Journal of the Korea Institute of Military Science and Technology (한국군사과학기술학회지)

The Korea Institute of Military Science and Technology (한국군사과학기술학회)
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Considerations in Practical Advanced Guidance Law Development

실용적 첨단유도법칙 개발을 위한 고려사항

  • Published : 2002.05.01
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Abstract

Many modern guided weapon systems employ sophisticated target sensors as well as powerful computing systems. Due to such advanced features, they are required to achieve better guidance accuracy, and at the same time other guidance objectives for better weapon effectiveness and survivability. In this paper, we overview some of the technical considerations in such advanced guidance algorithm development, and briefly look at some related research works. More specifically, we discuss impact angle control, time-varying nature of the guidance system, time-to-go estimation, guidance loop stability, effect of autopilot lag and physical limitations in control variables, parasitic paths in guidance loops, etc. We also briefly look at some advanced concepts such as integrated guidance and control loop design, target adaptive guidance, guidance law development based on dual control concept, and terminal evasive maneuver.

Keywords

References

  1. J.Wang and X.Xie, 'A Derivation of Pure Proportional Navigation', Proc. American Control Conf., San Diego, California, pp.3758-3759, Jun. 1999
  2. U.S.Shukla and P.R.Mahapatra, 'The Proportional Navigation Dilemma-Pure or True?', IEEE Trans. Aerosp. Electron Syst., Vol.26, No.2, pp.382-392, Mar. 1990 https://doi.org/10.1109/7.53445
  3. B.S.Kim, J,G.Lee, and HS.Han, 'Biased PNG Law for Impact with Angular Constraint', IEEE Trans. Aerosp. Electron Syst., Vol.34, No.1, pp.277-288, Jan. 1998 https://doi.org/10.1109/7.640285
  4. T.L.Song, S,J.Shin, and H. Cho, 'Impact Angle Control for Planar Engagement', IEEE Trans. Aerosp. Electron Syst., Vol.35, No.4, pp.1439-1444, Oct. 1999 https://doi.org/10.1109/7.805460
  5. 류창경, 조항주, '표적 충돌각과 최대가속도 제한을 고려한 최적유도기법', '92 한국자동제어학술회의 논문집, 서울, pp.601-606, 1992
  6. C.K.Ryoo, H.Cho, and M-J. Tahk, 'Performance Characteristics of Linear Optimal Guidance Laws for Varying Velocity Missiles', Proc. 2nd Asian Control Conf, Seoul, Korea, VoW, pp.395-398, July 22-25, 1997
  7. H.Cho, C.K.Ryoo, and M-J. Tahk, 'Closed Form Optimal Guidance Law for Missiles of Time-Varying Velocity', J. Guid Contr. Dyram, Vol.19, No.5, pp.1017-1022, Sep-Oct. 1996 https://doi.org/10.2514/3.21740
  8. H.Cho, C.K.Ryoo, and M-J. Tahk, 'Implementation of Optimal Guidance Laws Using Predicted Missile Velocity Profiles', J Guid Contr. Dynam, Vol.22, No.4, pp.579-588, July-Aug. 1999 https://doi.org/10.2514/2.4420
  9. M-J,Tahk, C.K.Ryoo, and H.Cho, 'Recursive Time-To-Go Estimation for Homing Guidance', IEEE Trans. Aerosp. Electron Syst., Vol.38, No.1, Jan. 2002
  10. 김을곤, 이용인, '비례항법상수 N에 따른 개루프궤적 및 Time-to-go 특성', 한국항공우주학회지, 제27권, 제4호, pp.115~120, 6, 1999
  11. J.Rusnak, 'Optimal Guidance Laws with Uncertain Time-of-flight', IEEE Trans. Aerosp. Electron Syst, Vol.36, No.2, pp.721-725, Apr. 2000 https://doi.org/10.1109/7.845272
  12. J.-H.Oh and J.-J,Ha, 'Capturability of the 3-Dimensional Pure PNG Law', IEEE Trans. Aerosp. Electron Syst., Vol.35, No.2, pp.491-503, Apr. 1999 https://doi.org/10.1109/7.766931
  13. D.-Y.Rew, M-J.Tahk, and R.Cho, 'Short-Time Stability of Proportional Navigation Guidance Loop', IEEE Trans. Aerosp. Electron Syst: Vol.32, No.3, pp.1107-1115, Jul. 1996 https://doi.org/10.1109/7.532269
  14. P.Gurfil, M.Jodorkovsky, and M. Guelman, 'Neoclassical Guidance for Homing Missiles', J. Guid Contr. Dynam, Vol.24, No.3, pp.452-459, May-Jun. 2001 https://doi.org/10.2514/2.4765
  15. P.Gurfil, M.Jodorkovsky, and M Guelman, 'Design of Nonsaturating Guidance Systems', J Guid Contr. Dynam, Vol.23, No.4, pp.693-700, Jul.-Aug., 2000 https://doi.org/10.2514/2.4585
  16. W.A.Kaufmann, 'Design Issues for Bank-toTum Control', Workshop on Bank-to-Tum Controlled Terminal Homing Missiles, GACIAC PR 85-01, pp.31-55, 19-20 Sep. 1984
  17. 황익호,황태원,'2축 김발 호밍 탐색기를 위한 시선변화율 추정기법', 제어. 자동화, 시스템 공학논문지 게재예정
  18. 김필성, 조항주, 'Time-to-go 추정치를 이용한 근사적 표적적응유도', 제7차 유도무기 학술대회 논문집, 대전, pp.249-253, 1997
  19. T.L.Song, 'Target Adaptive Guidance for Passive Homing Missiles', IEEE Trans. Aerosp. Electron Syst; Vol.33, No.1, pp.312-316, Jan. 1997 https://doi.org/10.1109/7.570794
  20. D.GHull, J,L.Speyer, and D.B.Burris, 'inear-Quadratic Guidance Law for Dual Control of Homing Missiles', J. Guid Contr. Dynam, Vol.13, No.1, pp.137-144, Jan.-Feb. 1990 https://doi.org/10.2514/3.20527
  21. also in Proc. AIAA Guidance, Navigation, and Control Conf., AIAA Paper 87-2381, pp.551-559, 1987
  22. H.-I.Lee, M.-J,Tahk, and B.-C.Sun, 'Practical Dual Control Guidance Using Adaptive Intermittent Maneuver Strategy', J. Guid Contr. Dvnam, Vol.24, No.5, Sep.-Oct., 2001
  23. Technologies for Future Precision Strike Missile Systems(RTO Lecture Series 221), RTO-EN-018, Research and Technology Organization/NATO, 2001
  24. Y.Lipman and J,Shinar, 'Mixed- strategy Guidance in Future Ship Defense', J Guid Contr. Dynam, Vol.19, No.2, pp.334-339, Mar.-Apr, 1996 https://doi.org/10.2514/3.21623
  25. K.Becker, 'Closed-form solution of pure proportional navigation,' IEEE Trans. Aerosp. Electron Syst, Vol.26, No.3, pp.526-533, May 1990 https://doi.org/10.1109/7.106131
  26. 조항주, 'PNG의 항법상수와 이와 관련된 최적제어 문제', '92 한국자동제어학술회의 논문집, 서울, pp.578~583, 1992
  27. D.G.Hull, J.J Radke, and R.E.Mack, 'Timeto-go prediction for homing missiles based on minimum-time intercepts', J. Guidance. Vol. 14, No.5, pp.865-871, Sept-Oct, 1991 https://doi.org/10.2514/3.20725
  28. C.-F.Lin, Advanced Control Systems Design, Prentice Hall, Englewood Cliffs, New Jersey, 1993