Advances in aircraft design: multiobjective optimization and a markup language
Today's modern aerospace systems exhibit strong interdisciplinary coupling and require a multidisciplinary, collaborative approach. Analysis methods that were once considered feasible only for advanced and detailed design are now available and even practical at the conceptual design stage. This...
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ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-251422021-09-30T05:27:12Z Advances in aircraft design: multiobjective optimization and a markup language Deshpande, Shubhangi Govind Computer Science Watson, Layne T. Canfield, Robert A. Fox, Edward A. North, Christopher L. Ramakrishnan, Naren Kolonay, Raymond M. Multiobjective optimization Pareto optimality direct search method surrogates adaptive scalarization Delaunay triangulation multidisciplinary aircraft design markup language XML schema. Today's modern aerospace systems exhibit strong interdisciplinary coupling and require a multidisciplinary, collaborative approach. Analysis methods that were once considered feasible only for advanced and detailed design are now available and even practical at the conceptual design stage. This changing philosophy for conducting conceptual design poses additional challenges beyond those encountered in a low fidelity design of aircraft. This thesis takes some steps towards bridging the gaps in existing technologies and advancing the state-of-the-art in aircraft design. The first part of the thesis proposes a new Pareto front approximation method for multiobjective optimization problems. The method employs a hybrid optimization approach using two derivative free direct search techniques, and is intended for solving blackbox simulation based multiobjective optimization problems with possibly nonsmooth functions where the analytical form of the objectives is not known and/or the evaluation of the objective function(s) is very expensive (very common in multidisciplinary design optimization). A new adaptive weighting scheme is proposed to convert a multiobjective optimization problem to a single objective optimization problem. Results show that the method achieves an arbitrarily close approximation to the Pareto front with a good collection of well-distributed nondominated points. The second part deals with the interdisciplinary data communication issues involved in a collaborative mutidisciplinary aircraft design environment. Efficient transfer, sharing, and manipulation of design and analysis data in a collaborative environment demands a formal structured representation of data. XML, a W3C recommendation, is one such standard concomitant with a number of powerful capabilities that alleviate interoperability issues. A compact, generic, and comprehensive XML schema for an aircraft design markup language (ADML) is proposed here to provide a common language for data communication, and to improve efficiency and productivity within a multidisciplinary, collaborative environment. An important feature of the proposed schema is the very expressive and efficient low level schemata. As a proof of concept the schema is used to encode an entire Convair B58. As the complexity of models and number of disciplines increases, the reduction in effort to exchange data models and analysis results in ADML also increases. Ph. D. 2014-01-24T09:00:42Z 2014-01-24T09:00:42Z 2014-01-23 Dissertation vt_gsexam:2103 http://hdl.handle.net/10919/25142 In Copyright http://rightsstatements.org/vocab/InC/1.0/ ETD application/pdf text/xml application/octet-stream Virginia Tech |
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Multiobjective optimization Pareto optimality direct search method surrogates adaptive scalarization Delaunay triangulation multidisciplinary aircraft design markup language XML schema. |
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Multiobjective optimization Pareto optimality direct search method surrogates adaptive scalarization Delaunay triangulation multidisciplinary aircraft design markup language XML schema. Deshpande, Shubhangi Govind Advances in aircraft design: multiobjective optimization and a markup language |
description |
Today's modern aerospace systems exhibit strong interdisciplinary coupling and require a multidisciplinary, collaborative approach. Analysis methods that were once considered feasible only for advanced and detailed design are now available and even practical at the conceptual design stage. This changing philosophy for conducting conceptual design poses additional challenges beyond those encountered in a low fidelity design of aircraft. This thesis takes some steps towards bridging the gaps in existing technologies and advancing the state-of-the-art in aircraft design.
The first part of the thesis proposes a new Pareto front approximation method for multiobjective optimization problems. The method employs a hybrid optimization approach using two derivative free direct search techniques, and is intended for solving blackbox simulation based multiobjective optimization problems with possibly nonsmooth functions where the analytical form of the objectives is not known and/or the evaluation of the objective function(s) is very expensive (very common in multidisciplinary design optimization). A new adaptive weighting scheme is proposed to convert a multiobjective optimization problem to a single objective optimization problem. Results show that the method achieves an arbitrarily close approximation to the Pareto front with a good collection of well-distributed nondominated points.
The second part deals with the interdisciplinary data communication issues involved in a collaborative mutidisciplinary aircraft design environment. Efficient transfer, sharing, and manipulation of design and analysis data in a collaborative environment demands a formal structured representation of data. XML, a W3C recommendation, is one such standard concomitant with a number of powerful capabilities that alleviate interoperability issues. A compact, generic, and comprehensive XML schema for an aircraft design markup language (ADML) is proposed here to provide a common language for data communication, and to improve efficiency and productivity within a multidisciplinary, collaborative environment. An important feature of the proposed schema is the very expressive and efficient low level schemata. As a proof of concept the schema is used to encode an entire Convair B58. As the complexity of models and number of disciplines increases, the reduction in effort to exchange data models and analysis results in ADML also increases. === Ph. D. |
author2 |
Computer Science |
author_facet |
Computer Science Deshpande, Shubhangi Govind |
author |
Deshpande, Shubhangi Govind |
author_sort |
Deshpande, Shubhangi Govind |
title |
Advances in aircraft design: multiobjective optimization and a markup language |
title_short |
Advances in aircraft design: multiobjective optimization and a markup language |
title_full |
Advances in aircraft design: multiobjective optimization and a markup language |
title_fullStr |
Advances in aircraft design: multiobjective optimization and a markup language |
title_full_unstemmed |
Advances in aircraft design: multiobjective optimization and a markup language |
title_sort |
advances in aircraft design: multiobjective optimization and a markup language |
publisher |
Virginia Tech |
publishDate |
2014 |
url |
http://hdl.handle.net/10919/25142 |
work_keys_str_mv |
AT deshpandeshubhangigovind advancesinaircraftdesignmultiobjectiveoptimizationandamarkuplanguage |
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1719486388261355520 |