MATEC Web of Conferences
Volume 52, 20162016 International Conference on Design Engineering and Science (ICDES 2016)
|Number of page(s)||7|
|Section||Chapter 1: Modeling and Simulation|
|Published online||11 April 2016|
Aircraft Performance Analysis in Conceptual Design Phase based on System-of-Systems Simulations
School of Aeronautic Science and Engineering, Beihang University, Beijing, China
a Corresponding author: email@example.com
To obtain a competitive design in aircraft conceptual design phase, this paper propose an aircraft performance analysis method based on system-of-systems (SoS) simulations. The analysis process includes design space exploration and mission effectiveness analysis and the stochastic nature in SoS mission is captured based on a Monte Carlo method. Meanwhile as an example, the performance of UAVs which are applied in earthquake search and rescue SoS is analysed based on SoS simulations. The results show that the level of aircraft performance which leads to an optimum SoS effectiveness could be designed below the maximum performance. And it is necessary to apply SoS simulations into aircraft conceptual design phase to help designers optimize aircraft performance.
© Owned by the authors, published by EDP Sciences, 2016
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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