A Tailless UAV Multidisciplinary Design Optimization Using Global Variable Fidelity Modeling

• Published in: International journal of aeronautical and space sciences Vol. 18; no. 4; pp. 662 - 674
• Main Authors: Tyan, Maxim, Nguyen, Nhu Van, Lee, Jae-Woo
• Format: Journal Article
• Language: English
• Published: 한국항공우주학회 01.12.2017
• Subjects: 항공우주공학; Multidisciplinary Design Optimization (MDO); Variable fidelity optimization; Unmanned Oerial Vehicle (UAV); Tailless aircraft; Aircraft conceptual design
• ISSN: 2093-274X; 2093-2480
• DOI: 10.5139/IJASS.2017.18.4.662

This paper describes the multidisciplinary design optimization (MDO) process of a tailless unmanned combat aerial vehicle (UCAV) using global variable fidelity aerodynamic analysis. The developed tailless UAV design framework combines multiple disciplines that are based on low-fidelity and empirical analysis methods. An automated high-fidelity aerodynamic analysis is efficiently integrated into the MDO framework. Global variable fidelity modeling algorithm manages the use of the highfidelity analysis to enhance the overall accuracy of the MDO by providing the initial sampling of the design space with iterative refinement of the approximation model in the neighborhood of the optimum solution. A design formulation was established considering a specific aerodynamic, stability and control design features of a tailless aircraft configuration with a UCAV specific mission profile. Design optimization problems with low-fidelity and variable fidelity analyses were successfully solved. The objective function improvement is 14.5% and 15.9% with low and variable fidelity optimization respectively. Results also indicate that low-fidelity analysis overestimates the value of lift-to-drag ratio by 3-5%, while the variable fidelity results are equal to the high-fidelity analysis results by algorithm definition. KCI Citation Count: 4