkEtLAzEUhYMoWKsL_8GAILiYevOcFFdSx2fRjYK7kMkkJaVNxmQK-u-d0oILV-ce-DiXcxA6xzAhHLNrPHkGXlHBDtAIc0pLKvnnIRoBAC4x4-QYneS8HBypJB6hm9cYWtvbtPbB596b4iX5hQ-LwsVU1GE4rU1bf2ezX4Si_u5WMenex3CKjpxeZXu21zH6uK_fZ4_l_O3haXY7LzUltC8FayQDAVhba1uHDVRGtsJVzLaNnlbOWTCUi6lmRsgGjCYMsMBaAhXUOTpGF7vcLsWvjc29WsZNCsNLRQgQLofGMFBXO8qkmHOyTnXJr3X6URjUdhuF1X6bgb3csdpr_Zf2H_wFs2Bhog</recordid><startdate>20190401</startdate><enddate>20190401</enddate><creator>Bae, Harok</creator><creator>Clark, Daniel L</creator><creator>Forster, Edwin E</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20190401</creationdate><title>Nondeterministic Kriging for Engineering Design Exploration</title><author>Bae, Harok ; Clark, Daniel L ; Forster, Edwin E</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a323t-64b840601aeeedf1c07c8d6f74edba97ffe0c3569a4c68b0ca240161a80363ff3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>Aircraft design</topic><topic>Building design</topic><topic>Computer simulation</topic><topic>Decision making</topic><topic>Design engineering</topic><topic>Kriging interpolation</topic><topic>Mathematical models</topic><topic>Numerical prediction</topic><topic>Stability</topic><topic>Uncertainty</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Bae, Harok</creatorcontrib><creatorcontrib>Clark, Daniel L</creatorcontrib><creatorcontrib>Forster, Edwin E</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>AIAA journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Bae, Harok</au><au>Clark, Daniel L</au><au>Forster, Edwin E</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Nondeterministic Kriging for Engineering Design Exploration</atitle><jtitle>AIAA journal</jtitle><date>2019-04-01</date><risdate>2019</risdate><volume>57</volume><issue>4</issue><spage>1659</spage><epage>1670</epage><pages>1659-1670</pages><issn>0001-1452</issn><eissn>1533-385X</eissn><abstract>In this paper, the nondeterministic kriging (NDK) method is proposed, aiming for the applications of engineering design exploration, especially when only a limited number of random samples is available from either nondeterministic simulations or physical experiments under uncertainty. To handle nondeterministic data, the proposed NDK method uses separate aleatory and epistemic uncertainty processes. In a general situation in which resources are limited in generating random samples, an aleatory variance is assessed via a local regression kernel process. It is often found that a prediction model built with a conventional kriging suffers from the overfitting issue, which becomes worse with noisy and random data. The proposed NDK method can provide physically meaningful insights into both the main trend and the prediction uncertainty of system behaviors by capturing uncertainty in the sample data and suppressing the numerical instability. The predicted uncertainty from the proposed approach can be represented in terms of distinguishable aleatory and epistemic uncertainties, which will be useful in a decision-making process for an adaptive model building and design exploration. 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subjects | Aircraft design Building design Computer simulation Decision making Design engineering Kriging interpolation Mathematical models Numerical prediction Stability Uncertainty |
title | Nondeterministic Kriging for Engineering Design Exploration |
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