• 대한전기학회
Mobile QR Code QR CODE : The Transactions of the Korean Institute of Electrical Engineers
  • COPE
  • kcse
  • 한국과학기술단체총연합회
  • 한국학술지인용색인
  • Scopus
  • crossref
  • orcid
The Transactions of the Korean Institute of Electrical Engineers

The Transactions of the Korean Institute of Electrical Engineers

ISO Journal TitleTrans. Korean. Inst. Elect. Eng.
SCImago Journal & Country Rank

Journal Search

  1. Home
  2. Archive
  3. 2024-07 (Vol.73 No.07)
  4. 10.5370/KIEE.2024.73.7.1220
XML PDF INFO REF

References

1 
B. E. Jeon, and C. H. Song, "Control Technology of Missile“, Journal of The Korean Society for Aeronautical and Space Sciences, pp.178-183, 1997.URL
2 
B. A. While, and A. Tsourdos, “Modern missile guidance design: An overview,” Proceedings of IFAC, vol. 34, no. 15, pp.431-436, 2001.DOI
3 
F. W. Nesline, and N. C. Nabbefeld,, "Design of Digital Autopilots for Homing Missiles", Proceedings of AGARD Conference, pp.1-14, 1979.URL
4 
F. W. Nesline, and M. L. Nesline,, "How Autopilot Requirements Constrain the Aerodynamic Design of Homing Missiles", Proceedings of American Control Conference, pp. 716-730, 1984.DOI
5 
M. P. Horton, "Autopilot for Tactical Missiles: An overview", Proceedings of the Institution of Mechanical Engineers, Part 1: Journal of Systems and Control Engineering, vol. 209, no. 2, pp. 127-139, 1995.DOI
6 
F. W. Nesline, B. H. Wells, and P. Zarchan, "A Combined Optimal/Classical Approach to Robust Missile Autopilot Design", Journal of Guidance, Control, and Dynamics, vol 4, no. 3, 1981.URL
7 
F. W Nesline, and P. Zarchan, "Why Modern Controllers Can Go Unstable in Practice", AIAA Guidance and Control Conference, vol. 7, no. 4, pp. 495-500, 1984.DOI
8 
Y. S. Kim, and S. H. Kim, "Study of Missile Aerodynamic Characteristics with Three Loop Acceleration Autopilot Structure", Journal of Institute of Control, Robotics and Systems, vol. 8, no. 8, 2002.DOI
9 
C. P. Mracek, and D. B. Ridgely,, "Missile Longitudinal Autopilots: Comparison of Multiple Three Loop Topologies", AIAA Guidance, Navigation, and Control Conference and Exhibit, 2005.DOI
10 
D. Hwang, and M. J. Tahk,, "The Inverse Optimal Control Problem for Three-Loop Missile Autopilot," International Journal of Aeronautical & Space Sciences, vol. 19, pp. 411-422, 2018.DOI
11 
C. P. Mracek, and D. B. Ridgely, "Optimal Control Solution for Dual(Tail and Canard) Controlled Missiles", AIAA Guidance, Navigation, and Control Conference and Exhibit, 2006.DOI
12 
K. H. Im, D. Chwa, and J. Y. Choi, "Multi-Input Multi-Output Nonlinear Autopilot Design for Ship-to-Ship Missiles", International Journal of Control, Automation, and Systems vol. 4, no. 2,, pp. 255-270, 2006.URL
13 
J. H. Yeom, S. H. Song, J. W. Hong, and I. J. Ha, "Singular Perturbationlike Approach to Compensation of Actuator Dynamics Effect in Missile Control", IEEE Transactions on Aerospace and Electronic Systems, vol. 50, no. 4, 2014.DOI
14 
S. H. Kim, Y. S. Kim, and C. Song, "A Robust Adaptive Nonlinear Control Approach to Missile Autopilot Design", Control Engineering Practice vol. 12, no. 2, pp. 149-154, 2004.URL
15 
P. S. Sastry, S. K. Ray, and G. M. Gao, "Comparative Account of Robust $H_{\infty}$ Techniques for Missile Autopilot Design", International Journal of Image, Graphics, and Signal Processing, vol. 11, no. 4, pp. 26-41, 2019.URL
16 
J. H. Blakelock, Automatic Control of aircraft and missiles, John Wiley & Sons, pp. 17-26, 1991.URL
17 
S. S. Chin, Missile Configuration Design, McGraw Hill Book Company, 1961.URL
18 
D. Moerder, and A. Calise, "Convergence of a Numerical Algorithm for Calculating Optimal Output Feedback Gain", IEEE Transactions on Automatic Control,, vol. 30, no. 9, pp. 900-903, 1985DOI
19 
C. H. Lee, S. He, and J. H. Hong, “Investigation on Physical Meaning of three-loop Autopilot”, International Journal of Control, Automation and Systems vol. 18, pp. 2709-2720, 2020.DOI