과제정보
본 연구는 국토교통부/국토교통과학기술진흥원(과제번호 20CTAP-C152021-02), 한국연구재단(No. 2020R1A6A1A03046811), 민군협력진흥원의 지원으로 민군협력기술사업(웨어러블 디스플레이 장치를 이용한 고신뢰성 무인비행체 시뮬레이터 기술 개발 과제)을 통해 수행된 과제임.
참고문헌
- Allerton, D., "The impact of flight simulation in aerospace," Aeronautical Journal, Vol. 114, December 2010, pp. 747~756. https://doi.org/10.1017/S0001924000004231
- Tyan, M., Kim, M. K., Pham, V., Choi, C. K., Nguyen, T. L. and Lee, J.-W., "Development of Advanced Aerodynamic Data Fusion Techniques for Flight Simulation Database Construction," AIAA 2018 Modeling and Simulation Technologies Conference, 2018-3581.
- Box, G. E. P. and Wilson, K. B., "On the Experimental Attainment of Optimum Conditions," Journal of the Royal Statistical Society Series B (Methodological), Vol. 13, No. 1, 1951, pp. 1~45. https://doi.org/10.1111/j.2517-6161.1951.tb00067.x
- Smith, K., "On the Standard Deviations of Adjusted and Interpolated Values of an Observed Polynomial Function and Its Constants and the Guidance They Give Towards a Proper Choice of the Distribution of Observations," Biometrika, Vol. 12, No. 1/2, 1918 pp. 1~85. https://doi.org/10.1093/biomet/12.1-2.1
- Matheron, G., "Principles of geostatistics," Economic Geology, Vol. 58, No. 8, December 1963, pp. 1246~1266. https://doi.org/10.2113/gsecongeo.58.8.1246
- Tyan, M., Nguyen, N. V. and Lee, J.-W., "A Tailless UAV Multidisciplinary Design Optimization Using Global Variable Fidelity Modeling," International Journal of Aeronautical and Space Sciences, Vol. 18, No. 4, 2017, pp. 662~674. https://doi.org/10.5139/IJASS.2017.18.4.662
- Nguyen, N. V. and Lee, J.-W., "Adaptive Multifidelity Constraints Method for Efficient Multidisciplinary Missile Design Framework," Journal of Spacecraft and Rockets, Vol. 53, No. 1, 2016, pp. 184~194. https://doi.org/10.2514/1.A33312
- Tyan, M., Nguyen, N. V. and Lee, J.-W., "Improving Variable-fidelity Modeling by Exploring Global Design Space and Radial Basis Function Networks for Aerofoil Design," Engineering Optimization, Vol. 47, No. 7, 2015, pp. 885~908. https://doi.org/10.1080/0305215X.2014.941290
- Nguyen, N. V., Tyan, M. and Lee, J.-W., "A Modified Variable Complexity Modeling for Efficient Multidisciplinary Aircraft Conceptual Design," Optimization and Engineering, Vol. 16, No. 2, 2015, pp. 485~505.
- Nguyen, N. V., et al., "Multidisciplinary Unmanned Combat Air Vehicle System Design Using Multi-fidelity Model," Aerospace Science and Technology, Vol. 26, No. 1, 2013, pp. 200~210. https://doi.org/10.1016/j.ast.2012.04.004
- Forrester, A. I. J. and Keane, A. J., "Recent advances in surrogate-based optimization," Progress in Aerospace Sciences, Vol. 45, No. 1-3, January 2009, pp. 50~79. https://doi.org/10.1016/j.paerosci.2008.11.001
- Etz, A., "Introduction to the Concept of Likelihood and Its Applications," Advances in Methods and Practices in Psychological Science, Vol. 1, No. 1, 2018, pp. 60~69. https://doi.org/10.1177/2515245917744314
- Haftka, R. T., "Combining Global and Local Approximations," AIAA Jornal, Vol. 29, No. 9, 1991, pp. 1523~1525. https://doi.org/10.2514/3.10768
- Picheny, V., Ginsbourger, D., Roustant, O., Haftka, R. T. and Kim, N.-H., "Adaptive Designs of Experiments for Accurate Approximation of a Target Region," Journal of Mechanical Design, Vol. 132, No. 7, June 2010.
- Tyan, M. and Lee, J.-W., "Efficient multiresponse adaptive sampling algorithm for construction of variable-fidelity aerodynamic tables," Chinese Journal of Aeronautics, Vol. 32, No. 3, January 2019, pp. 547~558. https://doi.org/10.1016/j.cja.2018.12.012
- Lee, D., Nguyen, N. V., Tyan, M., Chun, H.-G., Kim, S. and Lee, J.-W., "Enhanced multi-fidelity model for flight simulation using global exploration and the Kriging method," Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 231, No. 4, 2017, pp. 606~620. https://doi.org/10.1177/0954410016641441
- Ronch, A. D., Ghoreyshi, M. and Badcock, K. J., "On the generation of flight dynamics aerodynamic tables by computational fluid dynamics," Progress in Aerospace Sciences, Vol. 47, No. 8, 2011, pp. 597~620. https://doi.org/10.1016/j.paerosci.2011.09.001
- Fox, M. C. and Forrest, D. K., "Supersonic Aerodynamic Characteristics of an Advanced F-16 Derivative Aircraft Configuration," NASA TP 3355, 1993.
- Lee, J.-W., Research on fighter-grade high-reliability virtual flight certification technology 2nd year-end report, 2018.
- Finck, R. D., USAF Stability and Control DATCOM, McDonnel Douglas Corporation, 1978.
- Supplemental Flight Manual, Lockheed Martin Corporation, T.0. GR1F-16CJ-1-1, 1997.
- Nguyen, L. T., Ogburn, M. E., Gilbert, W. P., Kibler, K. S., Brown, P. W. and Deal, P. L., "Simulator Study of Stall/PostStall Characteristics of a Fighter Airplane With Relaxed Longitudinal Static Stability," NASA TP 1538, 1979.
- Berndt, J. S., "JSBSim: An Open Source Flight Dynamics Model in C++," AIAA Modeling and Simulation Technologies Conference and Exhibit, AIAA 2004-4923, August 2004.