earticle

논문검색

<학술연구>

에너지 소비를 고려한 능동방호체계 발사대의 구동 프로파일 생성 방법 연구

원문정보

Study on the Generation Method of Driving Profiles for Launcher of Active Protection System Considering Energy Consumption

김민주, 백준민, 이혜탄

피인용수 : 0(자료제공 : 네이버학술정보)

초록

영어

The launcher of a hard-kill type APS (Active Protection System) requires rapid and precise driving to aim at incoming threats after detection. High angular acceleration is necessary for rapid driving, which demands high energy consumption. However, the capacity of the capacitor bank and power supply unit is limited due to weight and space constraints. If energy becomes insufficient during continuous operation, the voltage of the capacitor bank can drop below the minimum operating voltage of the drive motor, leading to problems such as torque deficiency. Therefore, it is necessary to determine an allowable angular acceleration that satisfies precision within the available energy and generate a driving profile accordingly. This paper proposes a method for deriving an allowable angular acceleration by analyzing the allowable energy and validates it through simulation. We examined the allowable energy by verifying the charged voltage of the capacitor bank, formulated equations for energy at the point of maximum consumption, and derived an equation for allowable angular acceleration through numerical analysis. By applying the proposed algorithm in simulations, we confirmed that the voltage of the capacitor bank did not drop below the minimum operating voltage of the driving motor during three consecutive operations. Therefore, it is expected that the stability of the APS launcher can be improved by applying the proposed algorithm, and continuous operation with limited performance is anticipated to be possible.

목차

Abstract
1. 서론
2. 본론
2.1. 구동 프로파일 생성 방법
2.2. 최대 소비 에너지 도출
2.3. 곡면 피팅을 통한 허용 각가속도 도출
2.4. 시뮬레이션 검증
3. 결론
후기
References

저자정보

  • 김민주 M.J. Kim. Member, Artillery Systems R&D Center of Hanwha Aerospace
  • 백준민 J.M. Baek. Artillery Systems R&D Center of Hanwha Aerospace
  • 이혜탄 H.T. Lee. Artillery Systems R&D Center of Hanwha Aerospace

참고문헌

    ※ 기관로그인 시 무료 이용이 가능합니다.

    • 4,000원

    0개의 논문이 장바구니에 담겼습니다.