• Defense and Technology
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• no.10 s.224
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• pp.76-87
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• 1997

박격포는 성능과 전술적 관점에서 20세기말에 괄목할만한 발전을 하고 있다. 대구경화 및 사거리 신장, 신소재에 의한 경량화, 스마트탄 개발, 신관 및 유탄의 개발, 차량 탑재화로 신속한 기동, 사격통제시스템의 발전 등으로 시험사격 없이 초탄에 바로 정확한 효력사를 발사할 수 있으며, 미리 선정된 사격진지로 포탑화 장갑 박격포 시스템으로 신속한 기동이 가능하다.

• Aerospace Engineering and Technology
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• v.7 no.1
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• pp.229-235
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• 2008

The ground flight termination system(GFTS) could be used for the termination of launch vehicle in flight motion when the launch vehicle deviates from the designated route due to the system malfunction or failure as well as the launch vehicle can't be tracked by the ground tracking system. This paper introduces the basic concept and design of the ground flight termination system to be used for KSLV launch mission in NARO space center. In order to design the optimal ground flight termination system for KSLV launch application, the operational concept reflected on the flight trajectory and system characteristics of KSLV launch vehicle should be considered. Moreover the RF link budget analysis, and the analysis for system availability and reliability are done. Based on the analysis above, the each subsystem of ground flight termination to transmit the termination signal in stable is designed for KSLV launch mission.

• Proceedings of the KIEE Conference
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• 2001.11c
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• pp.327-330
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• 2001

본 논문에서는 위험요소를 내재하고 있는 로켓시스템에 대해 원거리에서 실시간 모니터링 및 제어를 할 수 있도록 원격 제어시스템을 설계, 개발하였다. 뿐만 아니라 로켓 근처에 위치한 무인 시설물 내에는 원격제어에 따른 로켓내부 시스템의 각종 센서 출력값을 멀티채널방식을 이용하여 장시간에 걸쳐 저장하고 원격지에 위치한 유인 시설물 내에서 LAN 통신을 통해 데이터를 분석할 수 있도록 DAS(Data Acquisition System)을 설계하고 개발하였다. 개발된 시스템은 간이 연계시험을 통해 입증하였으며, 향후 3단형 과학로켓발사통제시스템에 적용할 예정이다.

• Journal of Aerospace System Engineering
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• v.10 no.4
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• pp.59-66
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• 2016

India and China are capable of developing indigenous space launch vehicles, with the rocket technology transferred from the U.S., Western countries, and the Soviet Union, in the 1950s and 1960s. Barring the early 1990s, both countries are absent in the missile nonproliferation regime, and have no major space cooperation records with the U.S., since the establishment of the Missile Technology Control Regime in 1987. With the advent of the $21^{st}$ century, historic progress has been made in the U.S.-India space cooperation, which includes using Indian launch vehicles to launch U.S.non-commercial satellites. However, the U.S. is skeptical with regards to space cooperation and using Chinese space launch vehicle services. In this paper, we present the U.S. nonproliferation policy applied on launch vehicles of India and China, and different aspects of the policy will be examined to draw implications on Korean space activities.

• Journal of Korea Society of Industrial Information Systems
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• v.19 no.6
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• pp.53-61
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• 2014

For monitoring the flight trajectory and the status of a launch vehicle, the mission control system in NARO space center process data acquired from the ground tracking system, which consists of two tracking radars, four telemetry stations, and one electro-optical tracking system. Each tracking unit exhibits its own tracking error mainly due to multi-path, clutter and radio refraction, and by utilizing only one among transmitted informations, it is not possible to determine the actual vehicle trajectory. This paper presents a way of generating flight trajectory via post-processing the data received from the ground tracking system. The post-processing algorithm is divided into two parts: compensation for atmosphere radio refraction and multi-sensor fusion, for which a decentralized Kalman filter was adopted and implemented based on constant acceleration model. Applications of the present scheme to real data resulted in the flight trajectory where the tracking errors were minimized than done by any one sensor.

• Current Industrial and Technological Trends in Aerospace
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• v.5 no.2
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• pp.98-106
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• 2007

한 나라의 우주개발은 막대한 예산과 많은 시간이 소요되기 때문에 정부주도로 연구개발사업을 시작하는 것이 대체적인 선례이다. 하지만 때로는 우주개발을 지역사회나 주변 국가들과의 상황에 따라 생존을 위한 방편으로도 활용될 수 있다. 이러한 우려를 불식시키거나 완화하자는 차원에서 국제사회가 다자간 협의체인 미사일기술통제체제(MTCR, Missile Technology Control Regime)을 1987년부터 시작하여 매년 총회 및 회기간 회의를 통하여 국제사회에서 대량파괴무기의 운반체로 미사일이나 무인항공기 등과 관련된 시스템 및 부품 등의 기술이전 등에 관하여 규제를 하고 있는 것이다. 최근 국제사회에서 핵 프로그램 및 미사일 문제로 논쟁의 핵심이 되고 있는 이란에 대하여 우주개발과 미사일기술통제체제의 규제 등의 관점에서 본 논문을 검토하고자 한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.12
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• pp.1207-1215
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• 2008

Satellite generates a complex electromagnetic noise by conducted and radiated coupling effect of the various electrical instruments. This noise may cause serious problems on the satellite system. To minimize the electromagnetic coupling effects and maintain the system safety margin, system noise reduction technique should be applied from the beginning of the system design. The COMS system is evaluated by measuring the conducted noise on system electrical power leads at PSR(Power Supply Regulator) and verifying a 6 dB system safety margin under the complex noise environment with current injection. The radiated noise due to the complex transmit antenna configuration is evaluated by integrating all unit-level RE measurement results, and the RF compatibility between spacecraft and launch vehicle is analyzed with the above estimations. This paper describes the COMS EMC compatibility analysis with respect to each unit level EMC test results, and RF compatibility analysis between spacecraft and launch vehicle. The analyzed results will be reflected on FM(Flight Model) EMC test.

• Defense and Technology
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• no.3 s.121
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• pp.52-61
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• 1989

화력장비혁명의 내용을 알려면 단순히 정밀유도무기나 레이저 유도무기군만을 볼것이 아니라 전반적인 화력장비 차원에서의 잠재력을 살펴야 한다. 화력장비의 성능은 감시능력, 목표식별, 목표포착, 발사계획 및 조종통제, 파괴력 그리고 각 구성체계간의 신뢰성 있는 통신 능력에 달려있다. 이러한 기반위에서 각 요소들은 계속 기술적으로 발전하고 있다. 우리는 컴퓨터나 발전된 통신기술에 의해서 우선적으로 가능하게 된 자동전투관리시스템(ABMS)의 발전을 생각해야 한다

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2012.05a
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• pp.468-471
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• 2012

This paper describes a construction scheme of hot backup or triple modular redundancy control system in a ground hot-firing test facility to carry out performance assessment of propulsion system used in a space launch vehicle. It was possible for a hot backup redundancy control system with manual operated console to simulate TMR control system. A console layout of control system in control center to restrict imprudent works of operators was proposed.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.25 no.3
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• pp.311-318
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• 2014

Electromagnetic compatibility(EMC) performance of the first Korea space launch vehicle(KSLV-I) should be ensured and verified in order to guarantee the normal operation among the spacecraft, ground facilities which are installed in the space center, and other wireless communication networks. For the purpose of the EMC performance verification, pertinent EMC test specifications, methods, and procedures for both the subsystems and the system should be established in consideration of operational properties and electromagnetic environmental effects. And it is required to maintain and control the EMC properties consistently in accordance with the determined specifications up to the program closing phase. In this paper, sequential management work conducted during the overall development process of the KSLV-I is explained, and not only the phased EMC test plan for each model of the KSLV-I and its subsystem but also test method, specification, and results of the verification tests are presented. And also, multipaction analysis results are presented.