• Title/Summary/Keyword: 원격측정장치

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원격탐사위성의 탑재체전송자료 검증을 위한 소프트웨어의 개발

  • Lee, Sang-Taek;Gang, Hyo-Won
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.2
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    • pp.229.1-229.1
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    • 2012
  • 본 논문에서는 탑재체전송자료 검증을 위한 소프트웨어 개발에 관하여 소개하고자 한다. 원격탐사위성에 탑재되는 고성능원격측정센서는 대용량 데이터를 생성하며 탑재체자료전송장치를 통하여 고주파통신에 의해 지상으로 전송된다. 지상으로 전송되는 대용량 데이터는 다양한 통신경로의 외란으로부터 보호 등을 위하여 채널코딩을 수행된다. 또한 대용량 데이터의 실시간 전송을 위하여 압축이 수행되며 보안을 위한 암호화 역시 수행 된다. 본 논문에서는 이러한 탑재체자료를 검증하기 위한 소프트웨어들과 이러한 소프트웨어의 구성 체계등에 관하여 기술하고 있다.

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Teleoperation of Pneumatic Artificial Muscles Based on Joint Stiffness of Master Device (마스터장치의 회전강성을 고려한 공압인공근육의 원격조정)

  • Kim, Ryeong Hyeon;Kang, Bong Soo
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.37 no.12
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    • pp.1521-1527
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    • 2013
  • This study proposes a wearable master device that can measure the joint stiffness and the angular displacement of a human operator to enhance the adapting capability of a slave system. A lightweight inertial sensor and the exoskeleton mechanism of the master device can make an operator feel comfortable, and artificial pneumatic muscles having a working principle similar to that of human muscles improve the performance of the slave device on emulating what a human operator does. Experimental results revealed that the proposed master/slave system based on the muscle stiffness sensor yielded uniform tracking performance compared with a conventional position-feedback controller when the payload applied to the slave system changed.

Development of Data/Video Transmission System for flying vehicle (비행체 탑재용 데이터/영상 복합전송장치 개발)

  • Cho, Dong-Sik;Ra, Sung-Woong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.11
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    • pp.1052-1057
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    • 2007
  • A highly reliable Video Transmission System (VTS) was developed in order to obtain both video and digital data simultaneously in the real time flight test situation of a flying vehicle. The VTS integrates GPS data, digital telemetry data and video signals into a compact digital data package which is compressed and processed by an MPEG-2 Encoder and a DVB-S modulator respectively. The DVB-S modulator is composed of a specially devised Forward Error Correction processor and base band QPSK modulator. The designed VTS was verified and proved for its required functioning and performance through separate flight tests using an airplane and missiles.

Development of Video Transmission System for Rocket (로켓 탑재를 위한 영상 송수신장치 개발)

  • Cho, Dong-Sik;Rha, Sung-Woong
    • Journal of the Institute of Electronics Engineers of Korea TC
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    • v.46 no.2
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    • pp.60-65
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    • 2009
  • A highly reliable Video Transmission System (VTS) was developed in order to obtain both video and digital data simultaneously in the real time flight test situation of a flying vehicle. The VTS integrates GPS date digital telemetry data and video signals into a compact digital data package which is compressed and processed by an MPEG-2 Encoder and a modulator respectively. The modulator is composed of a specially devised Forward Error Correction processor and base band QPSK modulator. The designed VTS was verified and proved for its required functioning and performance through separate flight tests using an airplane and Rockets.

Dynamic Modeling based Flight Control of Hexa-Rotor Helicopter System (헥사로터형 헬리콥터의 동역학 모델기반 비행제어)

  • Han, Jae-Gyun;Jin, Taeseok
    • Journal of the Korean Institute of Intelligent Systems
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    • v.25 no.4
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    • pp.398-404
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    • 2015
  • In this paper, we describe the design and performance of a prototype multi-rotor unmaned aerial vehicle( UAV) platform featuring an inertial measurement unit(IMU) based autonomous-flying for use in bluetooth communication environments. Although there has been a fair amount of study of free-flying UAV with multi-rotors, the more recent trend has been to outfit hexarotor helicopter with gimbal to support various services. This paper introduces the hardware and software systems toward very compact and autonomous hexarotors, where they can perform search, rescue, and surveillance missions without external assistance systems like ground station computers, high-performance remote control devices or vision system. The proposed system comprises the construction of the test hexarotor platform, the implementation of an IMU, mathematical modeling and simulation in the helicopter. Furthermore, the hexarotor helicopter with implemented IMU is connected with a micro controller unit(MCU)(ARM-cortex) board. The micro-controller is able to command the rotational speed of the rotors and to get the measurements of the IMU as input signals. The control simulation and experiment on the real system are implemented in the test platform, evaluated and compared against each other.

Development of PCM Data Recorder for Telemetry System (원격측정용 PCM 데이터 저장장치 개발)

  • Koh, Kwang-Ryul;Lee, Sang-Bum;Lee, Hyun-Kyu;Kim, Whan-Woo
    • Journal of the Korea Institute of Military Science and Technology
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    • v.14 no.4
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    • pp.607-614
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    • 2011
  • This paper describes the development of pulse code modulation(PCM) data recorder with design, implementation and environmental test. PCM serial data that diverged from telemetry encoder output is used as the input and is reformed to parallel signal through FPGA processing. Controllers construct the packet by the sector and record it into non-volatile memory. Compact flash(CF) memory for data storage media, USB interface for data downloading, and a software for operating status diagnosis and file format conversion are used.

Development of Neutron, Gamma ray, X-ray Radiation Measurement and Integrated Control System (중성자, 감마선, 엑스선 방사선 측정 및 통합 제어 시스템 개발)

  • Ko, Tae-Young;Lee, Joo-Hyun;Lee, Seung-Ho
    • Journal of IKEEE
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    • v.21 no.4
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    • pp.408-411
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    • 2017
  • In this paper, we propose an integrated control system that measures neutrons, gamma ray, and x-ray. The proposed system is able to monitor and control the data measured and analyzed on the remote or network, and can monitor and control the status of each part of the system remotely without remote control. The proposed system consists of a gamma ray/x-ray sensor part, a neutron sensor part, a main control embedded system part, a dedicated display device and GUI part, and a remote UI part. The gamma ray/x-ray sensor part measures gamma ray and x-ray of low level by using NaI(Tl) scintillation detector. The neutron sensor part measures neutrons using Proportional Counter Detector(low-level neutron) and Ion Chamber Type Detector(high-level neutron). The main control embedded system part detects radiation, samples it in seconds, and converts it into radiation dose for accumulated pulse and current values. The dedicated display device and the GUI part output the radiation measurement result and the converted radiation amount and radiation amount measurement value and provide the user with the control condition setting and the calibration function for the detection part. The remote UI unit collects and stores the measured values and transmits them to the remote monitoring system. In order to evaluate the performance of the proposed system, the measurement uncertainty of the neutron detector was measured to less than ${\pm}8.2%$ and the gamma ray and x-ray detector had the uncertainty of less than 7.5%. It was confirmed that the normal operation was not less than ${\pm}15$ percent of the international standard.

원격측정명령처리기 성능검증모델 개발

  • Kim, Joong-Pyo;Koo, Cheol-Hea;Choi, Jae-Dong;Chae, Jong-Won;Kim, Jung-Hoon;Koo, Ja-Chun
    • Aerospace Engineering and Technology
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    • v.4 no.1
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    • pp.86-94
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    • 2005
  • This paper shows the results of design, analysis, manufacturing and test performed to develop the CTU(Command Telemetry Unit) EQM(Engineering Qualification Model). According to the key requirement specifications, the logics and circuits of each board are designed. In order to validate designs, some worst case, part stress, reliability, FMECA, radiation environment and launch environment analyses are performed. After manufacturing and assembling all boards, all functions of CTU EQM are verified through the functional test, environmental test and ETB test.

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인공신경망 사용 핵연료용기 파지 장치의 위치/방향 예견

  • 김기훈;박종범;윤지섭
    • Proceedings of the Korean Nuclear Society Conference
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    • 1996.11a
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    • pp.177-182
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    • 1996
  • Remote nuclear cask handling device (RNCHD)는 사용후 핵연료cask의 원격 조작에 있어서 안전성과 성능을 향상을 목적으로 한다. RNCHD의 한부분인 grapple은 사용후 핵연료cask의 이동 및 수송 또는 용기뚜껑의 개폐를 위하여 cask의 벽에 대각선으로 돌출되어있는 두 개의 trunnion에 삽입되어야한다. 그러나 trunnion으로의 grapple 삽입은 용기중심과 grapple 장치 중심사이의 위치와 방향편차 때문에 어렵게된다. 인공신경망은 grapple에 설치된 광전센서를 사용하여 용기의 중심으로 부터 grapple 장치의 상대적 위치를 계측하기위해 사용된다. 인공신경망 학습은 광전센서값과 grapple의 상대적 위치와 방향사이의 함수적 관계를 추론하기 위해 수행된다. 이렇게 측정된 RNCHD의 중심위치는 grapple의 자세를 맞추기 위한 제어입력값으로 제공된다. 인공신경망 학습을 위한 데이터는 grapple 장치와 trunnion을 모사한 1/2 스케일의 실험장치를 사용함으로써 얻어진다. 학습된 인공신경망은 학습에 사용 안된 센서입력값, 즉 새로운 grapple의 위치에 대해서도 정확성을 가지고 grapple 장치의 위치와 방위를 측정할 수 있었다.

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