• 한국군사과학기술학회지
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• 제14권6호
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• pp.1031-1036
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• 2011

In this paper, we have proposed a methodology which can test and evaluate on system level in development phase of command guided missile system. Test and evaluation play a significant role in the development of weapon system, providing the means for determining to what extent the weapon system satisfies its requirements, whether it functions normally in the operational environment. In case of command guided missile having seeker, the missile communications link provides data to allow the missile to fly an efficient trajectory toward target. Therefore, it is very important to test and evaluate for data link between missile and radar on whole system aspect. we introduce the concept and devices for system level test and evaluation of command guided missile system.

• 한국군사과학기술학회지
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• 제18권6호
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• pp.771-778
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• 2015

In this paper, we have proposed a design method for standardization of weapon information exchange between a weapon control computer of guided missile system and a high echelon command and control system. Because the weapon control computer based on diverse combat platforms is operated with several kinds of a high echelon system, it is necessary to provide a standardized design method for weapon information exchange between mutual system. In fact, it is possible to standardize a interface design specification of weapon information message because weapon information message is closely related to standard tactical data link message. It is essential that the interface design specification of weapon information is submitted to that of tactical data link information. It seems that this interface design specification is very useful in development process of the future weapon system.

• 한국군사과학기술학회지
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• 제18권1호
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• pp.37-45
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• 2015

These days many systems use the gps signal to get their own position. Because it's cheap and accurate and convenient. But, the strength of gps signal is very weak and can be easily interrupted by GPS jamming and GPS spoofing. Normally, fighter can use DME, TACAN, etc to correct their position error when GPS is not working. But, many aircraft which does not have those kinds of hardware need to pay additional cost to get it. In this paper, we propose how to overcome GPS jamming and GPS spoofing by only using data link system. The main purpose of this paper is to make the data link protocol to get an exact position information of own unit at gps error environment.

• 한국국방경영분석학회지
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• 제30권2호
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• pp.32-49
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• 2004

The Tactical Data Link System is a standardized communication link to exchange and interface positional, situational information, command and control in real time. It has been evaluated that this Link would play an important role for tactical interoperability, situation awareness, and execution of joint operations in the future war. But considering the rapidly changing war situations, even though being admitted the necessity of the Tactical Data Link System of Army helicopter, one of superpowers in the Army, substantially we don't still have any concrete concept to build it. Therefore, this work presents how to embody the Tactical Data Link System through computer-aided system engineering on the base of Tactical Data Link System operating concept analysis of helicopters-ground units.

• 시스템엔지니어링워크숍
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• 통권4호
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• pp.146-150
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• 2004

The Tactical Data Link System(TDLS) is a standardized communication link to exchange and interface positional, situational information, command and control in real time. It has been evaluated that the link would play an important role for tactical interoperability, situation awareness, and execution of joint operations in the future war. This work presents how to embody the TDLS through the systems engineering approach on the base of TDLS operating concept analysis of helicopters-groud units.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2003년도 하계종합학술대회 논문집 V
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• pp.2685-2688
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• 2003

A PC-based system for both monitoring and controlling SAUV is developed. The developed system is located on a ship and communicate with the SAUV through optical link through which the system sends motion command and receives video data, SSBL and Digital I/O data. The motion command includes velocity data and direction data. The overall system is developed with the intention of easy operation for operator and safe motion of SAUV. The easy operation is realized by GUI-based interface and the safe motion is realized by fault tolerant capability.

• 항공우주기술
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• 제1권2호
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• pp.45-50
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• 2002

본 논문에서는 지상 관제국과 2005SAT 위성 사이에서 RF 신호로써 명령 및 원격측정 데이터를 전달하는 기능을 수행하는 원격측정명령계 RF 서브시스템의 개념설계 단계의 링크버짓 해석을 수행하였다. 링크버짓 성능분석을 위해 업링크 및 다운링크 과정으로 나누고 업링크에 대해서는 위성체에서 전력흐름밀도 및 명령수신기에서 여유를 계산하고 다운링크에 대해서는 다운링크 EIRP 및 지상국에서 C/ $N_o$ 및 $E_b$/ $N_o$ 여유를 계산하여 전체적인 통신성능 여유를 만족하는지 조사를 하였다. 업링크 링크버짓 분석결과 명령수신기에서 충분한 전력 수신 여유가 있었으며 다운링크 링크버짓 분석결과 지상국에서 C/ No 및 $E_b$/ $N_o$의 여유가 적정함을 확인하였다.

• 시스템엔지니어링학술지
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• 제1권1호
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• pp.46-52
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• 2005

The Tactical Data Link System(TDLS) is a standardized communication link to exchange and interface positional, situational information, command and control in real time. It has been evalua ted that the link would play an important role for tactical interoperability, situation awareness, and execution of joint operations in the future war. But considering the rapidly changing war situations, even though being admitted the necessity of the TDLS of Army helicopter, one of superpowers in the Army, it is not yet built the detailed operational concept. Therefore, this work presents how to embody the TDLS through the systems engineering approach based on the TDLS operating concept analysis of helicopters-ground units.

• 한국전자통신학회논문지
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• 제16권6호
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• pp.1045-1052
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• 2021

현대전은 감시체계, 지휘통제체계, 타격체계가 첨단 정보통신기술로 상호 연결되어 전장상황을 공유하는 네트워크 중심전(NCW: Network Centric Warfare)으로 변화해 가고 있다. 한국군은 각 군의 전장상황에 맞게 Link-K, Link-16, Link-11, KVMF 등 다양한 전술데이터링크(TDL: Tactical Data Link)를 활용하고 있다. 한국형 합동 전술데이터링크체계(JTDLS : Joint Tactical Data Link System)는 지상/해상/공중 합동전력간 근실 시간으로 전술정보를 공유하는 체계로 Link-K, Link-16, KVMF에 Link-22를 추가 개발하고 있다. 본 논문에서는 JTDLS체계에 Link-22를 적용하기 위하여 체계 구성, Link-22 메시지 분석 및 전술 데이터 링크 처리기와 Link-22의 연동 구조를 제시하고자 한다.

• 전자공학회논문지S
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• 제34S권7호
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• pp.39-47
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• 1997

The mission of the TTC system is to acquire and process the telemetry data from the satellite and to provide mission planning and satellite control for the target stellite system. In this paper, the transmission scheme for the Tracking, Telemetry and Command(TTC) system of satelliteis described and determined according to the recommendation of CCSDS, and the channel characteristics are analyzed according to modulation method. Expecially, we introduced the concepts of carrier vs. telemetry data power ratio which causes the channel performance to degrade, and analyzed the effects of transmission performance according to the power ratio of carrier vs. telemetry data and the modulation index. The channel of the LEO TTC sytem is different with usual satellite communication system. So, we have generalized the link budget of TTC sytem for using the link budget of ground station well-known and proposed the determination method of modultion indices for improveing channel performance.