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Please use this identifier to cite or link to this item:
http://hdl.handle.net/1853/6273
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| Title: | An Integrated Decision-making Method to Identify Design Requirements Through Agent-based Simulation for Personal Air Vehicle System |
| Authors: | Lewe, Jung-Ho Ahn, Byung-Ho DeLaurentis, Daniel A. Mavris, Dimitri N. Schrage, Daniel P. |
| Subjects : | Agent-based modeling techniques Decision-making Design requirements Personal air vehicles Simulations Decision-making |
| Issue Date: | Oct-2002 |
| Publisher: | Georgia Institute of Technology |
| Series/Report no.: | ASDL;AIAA-2002-5876 |
| Abstract: | A product?s design requirements guide the next development efforts. Thus, correct decision-making is critical in generating design requirements as vehicle concepts are being formulated. A new method is proposed to account for system-of-systems aspects and to aid a decision-making process in synthesizing design requirements for a personal air vehicle system. The use of an agent-based modeling technique facilitates the abstraction of the key elements in the whole system. A traveling party is treated as an agent, and the infrastructure environment in the national transportation system is easily represented in the model. A number of simulations are performed to demonstrate the capability of this new approach. The method not only measures the effect of design requirements of a personal air vehicle system through sensitivity analyses, but also evaluates the effect of system technologies quantitatively, while maintaining the system-of-systems perspective. With this powerful method, designers can extract essential technical requirements that allow polishing of concept vehicles; policy makers can investigate the infrastructure and technology impact of new systems; and business planners can perform an analysis based on their own market assumptions. |
| Description: | Presented at AIAA Aircraft Technology, Integration, and Operation (ATIO) Technical Forum, October 1-3, 2002, Los Angeles, CA. |
| Type: | Paper |
| URI: | http://hdl.handle.net/1853/6273 |
| Appears in Collections: | Aerospace Systems Design Lab Publications
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