Flying-Wing Type UAV Design Optimization for Flight Stability Enhancement
![]() |
Seong, Dong-gyu
(Department of Aerospace Information Engineering, Konkuk University)
Juliawan, Nadhie (Department of Aerospace Information Engineering, Konkuk University) Tyan, Maxim (Department of Aerospace Information Engineering, Konkuk University) Kim, Sanho (Department of Aerospace Information Engineering, Konkuk University) Lee, Jae-woo (Department of Aerospace Information Engineering, Konkuk University) |
1 | Li, M., Bai, J., Li, L., Meng, X., Liu, Q. and Chen, B., "A gradient-based aero-stealth optimization design method for flying wing aircraft," Aerospace Science and Technology, Vol. 92, September 2019, pp. 156-169. DOI |
2 | Lei, S., Hua, Y., Yang, Z., Haoyu, Z. and Jun, H., "Dihedral influence on lateral-directional dynamic stability on large aspect ratio tailless flying wing aircraft," Chinese Journal of Aeronautics, Vol. 27, August 2014, pp. 1149-1155. DOI |
3 | Aircraft Design Education Research Society, Aircraft Conceptual Design, 2nd Edition, KyungMoon, Seoul, 2016, pp. 181-382. |
4 | Nelson, R. C., Flight Stability and Automatic Control, 2nd Edition, McGraw-Hill education, New york, 1998, pp. 131-234. |
5 | Kim, B. S., Kim, Y. D., Bang, H. C., Tak, M. J. and Hong, S. K., Flight dynamics and control, 1st Edition, KyungMoon, Seoul, 2004, pp. 15-142. |
6 | Jacopo, T., "Development of a Flight Dynamic Model of a Flying Wing Configuration," Master thesis, Sapienza - University of Rome, 2014. |
7 | Rosolem, R., Gupta, H. V., Shuttleworth, W. J. and Zeng, X., "A fully multiple-criteria implementation of the Sobol method for parameter sensitivity analysis," Journal of Geophysical Research, Vol. 117, April 2012, Res. 117, D07103. |
8 | Seong, D. G., "Iterative Design and Verification Analysis for Stability of Flying-Wing Type Drone," Proceeding of The Korean Society for Aeronautical and Space Sciences Spring Conference, April 2019, pp. 715-718. |
9 | U.S. Department of Defense, Military Specification Handbook MIL-HDBK-1797: Flying Qualities of Piloted Aircraft, 1997. |
10 | Drela, M., AVL 3.36 User primer, 2017, Available at http://web.mit.edu/drela/Public/web/avl/. |
11 | Boggs, P. T. and Tolle, J. W., "Sequential Quadratic Programming," Acta Numerica, Vol. 4, January 1995, pp. 1-51. DOI |
12 | Pereira, R. L., "Validation of software for the calculation of aerodynamic coefficients with a focus on the software package Tornado," tech.rep., Linkoping University, 2010 |
13 | ANSYS Fluent Theory Guide, 2013, Available at http://www.ansys.com |
14 | Python module Scipy.org, Available at https://docs.scipy.org/doc/scipy/reference/index.html |
15 | Elhefnawy, N., "A Sixth Generation Fighter? An Overview of the Essential Background," SSRN, (July 18, 2018). Available at SSRN: https://ssrn.com/abstract=3215780. |
16 | Raymer, D., Aircraft Design : A Conceptual Approach, 15th Edition, AIAA, Virginia, 2012, pp. 59-246. |
17 | Pan, Y., Huang, J., Li, F. and Yan, C., "Integrated Design Optimization of Aero-dynamic and Stealthy Performance for Flying Wing Aircraft," Proceedings of the International Multi Conference of Engineers and Computer Scientists, Vol. 2, March 2017, pp. 1051-1056. |
18 | Nickel, K. and Wohlfahrt, M., Tailless Aircraft in theory and practice, 1st Edition, Edward Arnold, London, 1994, pp. 8-120. |
19 | Qu, X., Zhang, W., Shi, J. and Lyu, Y., "A Novel Yaw Control Method for Flying-wing Aircraft in Low Speed Regime," Aerospace Science and Technology, Vol. 69, October 2017, pp. 636-649. DOI |
![]() |