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Development of a decision support framework for systems architecting in aerospace applications

Development of a decision support framework for systems architecting in aerospace applications
Development of a decision support framework for systems architecting in aerospace applications
This paper describes the development of a new decision support framework that assists system designers in identifying optimal architectural concepts, and a more focused design exploration strategy with the aim of improving system utility, and reducing life-cycle cost(LCC). The framework developed has been applied to the design of a low-cost Unmanned Aerial Vehicle (UAV) for use in coastal monitoring and search and rescue operations. The case study was used to demonstrate the applicability of the framework in allowing system designers to generate and trade between different architectural concepts, and also numerically capture the rationale behind the decision-making process. This is achieved by using a formal modelling approach that defines the architectural decision-making process as a network, whereby the nodes of the network represent system functions and the connecting edges represent the physical/preferential constraints declared by the decision maker on the architectural solution space. In addition, the framework makes use of multi-objective optimization methodologies, in combination with centrality measures from graph theory and a modified version of the main effects analysis from the Design of Experiments (DoE) literature, to identify Pareto optimal solutions and a focused architectural exploration strategy with the aim of improving upon the solutions within the Pareto set.
1-39
Surendra, Amrith
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Scanlan, James
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Eres, Hakki
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Harman, Adam
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Surendra, Amrith
a8965a4f-47aa-4817-82d2-ac091cdb7d08
Scanlan, James
7ad738f2-d732-423f-a322-31fa4695529d
Eres, Hakki
b22e2d66-55c4-46d2-8ec3-46317033de43
Harman, Adam
076eeee2-ba9f-4b49-85cf-da9aaec66ba4

Surendra, Amrith, Scanlan, James, Eres, Hakki and Harman, Adam (2015) Development of a decision support framework for systems architecting in aerospace applications. Journal of Aerospace Information Systems, 1-39. (In Press)

Record type: Article

Abstract

This paper describes the development of a new decision support framework that assists system designers in identifying optimal architectural concepts, and a more focused design exploration strategy with the aim of improving system utility, and reducing life-cycle cost(LCC). The framework developed has been applied to the design of a low-cost Unmanned Aerial Vehicle (UAV) for use in coastal monitoring and search and rescue operations. The case study was used to demonstrate the applicability of the framework in allowing system designers to generate and trade between different architectural concepts, and also numerically capture the rationale behind the decision-making process. This is achieved by using a formal modelling approach that defines the architectural decision-making process as a network, whereby the nodes of the network represent system functions and the connecting edges represent the physical/preferential constraints declared by the decision maker on the architectural solution space. In addition, the framework makes use of multi-objective optimization methodologies, in combination with centrality measures from graph theory and a modified version of the main effects analysis from the Design of Experiments (DoE) literature, to identify Pareto optimal solutions and a focused architectural exploration strategy with the aim of improving upon the solutions within the Pareto set.

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More information

Accepted/In Press date: 1 April 2015
Organisations: Computational Engineering & Design Group

Identifiers

Local EPrints ID: 377917
URI: http://eprints.soton.ac.uk/id/eprint/377917
PURE UUID: 18e64d2f-7a02-4cc1-bc5c-f0baa40d6ae9
ORCID for Hakki Eres: ORCID iD orcid.org/0000-0003-4967-0833

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Date deposited: 23 Jun 2015 15:08
Last modified: 15 Mar 2024 03:14

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Contributors

Author: Amrith Surendra
Author: James Scanlan
Author: Hakki Eres ORCID iD
Author: Adam Harman

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