• Journal of the Korean Society of Fisheries and Ocean Technology
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• v.23 no.1
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• pp.11-17
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• 1987

This paper describes an availability of the teltmeter device made as a trial to measure the under-water noise, and the results of the test. This telemeter device adopts FM-FM system, and its main carrier wave is 146.2MHz. The trans-mission power is about 1w, and the available distance of transmission is 2.5KM. The timer built in the telemeter device controls transmission time and pause time automatically by the R-C time-constant. The former is 30-32 seconds and the latter is 10-12 seconds. The underwater noise in the set net fishing ground and at the breeding tank was measured, and recorded simultaneously on land and at sea with the telemeter device. When the input voltages of the transmitter is 100-300mV, the value of telemetering ambient noise and bio-acoustic underwater noise well agreed with that of the direct measurement. And the teleme-tered underwater noise decreases in proportion the distance between the transmitter and receiver.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2004.05b
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• pp.251-254
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• 2004

인터넷의 보편화와 더불어 인터넷을 이용한 다양한 연구가 시도되고 있다 본 측정 시스템은 웹을 기반으로 하여 원격 측정 환경을 제공한다. 측정 시스템은 내장된 웹서버를 통해 원격 인터페이스를 제공하고, 사용자는 이를 통해 실시간으로 측정 진행 상황을 파악할 수 있다. 본 시스템은 임베디드 리눅스 기반에서 동작되며, 원격 인터페이스를 위해 TCP/IP를 이용한 인터넷과 JAVA환경에서 수행되도록 설계되었다.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.173.1-173.1
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• 2012

천리안 위성 원격측정명령계 RF부는 위성 장착 이후 발사 전까지 여러 단계의 위성체레벨 기능시험을 거치며 요구 성능을 만족하는지를 충분히 확인하였다. 위성 발사후부터 정상궤도 진입 후에 발사전 원격측정명령계 RF가 원하는 요구 기능 및 성능을 만족하고 있는지를 확인하는 궤도운용시험이 수행되었다. 본 논문은 원격측정명령계 RF부의 궤도운용시험 계획에 따라 수행하여 얻어진 시험 결과에 대한 분석에 대한 것이다. 먼저 발사 후 LEOP 동안 원격명령이 정상적으로 수신되고 수행되는지 확인하였다. 그 이후 원격명령이 언락되는 수신 파워 임계(Threshold) 입력 레벨 확인을 확인하였으며 원격측정 다운링크 주파수 변이가 요구범위에 있는지 확인하였으며, 수신신호 스펙트럼 측정을 통해 TM EIRP를 추정한 결과 링크 버짓 마진 대비 추가적인 마진이 있음을 확인하였으며 또한 TM 송신 신호 변조지수가 추정범위 안에 있는지를 확인하였다. 그리고 레인징 시험을 통해 수신기 및 레인징 기능이 정상적으로 동작하고 있음을 확인하였다. 이 궤도운용시험 결과는 후속 정지궤도복합위성 원격측정명령계 RF부 궤도운용시험을 위한 비교 자료로 활용될 것이다.

• Proceedings of the KIEE Conference
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• 2008.10b
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• pp.384-385
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• 2008

본 논문은 전력선이나 무선기지국 처에서 방축된 전자파를 인터넷, 휴대폰 등 통신수단을 이용하여 원격지에서 실시간으로 측정, 감시할 수 있도록 고안된 전자파 인체노출 원격측정 시스템에 대하여 기술한다. 본 시스템은 측정 자동화 및 무인차 개념이 도입되었으며, 국제규격에서 권고한 측정프로토콜에 따라 측정수행이 되므로 전자파인체노출기준의 적합성 여부론 판단하는 표준측정 시스템으로도 활용될 수 있다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.6
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• pp.96-101
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• 2003

Korea Sounding Rocket(KSR)-III onboard telemetry system has acquired various data from subsystems and sensors in the rocket, and radiated PCM/FM data using two S-band antennas during the flight. Simultaneously， it is necessary that the ground receiving systems track the rocket, and receive and decode telemetry data. Also post processed telemetry data are needed to be broadcasted on ethernet network in real time. Range safety display system displays flight trajectory using telemetry data in mission control center, and so flight manager makes a decision for flight termination from the trajectory This paper describes operating technique about telemetry reception, the development for the realtime data processing system, and the results for telemetering reception on fight test. We telemetered, processed, and broadcasted numerous telemetry data during the flight test successfully.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.2
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• pp.170-177
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• 2011

This paper proposes a telemetering method that transmits the real-time data together with the time-delayed data and that merges both data after flight test. The method can minimize the error data which occur in the communication environment affected by the multipath fading and transmit antenna pattern when telemetry data are received during the flight test. This method was applied to the design of the telemetry unit and the development of data merging program. By merging the resulting data of flight test and analyzing synchronization errors, its efficiency for the telemetry link is verified.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.45 no.5
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• pp.429-436
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• 2017

Since the telemetry performance using the time-delayed data dissipates the wireless channel resources, we propose the spectral efficient retransmission scheme in this paper. In the proposed scheme, the telemetry data is retransmitted based on triggered memory to improve the spectral efficiency. The proposed scheme minimizes the error caused by multipath fading, antenna pattern as well as the error caused by the flight events. In the flight simulation data, we show the proposed scheme improves the telemetry performance based on spectral efficient retransmission.

• Aerospace Engineering and Technology
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• v.6 no.1
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• pp.245-254
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• 2007

The on-board telemetry system of KSLV-1 transmits telemetry signal for the launch vehicle and satellite to ground telemetry system in real time. In ground telemetry system, antenna system acquires telemetry signals and transfers these to data processing system. Data processing system processes and recordes telemetry data and distributes it to each mission operator in order to monitor it the operation goes well or not. This document describes the configurations and functions of data processing system designed for efficient and appropriate processing of telemetry data.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.7
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• pp.98-105
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• 2005

In this paper, the decryption function of CCSDS telecommand of CTU EQM for the security of communications satellite was verified. In order to intensify the security level of DES CFB decryption algorithm applied to CTU EM, 3DES CFB decryption algorithm using three keys is implemented in the CTU EQM. As the decryption keys increased due to the 3DES algorithm, the keys and IV are stored in PROM memory, and used for the telecommand decryption by taking the keys and IVs corresponding to the selected key and IV indexes from the memory. The operation of the 3DES CFB is validated through the timing simulation of 3DES CFB algorithm, and then the 3DES CFB core implemented on the A54SX32 FPGA. The test environment for the telecommand decryption verification of the CTU EQM was built up. Through sending and decrypting the encrypted command, monitoring the opcodes, and confirming LED on/off by executing the opcodes, the 3DES CFB telecommand decryption function of the CTU EQM is verified.

• Aerospace Engineering and Technology
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• v.11 no.2
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• pp.73-79
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• 2012

Because the contact time between satellite and ground station is very limited in LEO (Low Earth Orbit) satellite, all telemetry data generated on spacecraft bus are stored in a mass memory and downlinked to the ground together with real time data during the contact time. The mass memory is initialized in the first system initialization phase and the page status of each memory block is generated step by step. After the completion of the system initialization, the telemetry data are continuously stored and the stored data are played back to the ground by command. And the memory scrubbing is periodically performed for correction of single bit error which can be generated on harsh space environment. This paper introduces the mass memory operation method for telemetry processing of LEO satellite. It includes a general mass memory data structure, the methods of mass memory initialization, scrubbing, data storage and downlink, and mass memory management of primary and redundant mass memory.