참고문헌 (25)

1. Sci Glob Secur P Zarchan 8 1 1999 10.1080/08929889908426470 Zarchan P (1999) Ballistic missile defense guidance and control issues. Sci Glob Secur 8:1 

   상세보기

2. Rev Modern Phys DK Barton 76 1307 2004 10.1103/RevModPhys.76.1307 Barton DK, Falcone R, Kleppner D, Lamb FK, Lau MK, Lynch HL, Moncton D, Montague D, Mosher DE, Priedhorsky W, Tigner M, Vaughan DR (2004) Report of the American physical society study group on boost-phase intercept systems for national missile defense: scientific and technical issues. Rev Modern Phys 76:1307 

   상세보기

3. 10.1109/CGNCC.2014.7007325 Zhang X, Lei H, Li J, Zhang DY (2014) Ballistic missile trajectory prediction and the solution algorithms for impact point prediction. In: Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference, Yantai, China 

   

4. Control Eng Pract EJ Song 6 8 41 1998 10.1016/S0967-0661(98)00041-0 Song EJ, Tahk MJ (1998) Real-time midcourse guidance with intercept point prediction. Control Eng Pract 6(8):41 

   상세보기

5. Aerosp Sci Technol O Montenbruck 6 962 2002 Montenbruck O, Markgraf M, Jung W, Bull B, Engler W (2002) GPS based prediction of the instantaneous impact point for sounding rockets. Aerosp Sci Technol 6:962 

6. 10.2514/6.2003-5722 Markgraf M, Montenbruck O, Turner P, Viertotak M (2003) Tracking system with onboard IIP prediction for sounding rockets, AIAA Guidance, Navigation, and Control Conference and Exhibit, Austin, TX. AIAA Paper 2003-5722. 

   

7. J Guidan Control Dyn J Ahn 25 2 2012 Ahn J, Roh WR (2012) Noniterative instantaneous impact point prediction algorithm for launch operations. J Guidan Control Dyn 25:2 

8. Zarchan P (2002) Tactical and strategic missile guidance, Vol. 199, Progress in astronautics and aeronautics, AIAA, Reston 

9. J Guid Control Dyn IS Jeon 33 136 2010 10.2514/1.40136 Jeon IS, Lee JI, Tahk MJ (2010) Homing guidance law for cooperative attack of multiple missiles. J Guid Control Dyn 33:136 

   상세보기

10. 10.3182/20110828-6-IT-1002.02304 Kim TH, Lee CH, Tahk MJ (2011) Time-to-go polynomial guidance laws with terminal impact angle acceleration constraints. Proceedings of the 18th IFAC World Congress, Milano 

    상세보기

11. J Guid Control Dyn CH Lee 36 5 2013 Lee CH, Kim TH, Tahk MJ (2013) Interception angle control guidance using proportional navigation with error feedback. J Guid Control Dyn 36:5 

12. IEEE Trans Aerosp Electron Syst MJ Tahk 38 1 2002 Tahk MJ, Ryoo CK, Cho H (2002) Recursive time-to-go estimation for homing guidance missiles. IEEE Trans Aerosp Electron Syst 38:1 

13. Whang IH, Ra WS (2008) Time-to-go estimator for missiles guided by BPNG. In: Proceedings of IEEE International Conference on control, automation and systems, IEEE Publ., Piscataway, NJ. 

14. 10.1109/CDC.2013.6760652 Ghosh S, Ghose D, Raha S (2013) Three dimensional retro-PN based impact time control for higher speed nonmaneuvering targets. In: Proceedings of the IEEE Conference on Decision and Control, IEEE Publ., Piscataway, NJ 

    

15. J Guid Control Dyn N Dhananjay 37 4 2014 10.2514/1.G000082 Dhananjay N, Ghose D (2014) Accurate time-to-go estimation for proportional navigation guidance. J Guid Control Dyn 37:4 

    상세보기

16. J R Stat Soc Ser B G Box 13 1 1951 10.1111/j.2517-6161.1951.tb00067.x Box G, Wilson K (1951) On the experimental attainment of optimum conditions. J R Stat Soc Ser B 13:1 

    상세보기

17. J Guid Control Dyn J Ahn 35 2 645 2012 10.2514/1.56395 Ahn J, Seo J (2012) Instantaneous impact point prediction using the response surface method. J Guid Control Dyn 35(2):645-648 

    상세보기

18. AE Bryson 1975 Applied optimal control: optimization, estimation and control Bryson AE (1975) Applied optimal control: optimization, estimation and control. CRC Press, Boca Raton 

19. IEEE Trans Evol Comput MJ Tahk 4 2 114 2000 10.1109/4235.850652 Tahk MJ, Sub BC (2000) Coevolutionary augmented Lagrangian methods for constrained optimization. IEEE Trans Evol Comput 4(2):114-124 

    상세보기

20. JY Lee 2015 Parameter optimization of multistage missile for terminal velocity maximization Lee JY, Hong SM, Kim YW, Tahk MJ (2015) Parameter optimization of multistage missile for terminal velocity maximization. Asia-Pacific International Symposium on Aerospace Technology, Engineers Austrailia 

21. 10.1007/s42405-019-00224-y Hong SM, Tahk MJ, Lee CH (2019) Stage optimization of anti-air missiles using practical guidance laws. Int J Aeronaut Sp Sci, 1-10. 

    상세보기

22. Int J Sports Sci Eng PS Chudinov 5 1 27 2011 Chudinov PS (2011) Approximate analytical investigation of projectile motion in a medium with quadratic drag force. Int J Sports Sci Eng 5(1):27-42 

23. IFAC-PapersOnLine S Han 49 17 40 2016 10.1016/j.ifacol.2016.09.008 Han S, Hwang MC, Lee BY, Ahn J, Tahk MJ (2016) Analytic solution of projectil motion with quadratic drag and unity thrust. IFAC-PapersOnLine 49(17):40-45 

    상세보기

24. 10.1109/TAES.2013.6621856 Kim TH, Lee CH, Jeon IS, Tahk MJ (2013) Augmented polynomial gduiacne with impact time and angle constraints. IEEE Transactions on aerospace and electronics systems, Vol. 49, No. 4. 

    상세보기

25. 10.1177/0954410016664928 Seo MG, Tahk MJ (2017) Suboptimal mid-course guidance algorithm for accelerating missiles. In: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 31(11) 

    상세보기

활용도 Top5 논문

더보기

해당 논문의 주제분야에서 활용도가 높은 상위 5개 콘텐츠를 보여줍니다.
더보기 버튼을 클릭하시면 더 많은 관련자료를 살펴볼 수 있습니다.