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

  • 제12권3호
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  • Pages.272-281
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  • 2009
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  • 1598-9127(pISSN)
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  • 2636-0640(eISSN)
한국군사과학기술학회 (The Korea Institute of Military Science and Technology)
권호 표지

SQP와 CEALM 최적화 기법에 의한 대공 방어 유도탄에 대한 3차원 최적 회피 성능 비교

Performance Comparison of 3-D Optimal Evasion against PN Guided Defense Missiles Using SQP and CEALM Optimization Methods

  • 발행 : 2009.06.05
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초록

In this paper, three-dimensional optimal evasive maneuver patterns for air-to-surface attack missiles against proportionally navigated anti-air defense missiles were investigated. An interception error of the defense missile is produced by an evasive maneuver of the attack missile. It is assumed that the defense missiles are continuously launched during the flight of attack missile. The performance index to be minimized is then defined as the negative square integral of the interception errors. The direct parameter optimization technique based on SQP and a co-evolution method based on the augmented Lagrangian formulation are adopted to get the attack missile's optimal evasive maneuver patterns. The overall shape of the resultant optimal evasive maneuver is represented as a deformed barrel-roll.

키워드

참고문헌

  1. P. Zarchan, 'Proportional Navigation and Weaving Targets', Journal of Guidance, Control and Dynamics, Vol. 18, No. 5, pp. 969-974, Sep.-Oct., 1995 https://doi.org/10.2514/3.21492
  2. F. Imado and S. Uehara, 'High-g Barrel Roll Maneuvers Against Proportional Navigation from Optimal Control Viewpoint', Journal of Guidance, Control and Dynamics, Vol. 21, No. 6, pp. 876-881, 1998 https://doi.org/10.2514/2.4351
  3. C. K. Ryoo, I. H. Whang and M. J. Tahk, '3-D Evasive Maneuver Policy for Anti-Ship Missiles Against Close-In Weapon Systems', AIAA Guidance, Navigation and Control Conference, Austin, USA, Aug. 2003
  4. P. Zarchan, Tactical and Strategic Missile Guidance, Fourth Edition, AIAA Progress Series in Astronautics and Aeronautics, Vol. 176, Washington DC, 1998
  5. C. Lawrence, J. L. Zhou and A. L. Tits, User's Guide for CFSQP Version 2.5 : A C Code for Solving(Large Scale) Constrained Nonlinear(Minmax) Optimization Problems, Generating Iterates Satisfying All Inequality Constraints, Institute for Systems Research, University of Maryland, 1997
  6. M. J. Tahk and B. C. Sun, 'Co-evolutionary Augmented Lagrangian Methods for Constrained Optimization', IEEE Transactions on Evolutionary Computation, Vol. 4, No. 2, pp. 114-124, July 2000 https://doi.org/10.1109/4235.850652
  7. J. T. Betts, 'Survey on Numerical Methods for Trajectory Optimization', Journal of Guidance, Control and Dynamics, Vol. 21, No. 2, pp. 193-207, Mar.-Apr., 1998 https://doi.org/10.2514/2.4231
  8. D. G. Hull, 'Conversion of Optimal Control Problems into Parameter Optimization Problems', Journal of Guidance, Control and Dynamics, Vol. 20, No. 1, pp. 57-60, Jan.-Feb., 1997 https://doi.org/10.2514/2.4033
  9. 홍영석, 탁민제, '최적화 프로그램(CEALM과 NPSOL)의 성능 비교', 유도무기 학술대회 논문집, 12권, pp. 59-62, 2003
  10. 최경용, 김종한, 안조영, 탁민제, 'CEALM 최적화기법에 의한 유도비행체A의 조종게인 산출', 유도무기 학술대회 논문집, 11권, pp. 76-79, 2001
  11. C. S. Park and M. J. Tahk, 'A Co-evolutionary Minimax Solver and its Application to Autopilot Design', Proceeding of AIAA Guidance, Navigation and Control Conference, Boston, USA, Aug. 1998