$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

유도무기 임무 분석을 위한 레이더 성능 모델
A Radar Performance Model for Mission Analyses of Missile Models 원문보기

韓國軍事科學技術學會誌 = Journal of the KIMST, v.20 no.6, 2017년, pp.822 - 834  

김진규 (국방과학연구소 제1기술연구본부) ,  우상효 (국방과학연구소 제1기술연구본부)

Abstract AI-Helper 아이콘AI-Helper

In M&S, radar model is a software module to identify position data of simulation objects. In this paper, we propose a radar performance model for simulations of air defenses. The previous radar simulations are complicated and difficult to model and implement since radar systems in real world themsel...

주제어

AI 본문요약
AI-Helper 아이콘 AI-Helper

* AI 자동 식별 결과로 적합하지 않은 문장이 있을 수 있으니, 이용에 유의하시기 바랍니다.

제안 방법

  • For the future works, we plan to define functionality of seeker performance model in our missile behavior model. At the conclusion, we design and implement the seeker model in M&S that is completely operated by measured performance data in real world like our radar performance model in this paper.
  • First, the calculations of azimuth, elevation and slant range are obtaining relative azimuth, elevation, and distances from our radar position to a target position in 3 dimensions. Equation (1) shows expressions for a relative azimuth angle from the radar To a target.
  • In this paper, we focused on radar systems for air defenses, and we attempted to design our radar performance model to be a simple model and feasible to visual verifications. In the design of our radar model, we have carried out reducing gaps between simulation data and real world data in mission level analyses of our missile model.
  • 6 illustrates the processes of our radar model. The objective of the radar model is to obtain a data set: observed longitude, latitude and altitude of a target at current simulation time. The radar performance model consists of seven phases in two calculations, two computations, and three models; ① Azimuth, Elevation, and Slant Range Calculation, ② Real RCS Computation,③ Detection Range Computation, ④ Azimuth and Elevation Coverage Calculation, ⑤ RCS Estimation Model, ⑥ Line Of Sight Model, and ⑦ Longitude Latitude and Altitude Estimation Model.
  • The objective of the radar model is to obtain a data set: observed longitude, latitude and altitude of a target at current simulation time. The radar performance model consists of seven phases in two calculations, two computations, and three models; ① Azimuth, Elevation, and Slant Range Calculation, ② Real RCS Computation,③ Detection Range Computation, ④ Azimuth and Elevation Coverage Calculation, ⑤ RCS Estimation Model, ⑥ Line Of Sight Model, and ⑦ Longitude Latitude and Altitude Estimation Model. The calculation means an acquisition of values with a single equation.
  • In this phase, the radar model calculates minimum azimuth/elevation angles and maximum azimuth/elevation angles at current simulation time according to its scan time. Then, the model determines whether a target is in its coverages with relative azimuth and elevation to the target, resulted from azimuth, elevation, and slant range calculation phase. In the following three subsections, we discuss the remaining three models in our radar model.
  • Therefore, in this paper, we transform these complex radar systems into a simple model for analyzing mission planning results of our missile models based on time and spatial domains. In the following section, we will discuss the design solutions of our simple radar model.
  • With those results, we could compare them in views of RCS exposure time, RCS fluctuation, and average of slant range error. In other words, we can conclude thaTLess RCS exposure time is the most proper mission planning result in our missile model.
본문요약 정보가 도움이 되었나요?

참고문헌 (11)

  1. Jingyu Kim, "Design of the Radar Performance Model for Mission analyses of Missile Models," KIMST Fall Conference Proceedings, pp. 447-448, 2016. 

  2. Jingyu Kim, “HLA/RTI based on the Simulation Composition Technology,” Journal of the KIMST, Vol. 19, No. 2, pp. 244-251, 2016. 

  3. BAE SYSTEMS, SADM-AE USER'S Guide, Vol. 1: Theory, Australia Ltd. 2012. 

  4. Bassem R. Mahafza, Radar System Analysis and Design Using MATLAB, CHAPMAN & HALL/CRC, 2000. 

  5. Sandwell, David T., Reference Earth Model-WGS84, 2002(accessed via topex.ucse.edu/geodynamics/). 

  6. U. S. Naval Research Laboratory, SIMDIS User Manual. Visualization System Integration Section. Code 5773, 2012. 

  7. The MathWorks, Mapping Toolbox For Use with MATLAB, User's Guide Version 2, The MathWorks Inc., 2004. 

  8. Roger Aarenstrup, Managing Model-Based Design, The MathWorks Inc, 2015. 

  9. M. D. Pretty, R. W. Franceschini, J. Panagos, "Multi-Resolution Combat Modeling," In Engineering Principles of Combat Modeling and Distributed Simulation, Edited by A. Tolk, pp. 607-640, John Wiley & Sons, 2012. 

  10. Morris R. Driels, "Introduction to Statistical Methods," In Weaponeering Conventional Weapon System Effectiveness, Second Edition, America Institute of Aeronautics and Astronautics(AIAA), 2013. 

  11. Teledyne Brown Engineering Inc., User's Manual EXTENTED AIR DEFENSE SIMULATION (EADSIM), Ver. 16.00, 2010. 

저자의 다른 논문 :

섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트

맨위로