• Aerospace Engineering and Technology
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• v.1 no.2
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• pp.45-50
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• 2002

A conceptual design on the link budget of TC&R RF subsystem which transfers command and telemetry data as RF signal between the ground system and the 2005SAT spacecraft is presented in this paper. In order to perform the analysis of the link budget, we divided the analysis process into two processes, i.e., uplink and downlink process. For the uplink the power flux density at the spacecraft and the margin of the command receiver are calculated. In the case of the downlink the downlink EIRP and the margin of C/ No and Eb / No at the ground station are calculated. Through the uplink performance analysis, the power at the command receiver has well efficient margin, and the margin of C/ No and Eb / No is also fully proper for the downlink case.

• Aerospace Engineering and Technology
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• v.2 no.2
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• pp.167-178
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• 2003

The design on the Telemetry Ground System for launch of KSLV(Korea Space Launch Vehicle) in the korean Space center has been conducted in this study. For the optimized system design, first of all, the system deployment plan reflecting the topographic and geographic environments of the space center and launch vehicle characteristics has been developed. The RF link budget analysis for the maximum tracking range, requirement for receiving subsystem including antenna subsystem, requirement for data processing subsystem are also analyzed based on the On-Board Telemetry characteristics and launch vehicle parameters. Based on those analysis, telemetry ground system containing tracking/receiving subsystem, recording subsystem and data processing subsystem, timing subsystem, calibration subsystem and monitoring and control subsystem are designed. Futhermore, the analysis for the maximum permissible data latency and communication protocol between each telemetry station and control center are conducted and the entire system is designed so that the major telemetry parameters selected to the best quality are provided in real time to the control center(RCC, RSC) for the launch mission operation.

• Journal of the Korea Convergence Society
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• v.11 no.10
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• pp.53-61
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• 2020

Recently, as the uncontact service is activated in earnest due to the Corona 19 virus, the necessity of system development to provide non-face-to-face contact remote medical service has increased. In this study, we propose a smart healthcare system, Rm_She(Remote Medical Smart Healthcare System). Rm_She can collect and manage various vital signs information by connecting various healthcare products that detect bio-signals based on IoT to one application. The health check app (HC_app) is used to connect vital sign measurement devices to a wireless LAN and receive vital sign values from the HC_app. Then, the vital signs are output to the user on the smartphone, and the corresponding information is transmitted to the healthcare management server. The healthcare server receives the measured values and stores them in a database, and the stored measured values are provided as a web service so that medical staff can remotely monitor them in real time.

• Journal of Satellite, Information and Communications
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• v.8 no.4
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• pp.111-116
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• 2013

Because LEO (Low Earth Orbit) satellite has very limited contact time between satellite and ground station, all telemetry data generated on satellite are stored in a mass memory and transmitted to the ground during the contact time. There are two downlink modes, real-time mode and playback mode. Only real-time data frames are transmitted to the ground in real-time mode, real-time and playback data frames stored into mass memory are transmitted to the ground in playback mode. In accordance with the data transmission rate, there are two downlink rates, low downlink rate and high downlink rate. This paper briefly introduces downlink interfaces and flight software of a LEO satellite developed in KARI. And it presents the telemetry storage method, real-time and playback downlink management method, and downlink channel and rate control method.

• Journal of Advanced Navigation Technology
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• v.24 no.2
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• pp.134-141
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• 2020

Telemetry system is a communication system that measures and transmits various signals in the aircraft to the ground for collecting and monitoring flight data during the development of unmanned air vehicle and satellite launch vehicles. With the recent development of wireless communication technology, it is becoming important to apply encryption of telemetry system to prepare with security threats that may occur during flight data transmission. In this paper, we suggested and implemented the application method of ARIA-256, Korean standard encryption algorithm, to apply encryption to telemetry system. In consideration of the block error propagation and the telemetry frame characteristics, frame is encrypted using the CTR mode and can apply the Reed-solomon codes recommended by CCSDS. ARIA algorithm and cipher frame are implemented in FPGA, and simulation and hardware verification system confirmed continuous frames encryption.

• Proceedings of the Korean Society of Computer Information Conference
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• 2016.07a
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• pp.123-124
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• 2016

본 논문에서는 사물인터넷 기법을 원격지에서 재배환경을 제어할 수 있는 온실 원격제어시스템을 제안한다. 온실원격제어시스템은 온실내의 환경정보를 계측하여 서버에 저장하고, 이 정보를 이용하여 사용자가 제어함으로서 최적의 재배환경으로 조절하고, 저장된 재배 환경정보를 활용하여 작물의 최적의 재배를 위한 기초 자료로 활용하도록 한다. 온실 원격 제어시스템을 웹과 연동하여 각종 기기를 이용하여 원격으로 제어함으로서 각 사용자들이 온실에 접근하지 않고 원격으로 환경을 제어할 수 있도록 구성하였다. 온실 원격제어시스템은 제어부, 통신부 그리고 계측부로 구성하였으며, 무선인터넷을 통하여 5초마다 제어신호를 확인하여 처리하고, 온도를 측정하여 서버에 저장하여 동작을 확인하였다. 따라서 본 논문에서 제안하는 온실 원격제어시스템은 최적의 생장환경을 지속적으로 제공하여 농가의 생산 효율성을 증대 시킬 수 있으리라 사료된다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.49 no.5
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• pp.417-424
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• 2021

The S-band telemetry and telecommand formats for geostationary orbit satellites should have sufficient reliability, since they transmit massive satellite health data and receive the mission commands in the 36,000km of the geostationary orbit. Also, they have to efficiently manage the large quantity of satellite health data under the limited data transmission rate. Cheollian-2A and 2B satellites were developed by Korea Aerospace Research Institute and launched at 2018 and 2020, respectively. Their missions are to conduct continuously the mission of Cheollian-1, which was the first geostationary orbit satellite of Korea. Therefore, the fundamental S-band data format design for Cheollian-2A and 2B should meet the requirements of Cheollian-1. Meanwhile the latest remote data processing techniques for these newest geostationary orbit satellites should be implemented. In this paper, the advanced S-band space data formats and management methods are proposed for more efficient data transmission, reception and operation with the limited data rate of the geostationary orbit satellites. The implemented results in the flight software of Cheollian-2A and 2B are described in detail.

• Proceedings of the KSRS Conference
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• 2006.03a
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• pp.121-124
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• 2006

• Bulletin of Korea Environmental Preservation Association
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• s.411
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• pp.9-12
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• 2014

환경부에서는 에코스마트 상수도 기술, 하 폐수 고도처리기술, 폐금속 유용자원 재활용 기술, 친환경자동차 기술 등 수출 전략형 및 상용화를 위한 4대 글로벌 탑 기술개발사업단 및 Non-$CO_2$ 온실가스 저감기술개발사업단을 발족하였으며, 2014년에는 센서 기술과 ICT 기술을 접목한 원격측정제어 시스템을 개발하여 환경측정기기의 국산화율을 높이고 관련 산업의 경쟁력제고를 위하여 원격 측정제어기술개발 사업단을 발족할 계획이다.

• Proceedings of the KSRS Conference
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• 2007.03a
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• pp.138-141
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• 2007

본 논문에서는 제작이 간편하고, 저렴하여, 설치가 용이한 Trihedral comer reflector를 연결하여 전방향(omni-directional)에서 전파를 입사방향으로 반사하도록 전파반사기를 설계한다. Scale-down된 사각(Square) 형태와 원형(circular) 형태의 Retroreflector를 제작하고 RCS(radar cross section)의 각도별 패턴 특성을 측정하여 이론적, 수치 해석적 계산과 비교한 결과를 보인다. 측정된 RCS 절대 값과 패턴을 이론식 및 시뮬레이션 수치 해석 값과 비교하여 데이터의 적정성을 분석한다.