• Journal of Astronomy and Space Sciences
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• v.22 no.4
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• pp.451-462
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• 2005

Optimal Trajectory Correction Maneuver (TCM) design algorithm has been developed using the B-plane targeting method for future Korean Mars missions. For every-mission phase, trajectory informations can also be obtained using this developed algorithms which are essential to design optimal TCM strategy. The information were computed under minimum requiring perturbations to design Mars missions. Spacecraft can not be reached at designed aim point because of unexpected trajectory errors, caused by many perturbations and errors due to operating impulsive maneuvers during the cruising phase of missions. To maintain spacecraft's appropriate trajectory and deliver it to the designed aim point, B-plane targeting techniques are needed. A software NPSOL is used to solve this optimization problem, with the performance index of minimizing total amount of TCM's magnitude. And also executing time of maneuvers on be controlled for the user defined maneuver number $(1\~5)$ of TCMs. The constraints, the Mars arrival B-plane boundary conditions, are formulated for the problem. Results of this work show the ability to design and analyze overall Mars missions, from the Earth launch phase to Mars arrival phase including capture orbit status for future Korean Mars missions

• Defense and Technology
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• no.3 s.157
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• pp.48-53
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• 1992

개발자는 사용자인 60만 소요군을 위한 무기체계의 인구개발 사업을 수행할 때에 연구개발 초기 단계에서부터 양산배치, 운용단계까지 사용자의 작전운용 및 정비지원 요구사항들을 상세히 분석해야 한다. 그렇게 하기위해서는 소요군의 현재/미래, 작전운용/정비지원 임무, 기상조건, 지형지물 조건, 적의 무기체계, 적의 작전운용/정비지원 조건 등을 개발자가 구체적으로 분석해야만이 개발목표 무기체계의 성능설계와 사용자의 인간공학적 문제인식을 도출할 수 있을 것이다

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2023.11a
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• pp.74-76
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• 2023

해저공간을 인류의 삶의 터전으로 바꾸기 위해서는 거주자의 안전이 반드시 확보되어야 한다. 하지만 해저거주공간에서 발생할 수 있는 재난과 재난 발생 시 이루어지는 피난의 특성에 대해서는 연구가 적다. 그러므로 본 연구에서는 해저거주공간의 재난 및 피난 특성에 관해 연구를 진행한다. 현재 운용 중인 해저거주공간의 사례가 드물어 우선 수중공간에서 장기간 임무를 수행하는 잠수함의 사고 사례와 수중연구실로 운영되고 있는 수중해비타트의 사고 사례를 분석하여 해저거주공간의 재난 및 피난 특성을 도출한다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.19 no.5
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• pp.35-44
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• 2018

The purpose of this study was to derive the factors that affect the development cost and the priority/weight of effectiveness in the pre-development stage of a service robot to estimate the development cost. In particular, the functions of service robots vary according to the field of application, and their prices are not only different but most of them are small-scale production; hence, a cost estimation is necessary. In this research, the factors affecting the service robot development cost in the process of service robot development and adding functions are classified as a functional factor while the factors that affect the entire development cost due to environmental causes, in which the service robot is operated or in the development process, are classified as an adjustment factor. The FGI was conducted to derive the factors and a Delphi survey was conducted among 84 domestic experts to determine the weights of the factors. As a result of the analysis, six functional factors (41 detailed criteria) and five adjustment factors (17 criteria) were derived, the cost weight and rank of the factors were suggested. This study suggests that the development cost of the service robot can be used as a decision-making strategy to select the operation functions in the development process, and can be utilized as an essential tool for the service robot development.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.19 no.11
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• pp.332-337
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• 2018

Aircraft searchlights are used in search or rescue missions when performing night missions, and provide infrared light to keep operations in concealment. During aircraft operation, the infrared ray transmission filter glass for generating infrared rays can break, resulting in problems such as loss of concealment ability and maintenance. In this paper, we describe the procedure for testing the operating conditions of the searchlight when the defect occurs and finding the cause of the defect. We also summarize various methods to improve the cause and process of making the improved filter prototype. In addition, we also describe the results of verifying the performance requirements of the searchlight. As a result of the test and verification, the damage of the filter was improved and the improved filter was applied to the aircraft.

• Journal of the Korean Society for Library and Information Science
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• v.55 no.1
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• pp.231-249
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• 2021

The need for the development of practical manuals for responding to disasters in public libraries has emerged after COVID-19 was confirmed in Korea in January 2020. The library is a social organization directed affected by COVID-19. Therefore, a reasonable and consistent disaster response manual should be developed and used as a guideline for responding to disasters at the library sites. This study aims to derive implications by examining the current situation of public library manuals for both domestic and international. Furthermore, the responses of overseas libraries experiencing major disasters were analyzed and issued to reflect the current domestic situation. As a result of the study, it was suggested that the library's role as a social organization for disaster response should be enhanced, and that disaster experience needs to be implemented, as guidelines, toolkits, and archive.

• Bulletin of the Korean Space Science Society
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• 2009.10a
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• pp.28.3-28.3
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• 2009

과학기술위성 3호는 2007년 6월에 사업착수를 시작하여, 동년 8월 시스템요구사항검토회의(SRR)를 통해 임무 요구사항을 도출하였고, 동년 12월에 시스템기본설계검토회의(SDR)과 2008년 9월 시스템예비설계검토회의(PDR)를 개최하여 시험인증모델(EQM, Engineering& Qualification Model) 제작을 시작하여, 납품을 완료하고 ETB(Engineering Test Bed)상에서 유닛의 기능 시험 및 접속시험, 그리고 환경시험을 수행을 완료하였다. 또한 열구조모델 (STM, Structure and Thermal Model)도 제작을 완료하고 발사환경시험과 열평형 환경시험을 완료하였다. 이와같이 시험인증모델 및 열구조모델에 대한 지상에서의 시험과 검증이 완료된 시험결과를 바탕으로 2009년 9월 상세설계를 완료하고 비행모델 제작에 착수할 예정이다. 이 논문에서는 과학기술위성 3호의 시험인증모델에 대한 시험의 목적, 종류 그리고 검증에 대한 결과 그리고 향후 계획에 대해 발표하고자 한다. 참고로 과학기술위성 3호는 주탑재체인 다목적적외선영상시스템(MIRIS)은 우리 은하계의 근적외선 관측, 우주 배경복사 관측 및 지구 지표면의 적외선 영상 획득을 임무로 하고 있고, 부탑재체인 초소형 영상 분광기(COMIS)는 한반도 지역의 다중 스펙트럼 영상을 획득함으로써 대기관측 및 환경감시의 임무를 가지고 있다.

• Journal of the Korean Society of Propulsion Engineers
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• v.24 no.1
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• pp.17-23
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• 2020

Upper stage of launch vehicle mainly injects a lunar explorer from low earth orbit to the moon at a distance of 380,000 km. In foreign lunar explorer, the upper stage is separated from the explorer after the explorer is injected into the earth-moon transfer trajectory, and the lunar explorer then uses on-board propellant to carry out mid-course correction maneuvers and lunar orbit insertion maneuvers. This study describes a newly presented small liquid upper stage. Using a small liquid upper stage with a wet mass of 2.9 tonnes, the lunar explorer not only can be injected earth-moon transfer trajectory but also can be performed lunar orbit insertion. This study provides acceptable mass range of the lunar explorer and the scope of acceptable mission range also describes based on the launch from Naro Space Center.

• Journal of the Korea Society for Simulation
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• v.23 no.1
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• pp.33-42
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• 2014

In this paper we analyzed the search patterns for the anti-submarine warfare (ASW) surface ships cooperating with ASW helicopters. For this purpose, we modeled evasive motion of a submarine with a probabilistic method. And maneuvers and search actions of ships and helicopters participating in the anti-submarine search mission are designed. And for each simulation scenario, the case where a ship and a helicopter searches a submarine independently according to its optimized search pattern is compared with the case where the search platforms participate in the ASW mission cooperatively. Based on the simulation results, we proposed the reconfigured search patterns that help cooperative ASW surface ships increase the total cumulative detection probability (CDP).

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.7
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• pp.636-645
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• 2012

This paper presented the CanSat competition as one of very small satellite programs for expending the space technology base. The CanSat was compared and characterized with a real satellite and the foreign CanSat competition cases and domestic CanSat development trends were summarized. On the basis of the above information, the organizational structure and function were suggested for domestic CanSat competition and the required technologies, such as satellite, launcher and ground station were described. And also, the prior plan for competition, including mission, education and schedule were suggested.