Optimal Hierarchical Design Methodology for AESA Radar Operating Modes of a Fighter
(주)코리아스칼라
- 최초 등록일
- 2024.01.15
- 최종 저작일
- 2023.12
- 13페이지/ 어도비 PDF
- 가격 4,500원
* 본 문서는 배포용으로 복사 및 편집이 불가합니다.
서지정보
ㆍ발행기관 : 한국산업경영시스템학회
ㆍ수록지정보 : 산업경영시스템학회지 / 46권 / 4호
ㆍ저자명 : 김흥섭, 김성호, 장우석, 설현주
목차
1. 서 론
2. 기존 문헌고찰
3. 문제정의
4. 운용모드 배치 최적화 방법론
4.1 운용모드 변경을 위한 HOTAS 조작
4.2 운용모드(기능) 간 전이확률행렬(TPM)
4.3 운용모드 배치 최적화 수리계획모형
5. 수치실험
6. 결론 및 향후 연구방향
Acknowledgements
References
영어 초록
This study addresses the optimal design methodology for switching between active electronically scanned array (AESA) radar operating modes to easily select the necessary information to reduce pilots' cognitive load and physical workload in situations where diverse and complex information is continuously provided. This study presents a procedure for defining a hidden Markov chain model (HMM) for modeling operating mode changes based on time series data on the operating modes of the AESA radar used by pilots while performing mission scenarios with inherent uncertainty. Furthermore, based on a transition probability matrix (TPM) of the HMM, this study presents a mathematical programming model for proposing the optimal structural design of AESA radar operating modes considering the manipulation method of a hands on throttle-and-stick (HOTAS). Fighter pilots select and activate the menu key for an AESA radar operation mode by manipulating the HOTAS’s rotary and toggle controllers. Therefore, this study presents an optimization problem to propose the optimal structural design of the menu keys so that the pilot can easily change the menu keys to suit the operational environment. K
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