A robust optimization methodology for preliminary aircraft design

التفاصيل البيبلوغرافية
العنوان: A robust optimization methodology for preliminary aircraft design
المؤلفون: Matthieu Belleville, Pierre Maréchal, Thierry Druot, Aude Rondepierre, Sylvain Prigent
المساهمون: Institut Supérieur de l'Aéronautique et de l'Espace (ISAE-SUPAERO), Airbus Operation S.A.S., Airbus [France], Institut de Mathématiques de Toulouse UMR5219 (IMT), Université Toulouse Capitole (UT Capitole), Université de Toulouse (UT)-Université de Toulouse (UT)-Institut National des Sciences Appliquées - Toulouse (INSA Toulouse), Institut National des Sciences Appliquées (INSA)-Université de Toulouse (UT)-Institut National des Sciences Appliquées (INSA)-Université Toulouse - Jean Jaurès (UT2J), Université de Toulouse (UT)-Université Toulouse III - Paul Sabatier (UT3), Université de Toulouse (UT)-Centre National de la Recherche Scientifique (CNRS), Univ. Toulouse, ISAE-Supaéro, Institut National des Sciences Appliquées - Toulouse (INSA Toulouse), Institut National des Sciences Appliquées (INSA)-Institut National des Sciences Appliquées (INSA)-Université Toulouse 1 Capitole (UT1), Université Fédérale Toulouse Midi-Pyrénées-Université Fédérale Toulouse Midi-Pyrénées-Université Toulouse - Jean Jaurès (UT2J)-Université Toulouse III - Paul Sabatier (UT3), Université Fédérale Toulouse Midi-Pyrénées-Centre National de la Recherche Scientifique (CNRS)
المصدر: Engineering Optimization
Engineering Optimization, 2016, 48 (5), pp.883-899. ⟨10.1080/0305215X.2015.1062985⟩
Engineering Optimization, Taylor & Francis, 2016, 48 (5), pp.883-899. ⟨10.1080/0305215X.2015.1062985⟩
بيانات النشر: HAL CCSD, 2016.
سنة النشر: 2016
مصطلحات موضوعية: 0209 industrial biotechnology, Mathematical optimization, Engineering, Control and Optimization, Optimization problem, ComputerApplications_COMPUTERSINOTHERSYSTEMS, 02 engineering and technology, Robust linear programming, Management Science and Operations Research, Industrial and Manufacturing Engineering, Nonlinear programming, Engineering optimization, 020901 industrial engineering & automation, 0203 mechanical engineering, Control theory, Application to aircraft design, Continuous optimization, 020301 aerospace & aeronautics, business.industry, Applied Mathematics, Multidisciplinary design optimization, Probabilistic-based design optimization, Robust optimization, [INFO.INFO-IA]Computer Science [cs]/Computer Aided Engineering, Stochastic programming, Computer Science Applications, [MATH.MATH-OC]Mathematics [math]/Optimization and Control [math.OC], business, Optimization under uncertainty
الوصف: This article focuses on a robust optimization of an aircraft preliminary design under operational constraints. According to engineers' know-how, the aircraft preliminary design problem can be modelled as an uncertain optimization problem whose objective (the cost or the fuel consumption) is almost affine, and whose constraints are convex. It is shown that this uncertain optimization problem can be approximated in a conservative manner by an uncertain linear optimization program, which enables the use of the techniques of robust linear programming of Ben-Tal, El Ghaoui, and Nemirovski [Robust Optimization, Princeton University Press, 2009]. This methodology is then applied to two real cases of aircraft design and numerical results are presented.
اللغة: English
تدمد: 0305-215X
1029-0273
DOI: 10.1080/0305215X.2015.1062985⟩
URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b02665f1f5058108356971adcd26c2eb
https://hal-univ-tlse2.archives-ouvertes.fr/hal-01493830/document
Rights: OPEN
رقم الانضمام: edsair.doi.dedup.....b02665f1f5058108356971adcd26c2eb
قاعدة البيانات: OpenAIRE
الوصف
تدمد:0305215X
10290273
DOI:10.1080/0305215X.2015.1062985⟩