DOI QR코드

DOI QR Code

A Requirement Assessment Algorithm for Anti-Ballistic Missile Considering Ballistic Missile's Flight Characteristics

탄도미사일의 비행특성을 고려한 요격미사일 소요 알고리즘

  • Received : 2011.06.20
  • Accepted : 2011.10.21
  • Published : 2011.12.05

Abstract

A Ballistic Missile(BM) is a missile that follows a sub-orbital ballistic flightpath with the objective of delivering one or more wardheads to a predetermined target and An Anti-Ballistic Missile(ABM) is a missile designed to destroy a ballistic missile before reaching its target. The main objective of this study is to assess the requirement of ABM by considering both flight characteristic of the SCUD-B/C, Nodong missiles and intercept performance of ABM in the Lower tier Ballistic Missile Defense(BMD). The Ballistic Missile's flight characteristics, such as trajectory, velocity etc., are estimated by simulation using the physical motion equations. The requirement of ABM is calculated by evaluating whether the BMD forces can defend those when the ballistic missiles attack prime facilities.

Keywords

References

  1. 권용수, "유도무기체계", 국방대학교, 2001. 1.
  2. 권용수, "탄도미사일 위협과 방어체계", 국방대학교, 2003. 12.
  3. 권용수, 최봉석, "탄도미사일의 비행궤적 특성 해석", 한국국방경영분석학회지 제32권, 제1호, 2006. 6.
  4. 김영호, "탄도미사일 방어 : 현황과 한국의 선택", 국제정치논총, 제50집, 제5호, pp. 155-156, 2010.
  5. 김정희, "TBM 비행궤적 해석을 통한 하층방어 센서체계 요구사항 도출에 관한 연구", 국방대학교 석사학위논문, 2009. 12.
  6. 방위사업청, "차기유도무기(SAM-X) 시험평가 결과", 2007. 2.
  7. 아시아경제, "[정치]북 미사일잡기 나선 한국형방어체계는", 2010. 10. 25.
  8. 연합뉴스, "미정보당국 '북, 대포동2호 시험발사할 것'", 연합뉴스, 2011. 3. 11.
  9. 조옥찬, "우주비행역학", 경문사, pp. 151-170, 1984.
  10. 황재훈, "美 '北, ICBM 관련기술 실험 다수성공'", 연합뉴스, 2011. 2. 17.
  11. YTN, "현인택, '북한 핵무기 6-10개 보유 추정'", 2011. 4. 7.
  12. David C. Wright et al., "An Analysis of the North Korean Nodong Missile", Science & Global Security, Vol. 4, p. 132, 1994.

Cited by

  1. A Study on Radar Received Power based on Target Observing Position vol.18, pp.12, 2014, https://doi.org/10.6109/jkiice.2014.18.12.3063
  2. A Study on the Optimal Allocation of Korea Air and Missile Defense System using a Genetic Algorithm vol.18, pp.6, 2015, https://doi.org/10.9766/KIMST.2015.18.6.797
  3. Analysis of Flight Trajectory Characteristics of Ballistic Missiles Considering Effects of Drag Forces vol.20, pp.2, 2016, https://doi.org/10.12673/jant.2016.20.2.134
  4. Analysis of Flight Trajectory Characteristics of the MRBM by Adjusting the Angle of a Flight Path vol.18, pp.2, 2015, https://doi.org/10.9766/KIMST.2015.18.2.173
  5. Method on Radar deployment for Ballistic Missile Detection Probability Improvement vol.20, pp.3, 2016, https://doi.org/10.6109/jkiice.2016.20.3.669
  6. Analysis of the Flight Trajectory Characteristics of North Korea SLBM vol.24, pp.3, 2015, https://doi.org/10.9709/JKSS.2015.24.3.009
  7. Prediction of Possible Intercept Time by Considering Flight Trajectory of Nodong Missile vol.3, pp.2, 2016, https://doi.org/10.20910/IJASE.2016.3.2.14
  8. RCS of Ballistic Missile Based on Radar Position vol.40, pp.1, 2015, https://doi.org/10.7840/kics.2015.40.1.209
  9. Analysis of the flight trajectory characteristics of North Korea SLBM due to launching mode vol.07, pp.04, 2016, https://doi.org/10.1142/S1793962316430054
  10. Performance Analysis of the Discrimination between Space-targets Using the Maneuvering vol.15, pp.11, 2017, https://doi.org/10.14801/jkiit.2017.15.11.55
  11. Extended Target State Vector Estimation using AKF vol.43, pp.6, 2015, https://doi.org/10.5139/JKSAS.2015.43.6.507