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참고문헌 (19)

1. Choi, K., Jin, J., Tahk, M., Yoon, S., and Byun, W., "An Optimization Technique for the Aero- dynamic Configuration Design of Guided Missile Systems," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 21, No. 3, 1993, pp.98-107. 

2. Yang, Y., et al., "An External Shape Optimization Study to Maximize the Range of a Guided Missile in Atmospheric Flight," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 37, No. 6, 2009, pp.519-526. 

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3. Bae, H., et al., "500 lbs-class Air-to-Surface Missile Design by Integration of Aerodynamics and RCS," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 40, No. 2, 2012, pp.184-191. 

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4. Kim, H., and Chang, Y., "Multidisciplinary Design Optimization of Earth Observation Satellite Conceptual Design Using Collaborative Optimization," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 43, No. 6, 2015, pp.568-583. 

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5. Park, K., et al., "Multidisciplinary Design Optimization of a Medium-Sized Solar Powered HALE UAV Considering Energy Balancing," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 40, No. 2, 2012, pp.129-138. 

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6. Lee, H., et al., "Analysis of Development Methods for a Multidisciplinary Design Optimization Framework," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 36, No. 10, 2008, pp.947-953. 

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7. Lee, S., et al., "Multidisciplinary Design and Optimization of Cruise Missile with Considering Survivability," Proceeding of The Korean Society for Aeronautical and Space Sciences Spring Conference, April 2007, pp.407-411. 

8. Choi, Y., Lee, J., and Byun, Y., "Optimal Supersonic Air-Launching Rocket Design Using Multidisciplinary System Optimization Approach," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 33, No. 12, 2005, pp.26-32. 

9. Ahuja, V., and Hartfield, R., "Optimization of Combined Rocket and Ramjet/Scramjet Ballistic Missile Designs," Journal of Propulsion and Power, Vol. 31, No. 6, 2015, pp.1544-1550. 

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10. Riddle, D., Hartfield, R., Burkhalter, J., and Jenkins, R., "Genetic Algorithm Optimization of Liquid Propellant Missile Systems," Journal of Spacecraft and Rockets, Vol. 46, No. 1, 2009, pp.151-159. 

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11. Villanueva, F., Linshu, H., and Dajun, X., "Small Solid Propellant Launch Vehicle Mixed Design Optimization Approach," Journal of Aerospace Technology and Management, Vol. 6, No. 3, 2014, pp.291-300. 

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12. Zakeri, M., Nosratollahi, M., and Novinzade, A., "Multi-Disciplinary System Design Optimization of a Launch Vehicle Upper-Stage," Journal of Aerospace Technology and Management, Vol. 9, No. 1, 2017, pp.49-62. 

13. http://missile.index.ne.jp/en 

14. http://missilethreat.csis.org/ 

15. Fleeman, E., Missile Design and Systems Engineering, AIAA Education, 2013. 

16. Nelson, R., Flight Stability and Automatic Control (2nd Ed.), McGraw Hill, 1998, p.48. 

17. Blakelock, J., Automatic Control of Aircraft and Missiles (2nd Ed.), John Wiley & Sons, 1991, p.66, p.92. 

18. Sobieszczanski-Sobieski, J., Morris, A., and Tooren, M. V., Multidisciplinary Design Optimization Supported by Knowledge Based Engineering, John Wiley & Sons, 2015, pp.98-115. 

19. Jung, J., et al., "Conceptual Design of a Reusable Unmanned Space Vehicle Using Multidisciplinary Optimization," International Journal of Aeronautical and Space Sciences Vol. 19, No. 3, 2018, pp.743-750. 

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