그림 1. 탄도미사일 구성요소 및 비행 단계 Fig. 1. Elements and flight stage of the ballistic missile.
그림 2. 추진단계에서 탄도미사일과 연료탱크간의 변별 시나리오 Fig. 2. Discrimination scenario between ballistic missile and debris at boost phase.
그림 3. 중간단계에서 탄두와 기만체간의 미세운동 Fig. 3. Micro-motion for warhead and decoy at mid-course phase.
그림 4. 탄두와 기만체에 대한 Iff(f′, f)의 예시들[5] Fig. 4. Examples of Iff(f′, f) for warhead and decoy[5].
그림 5. F3를 위한 기저영상 B(f′, f)[5] Fig. 5. Basis image B(f′, f) for F3[5].
그림 6. 종착단계에서 탄도계수추정 알고리즘 및 예시[4] Fig. 6. Algorithm and examples for ballistic factor estimation at terminal phase[4].
그림 7. 제안된 가중치 함수들 Fig. 7. Proposed weight functions.
그림 8. 탄두와 기만체의 CAD 모델들 Fig. 8. CAD models for warhead and decoy.
그림 9. 추진단계에서의 변별 결과 Fig. 9. Discrimination results at boost phase.
그림 10. 중간 및 종착 단계에서의 변별 결과. Fig. 10. Discrimination results at mid-course and terminal phase.
표 1. 탄두, 기만체 및 연료 탱크의 특징 Table 1. Characteristics for warhead, decoy, and debris.
표 2. 탄두와 기만체의 규격[4] Table 2. Specifications for warhead and decoy[4].
표 3. 기동 관련 실험 변수들[4] Table 3. Simulation parameters for maneuver[4].
표 4. 미세운동 관련 실험 변수들 Table 4. Simulation parameters for micro-motion.
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