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Computation Algorithm for Dynamic Launch Zone of Air-to-Air Missiles

공대공 유도탄의 동적발사영역(DLZ) 산출 알고리듬

  • Received : 2014.06.10
  • Accepted : 2014.08.19
  • Published : 2014.09.01

Abstract

A weapon control algorithm equipped on a fighter is closely related to the mission accomplishment and fighter survivability during engagement. The weapon control algorithm typically provides a pilot the dynamic launch zone(DLZ), the target shoot-down range of air-to-air missiles, in the head-up display(HUD). DLZ is produced by an engagement range computation algorithm. In this paper, the components of DLZ for AIM-9 and AIM-120 air-to-air missiles are introduced. The real-time computation algorithm for DLZ based on the pseudo 6-DOF program is then addressed The operational aspects of DLZ algorithm for the air-to-air missiles to various engagement scenarios is investigated vis simulations.

전투기 탑재용 무장제어 알고리듬은 교전상황에서 전투기의 임무 수행 및 생존과 직결된다. 무장제어 알고리듬은 조종사에게 DLZ라 불리는 표적 격추 가능 범위를 HUD에 전시해 준다. DLZ는 교전거리 계산 알고리듬을 이용하여 생성된다. 본 논문에서는 AIM-9과 AIM-120 공대공 유도탄의 DLZ 구성요소에 대해 소개하였다. 다음으로 가상 6-자유도 실시간 시뮬레이션 프로그램에 기반한 DLZ 산출 알고리듬에 관한 내용을 다루었다. 다양한 교전 시나리오 하에서 공대공 유도탄의 DLZ 산출 알고리듬 운용상의 특징을 시뮬레이션을 통해 조사하였다.

Keywords

References

  1. O. Goteman, K. Smith, and S. Dekker, "HUD with a Velocity(Flight-Path) Vector Reduces Lateral Error During Landing in Restricted Visibility," International Journal of Aviation Psychology, Vol. 17, 2007, pp.91-108. https://doi.org/10.1080/10508410709336939
  2. W. Yang, KODEF Military Aircraft Almanac, Planetmidea, 2008.
  3. S. E. Darland, P. T. Liu, J. F. Engels, and C. M. McSpadden, F-16 A/B Mid-Life Update Production Tape M1 The Pilot's Guide, Lockheed Martin, 1998, pp.125-152.
  4. F. A. Gorg, S. E. Darland, G. L. Kolling, and R. R. Bessire, F-16 A/B Mid-Life Update Production Tape M2 The Pilot's Guide, Lockheed Martin, 2000, pp.29-65.
  5. J. E. Clement, S. E. Darland, J. G. Woods, and A. F. Merrell, F-16 A/B Mid-Life Update Production Tape M3 The Pilot's Guide, Lockheed Martin, 2004 pp.8-18.
  6. J D. Faires, R. L. Burden, and B. Pirtle, Numerical Analysis, 3rd Ed., Brooks/Cole publishing company, 2003, pp.45-51.
  7. J D. Faires, R. L. Burden, and B. Pirtle, Numerical Analysis, 3rd Ed., Brooks/Cole publishing company, 2003, pp.33-38.
  8. B. S. Kim, Y, D, Kim, H, C, Bang, M, J, Tahk, and S, K, Hong, Flight Dynamics and control, Kyungmoon, 2004, pp.57-80.
  9. C. B. Park, Understanding of Flight Dynamics, Kyungmoon, 2004, pp.29-36.
  10. P. Zarchan, Tactical and Strategic Missile Guidance, 5th Ed., Vol. 219, AIAA, Reston VA, 2007, pp.15-21.
  11. W. B. Blake, Missile DATCOM, Air Force Research Laboratory, 1998.
  12. J. M. Sung, B. S. Kim, and B. H. Shin, "Development of a Air-to-Air Missile Simulation Program for the Lethality Evaluation," Journal of KSAS, Vol. 38, No. 3, 2010, pp.288-293. https://doi.org/10.5139/JKSAS.2010.38.3.288
  13. E. L. Fleeman, "Technologies for Future Precision Strike Missile Systems-Missile /Aircraft Integration," Defense Technical Information Center Compilation Part Notice, ADP010957, 2001.
  14. U.S. Air Force, http://www.af.mil/

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