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논문검색

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에너지 소비를 고려한 능동방호체계 발사대의 구동 프로파일 생성 방법 구현과 검증

원문정보

Implementation and Validation of the Generation Method of Driving Profiles for Launcher of Active Protection System Considering Energy Consumption.

김민주

피인용수 : 0(자료제공 : 네이버학술정보)

초록

영어

The launcher of a hard-kill type APS (Active Protection System) requires rapid and precise driving to target approaching threats after detection. High angular acceleration is required for rapid driving, which requires high energy consumption. However, the sufficient energy storage of the APS is limited due to weight and space constraints. If energy is insufficient during driving, the charged voltage of the capacitor bank may drop below the minimum operating voltage of the drive motor, which may result in problems such as torque insufficiency or saturation of the controller's integrator. Therefore, it is necessary to determine the maximum angular acceleration possible within the available energy and generate a corresponding driving profile. This paper proposes a method for calculating allowable energy and deriving allowable maximum angular acceleration for driving profile, and validates the proposed method through experiments. We established and implemented a method for deriving maximum angular acceleration through experimental methods to account for unknown frictional forces and mechanical errors in the launcher. By applying the proposed method, we confirmed that the system can operate at high speeds stably by reflecting appropriate angular acceleration even during continuous operation. Therefore, it is expected that the application of the proposed method will improve the operating stability of the APS launcher and enable continuous operation at maximum speed within limited energy.

목차

Abstract
1. 서론
1.1 논문의 배경
1.2 종래의 연구
1.3 연구의 목적
2. 구동 프로파일 생성 방법의 구현
2.1 구동 프로파일의 생성 방법
2.2 구동 프로파일의 에너지 소비 제한
2.3 구동 프로파일의 구현 전략
2.4 고각의 가속에너지 추정
2.5 허용에너지 연산
2.6 최대각가속도 도출
3. 구동 프로파일 생성 방법의 검증
4. 결론
후기
References

저자정보

  • 김민주 M.J. Kim. Member, Artillery System R&D Center of Hanwha Aerospace

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자료제공 : 네이버학술정보

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