• 제목/요약/키워드: Telemetry System

검색결과 351건 처리시간 0.027초

과학기술위성3호 홀 추력 제어기 개발 (Development of a Hall-thruster Propulsion Controller for Science Technology Satellite-3)

  • 이성호;조희근;유준
    • 한국항공우주학회지
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    • 제38권10호
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    • pp.992-997
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    • 2010
  • 과학기술위성3호(STSAT-3)용 홀추력시스템(HPS)의 추력제어모듈(PCM)은 압력정밀도 5%이하와 유량정밀도 3%이하를 목표로 한다. 압력제어기는 비례유량제어밸브(PFCV)와 저압압력센서를 사용하여 목표압력을 제어하도록 하고, 유량제어기는 PFCV와 홀추력기의 에노우드(anode) 전류를 이용하여 유량을 조절한다. 제어형태로는 비례,적분(PI) 제어기를 선택하고, PI 이득은 Matlab 시뮬레이션을 통하여 정한다. 시험결과 압력정밀도 <${\pm}$5%와 유량정밀도 <${\pm}$1.87%를 얻었다. 본 논문은 홀추력 제어모듈의 설계, 구현, 그리고 성능시험 결과를 기술한다.

저궤도 및 정지궤도위성의 TC&R RF 서브시스템 검증을 위한 RF 시험 장비 설계 (Design of Radio Frequency Test Set for TC&R RF Subsystem Verification of LEO and GEO Satellites)

  • 조승원;이상정
    • 한국항공우주학회지
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    • 제42권8호
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    • pp.674-682
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    • 2014
  • RFTS(Radio Frequency Test Set)은 저궤도 위성과 정지궤도 위성의 AI&T 기간 동안 TC&R RF 서브시스템을 검증하는 필수 장비이다. 본 논문에서는 새로운 RFTS의 상세 설계 내용을 제시하는데 기존의 RFTS와 달리 위성 프로젝트 별 시험 수행 시 수정 없이 바로 적용할 수 있도록 하였다. 하드웨어와 소프트웨어는 이를 만족하도록 설계 되었고 기능 별 모듈화와 상용품 사용의 확장으로 보다 손쉬운 제어와 운용이 될 수 있도록 하였으며 시스템의 신뢰성 향상을 가져오도록 하였다. 또한 보다 정확한 기준 클락을 채택하여 RF 측정에 대한 신뢰도를 높였다.

하수처리 활성오니공정의 에너지 절감을 위한 퍼지 제어 방법에 관한 연구 (A Study on Fuzzy Control Method of Energy Saving for Activated Sludge Process in Sewage Treatment Plant)

  • 남의석
    • 전기학회논문지
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    • 제67권11호
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    • pp.1477-1485
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    • 2018
  • There are two major issues for activated sludge process in sewage treatment plant. One is how to make sewage be more clean and the other is the energy saving in sewage treatment process. The major monitoring sewage qualities are chemical oxygen demand, phosphorus, nitrogen, suspended solid in effluent. These are transmitted to the national TMS(Telemetry Monitoring System) at every hour. If these exceed the environmental standard, the environmental charges imposed. So, these water qualities are to be controlled below the environmental standard in operation of sewage treatment plant. And recently, the energy saving is also important in process operation. Over 50% energy is consumed in blowers and motors for injection oxygen into aeration tank. So, with the water qualities to be controlled below the environmental standard, the energy saving also is to be accomplished for efficient plant management. Almost researches are aimed to control water quality without considering energy saving. AI techniques have been used for control water quality. AI modeling simulator provided the optimal control inputs(blower speed, waste sludge, return sludge) for control water quality. Blower speed is the main control input for activated sludge process. To make sewage be more clean, the excessive blower speed is supplied, but water quality is not better than the previous. In results, non necessary energy is consumed. In this paper we propose a new method that the energy saving also is to be accomplished with the water qualities to be controlled below the environmental standard for efficient plant management. Water qualities in only aeration tank are used the inputs of fuzzy models. Outputs of these models are chemical oxygen demand, phosphorus, nitrogen, suspended solid in effluent and have the environmental standards. In test, we found this method could save 10% energy than the previous methods.

牧乾草의 定量給與時 소 反芻行動의 變異性 (Variability of the Rumination-Behaviour in Steers fed a Constant Amount of Hay)

  • 전병태;태전실
    • 한국초지조사료학회지
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    • 제8권2호
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    • pp.68-76
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    • 1988
  • The variation of rumination response in steers fed a same amount of orcharograss hay was investigated. With three steers (6, 12, 24 months) of the Japanese Black Breed, rumination behaviour was measured continuously during a 5 days period by masseter EMG telemetry system. The results are summarized as follows: 1. The average daily ruminatio time of respective animals were 438,447 and 433 min. with small daily variation both within and among animal. But the rumination time per DM kg of hay consumed varied from 66 to 138 min., and calf spent longer than older calf. 2. Actural chewing time showed small variation, and percentage of actural chewing time spent in rumination time was from 88 to 93% on individual average. 3. The daily number of chewing in rumination was approximately 25,000 to 30,000 with large individual differences. The chews per DM kg intake varied from 3,800 to 9,600, and calf chewed more than older calf. 4. The average rate of chewing per 100 sec. (chewing speed), there was a large difference between animals I.e. 104, 114, 131 respectively, but very little variance between days in individual. 5. No relation between day to day variations in eating time and rumination behavior, but significantly positive correlation was observed in the relation among rumination time, chewing time, No. of boluses and No. of chews. 6. Active time of day in rumination altered considerably day to day, but variation in the amount of rumination per day as expressed by the rumination time was relatively small.

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Operational Report of the Mission Analysis and Planning System for the KOMPSAT-I

  • Lee, Byoung-Sun;Lee, Jeong-Sook;Kim, Jae-Hoon;Lee, Seong-Pal;Kim, Hae-Dong;Kim, Eun-Kyou;Park, Hae-Jin
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2003년도 한국우주과학회보 제12권2호
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    • pp.46-46
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    • 2003
  • Since its launching on 21 December 1999, the KOrea Multi-Purpose SATellite-Ⅰ (KOMPSAT-Ⅰ) has been successfully operated by the Mission Control Element (MCE), which was developed by the Electronics and Telecommunications Research Institute (ETRI). Most of the major functions of the MCE have been successfully demonstrated and verified during the three years of the mission life of the satellite. The Mission Analysis and Planning Subsystem (MAPS), which is one of the four subsystems in the MCE, played a key role in the Launch and Early Orbit Phase (LEOP) operations as well as the on-orbit mission operations. This paper presents the operational performances of the various functions in MAPS. We show the performance and analysis of orbit determinations using ground-based tracking data and GPS navigation solutions. We present four instances of the orbit maneuvers that guided the spacecraft from injection orbit into the nominal on-orbit. We include the ground-based attitude determination using telemetry data and the attitude maneuvers for imaging mission. The event prediction, mission scheduling, and command planning functions in MAPS subsequently generate the spacecraft mission operations and command plan. The fuel accounting and the realtime ground track display also support the spacecraft mission operations. We also present the orbital evolutions during the three years of the mission life of the KOMPSAT-Ⅰ.

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FEA 시뮬레이션을 이용한 혈관 상태 측정용 커패시티브 센서 설계; 체내 동맥 혈관 변화 모니터링이 가능한 이식형 텔레메트리 시스템 개발을 위한 (Design of Capacitive Sensors for Blood Vessel Condition Using FEA Simulation; For Developing of an Implantable Telemetry System to Monitoring the Arterial Change)

  • 강소명;이재호;웨이췬
    • 한국멀티미디어학회논문지
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    • 제22권11호
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    • pp.1280-1287
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    • 2019
  • For developing a wireless implantable device to monitoring the artery variation in real-time. The concept of a special vessel variation measurement capacitive sensor is presented in this paper. The sensor consists of two part; main sensor to measuring the arterial variation, and reference sensor is used to improve the accuracy of the capacitance value variation. Before sensor manufacture, a model of the sensor attached on the artery was designed in 3D to conduct in the FEA simulation to validate the validity and feasibility of the idea. The artery model was designed as layered structures and made of collagenous soft tissues with intima inside, followed by the media and the adventitia. Also, a grease layer was designed in the inner of the arterial wall to imitate the clogged arteries. The simulation was divided into two parts; sensor performance test by changing the diameter of the grease layer, and arterial wall tension test by changing the blood pressure. As the simulation results, the capacitance value measured by the proposed sensor is decreased follow the diameter of the grease increased. Also, large elastic deformation of the arterial wall since changing the blood pressure has been observed.

다중 환경요소의 원격감시 및 제어에 대한 연구 ((A study on the Telemetry monitoring and control of the multi environment factor))

  • 주귀영;최조천
    • 전자공학회논문지SC
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    • 제39권1호
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    • pp.7-15
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    • 2002
  • 원거리에 분산되어 있는 다수의 양식시설을 마이크로프로세서를 이용하여 원격으로 환경상태를 감시하고 제어하기 위한 알고리즘을 구현하였다. 각각의 시설에서 검출한 환경데이터를 하나의 프로세서에 수집한 후, 전화선을 이용하여 FSK 방식으로 원거리의 관리자에게 전송하고 데이터를 수신하여 표시기에 나타내므로써 시설들의 환경상태를 알 수 있다. 또한 관리자는 시설의 환경을 조절하는 제어기의 작동데이터를 설정하여 전송하면 해당시설로 전달되어 원격으로 환경을 제어할 수 있다. 다수의 시설에서 검출된 환경데이터를 최소의 회선을 사용하여 한곳으로 취득하기 위한 방법으로 멀티-프로세싱 기법을 적용하였고, 취득한 데이터와 제어용 데이터의 상호교환을 위한 알고리즘을 연구하였다. 먼저 프로세서 상호간의 통신시?스를 설계하여 데이터의 교환에 대한 통신알고리즘을 실험적으로 구현하였으며, 전화회선의 통과주파수 대역에서 전송특성의 검토로 설계한 FSK 변복조기의 성능을 분석하였다. 또한 대량의 시설을 관리하기 위하여 PC를 활용한 DB구축에 대한 알고리즘도 제시하였다. 본 연구의 목적은 최소의 비용으로 쉽게 사용할 수 있는 방법의 구현에 있으며, 시설의 관리에 소요되는 노동력의 감소와 환경상태의 악화에 의한 만약의 사태를 예방할 수 있는 경보를 제공하는 것으로 양식산업을 보다 과학적이고 기술적인 방향으로 개선하는데 있다.

과학기술위성 3호 X-대역 송신기 비행모델 설계, 제작 및 시험 (Design, Implementation and Test of Flight Model of X-Band Transmitter for STSAT-3)

  • 서규재;이정수;오치욱;오승한;채장수
    • 한국항공우주학회지
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    • 제40권5호
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    • pp.461-466
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    • 2012
  • 본 논문에서는 현재 KAIST 인공위성 연구센터(SaTReC)에서 개발 진행 중인 과학기술위성3호(STSAT-3) 위성체의 탑재체 데이터 전송을 위한 X대역 송신기 비행모델 개발 및 시험에 관하여 기술한다. 과학기술위성3호의 통신시스템은 크게 상태정보, 명령 송수신을 위한 통신채널과 임무데이터 전송을 위한 통신채널로 구성되며 상태 정보 및 명령 송수신을 위하여 S대역을 사용하며 임무데이터 전송용으로 X대역 주파수를 사용하고 있다. 과학기술위성 3호에서는 대용량 메모리 유닛(MMU; Mass Memory Unit)에 저장된 탑재체 관측정보가 X대역 송신기의 QPSK 변조기에서 변조를 하고, 변조된 신호는 스위치를 거친 이후에 안테나를 통해 송신된다. 본 논문에서는 과학기술위성 3호 X대역 송신기 내부의 변조방식, 저역통과 여파기, power amp, 스위치 등에 대해서 제작된 특성을 기술한다. X-band 송신기의 비행모델은 성능시험, 환경시험(진동시험, 열진공시험)을 성공적으로 마치고 위성체 조립 단계(Assembly Integration and Test, AIT)에 납품되었다.

VERTICAL OZONE DENSITY PROFILING BY UV RADIOMETER ONBOARD KSR-III

  • Hwang Seung-Hyun;Kim Jhoon;Lee Soo-Jin;Kim Kwang-Soo;Ji Ki-Man;Shin Myung-Ho;Chung Eui-Seung
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2004년도 한국우주과학회보 제13권2호
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    • pp.372-375
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    • 2004
  • The UV radiometer payload was launched successfully from the west coastal area of Korea Peninsula aboard KSR-III on 28, Nov 2002. KSR-III was the Korean third generation sounding rocket and was developed as intermediate step to larger space launch vehicle with liquid propulsion engine system. UV radiometer onboard KSR-III consists of UV and visible band optical phototubes to measure the direct solar attenuation during rocket ascending phase. For UV detection, 4 channel of sensors were installed in electronics payload section and each channel has 255, 290, 310nm center wavelengths, respectively. 450nm channel was used as reference for correction of the rocket attitude during the flight. Transmission characteristics of all channels were calibrated precisely prior to the flight test at the Optical Lab. in KARI (Korea Aerospace Research Institute). During a total of 231s flight time, the onboard data telemetered to the ground station in real time. The ozone column density was calculated by this telemetry raw data. From the calculated column density, the vertical ozone profile over Korea Peninsula was obtained with sensor calibration data. Our results had reasonable agreements compared with various observations such as ground Umkhr measurement at Yonsei site, ozonesonde at Pohang site, and satellite measurements of HALOE and POAM. The sensitivity analysis of retrieval algorithm for parameters was performed and it was provided that significant error sources of the retrieval algorithm.

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건식 듀얼 클러치의 열해석 모델에 대한 연구 (A Study on Thermal Analytical Model for a Dry Dual Clutch)

  • 류하오;이재천;노유정;조종환;이희락;고재욱;강지우
    • 드라이브 ㆍ 컨트롤
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    • 제12권1호
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    • pp.1-8
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    • 2015
  • The stability of friction characteristics and thermal management for a dry type dual clutch transmission (DCT) are inferior to those of a wet clutch. Too high temperature resulting from frequent engagement of DCT speeds up degradation or serious wear of the pressure plate or burning of the clutch disk lining. Even though it is significantly important to estimate the temperature of a dry double clutch (DDC) in real-time, few meaningful study of the thermal model of DDC has been known yet. This study presented a thermal analytical model of lumped parameters for a DDC by analyzing its each component firstly. Then a series of experimental test was carried out on the test bench with a patented temperature telemetry system to validate the proposed thermal model. The thermal model, whose optimal parameter values were found by optimization algorithm, was also simulated on the experimental test conditions. The simulation results of DDC temperature show consistency with the experiment, which validates the proposed thermal model of DDC.