RISS 학술연구정보서비스

검색

인기 검색어

    다국어 입력

    http://chineseinput.net/에서 pinyin(병음)방식으로 중국어를 변환할 수 있습니다.

    변환된 중국어를 복사하여 사용하시면 됩니다.

    예시)
    • 中文 을 입력하시려면 zhongwen을 입력하시고 space를누르시면됩니다.
    • 北京 을 입력하시려면 beijing을 입력하시고 space를 누르시면 됩니다.
    닫기
    KCI등재

    평형 편주각 기반 수정질점탄도모델의 탄도 보정계수 산정 = Fitting Factor Estimation for the Yaw of Repose Based Modified Point-Mass Trajectory Model

    한글로보기

    https://www.riss.kr/link?id=A110340661

    • 0

      상세조회
    • 0

      다운로드
    서지정보 열기
    • 내보내기
    • 내책장담기
    • 공유하기
    • 오류접수

    부가정보

    다국어 초록 (Multilingual Abstract) kakao i 다국어 번역

    This study presents a fitting factor calibration method to enhance the accuracy and consistency of STANAG 4355 Modified Point-Mass Model trajectory simulations. Conventional approaches, typically based on Mach number or quadrant elevation, focus on matching only the impact range, whereas the proposed method fits the entire trajectory shape, including the maximum ordinate and its corresponding range at the trajectory apex. A new fitting scheme incorporating the yaw of repose and projectile velocity is introduced to reflect aerodynamic influences during flight. Calibration is performed using an interior-point optimization minimizing discrepancies with reference firing-table data, with the objective function explicitly considering four trajectory features: range, lateral deviation, and the altitude and corresponding distance at the trajectory apex. Validation results demonstrate that the proposed model significantly improves trajectory representation and impact accuracy compared with conventional methods, providing a more reliable and consistent simulation framework for future projectile system development.
    번역하기

    This study presents a fitting factor calibration method to enhance the accuracy and consistency of STANAG 4355 Modified Point-Mass Model trajectory simulations. Conventional approaches, typically based on Mach number or quadrant elevation, focus on ma...

    This study presents a fitting factor calibration method to enhance the accuracy and consistency of STANAG 4355 Modified Point-Mass Model trajectory simulations. Conventional approaches, typically based on Mach number or quadrant elevation, focus on matching only the impact range, whereas the proposed method fits the entire trajectory shape, including the maximum ordinate and its corresponding range at the trajectory apex. A new fitting scheme incorporating the yaw of repose and projectile velocity is introduced to reflect aerodynamic influences during flight. Calibration is performed using an interior-point optimization minimizing discrepancies with reference firing-table data, with the objective function explicitly considering four trajectory features: range, lateral deviation, and the altitude and corresponding distance at the trajectory apex. Validation results demonstrate that the proposed model significantly improves trajectory representation and impact accuracy compared with conventional methods, providing a more reliable and consistent simulation framework for future projectile system development.

    더보기

    동일학술지(권/호) 다른 논문

    분석정보

    View

    상세정보조회

    0

    Usage

    원문다운로드

    0

    대출신청

    0

    복사신청

    0

    EDDS신청

    0

    동일 주제 내 활용도 TOP

    더보기

    주제

    연도별 연구동향

    연도별 활용동향

    연관논문

    연구자 네트워크맵

    공동연구자 (7)

    유사연구자 (20) 활용도상위20명

    이 자료와 함께 이용한 RISS 자료

    나만을 위한 추천자료

    해외이동버튼