• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2005년도 추계학술대회 논문집
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• pp.942-945
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• 2005

This paper tried to analyze the collection and management method of shop-floor information for development of digital framework in u-manufacturing. In detail, the shop-floor information collection method through the direct communication with manufacturing devices using network Including RS-232C/422, field bus and ethernet is analyzed and proposed. In case the direct communication is impossible, the information collection method through additional sensors or data acquisition units is analyzed and proposed. Moreover, the collection method through bar code reader or touch screen of operators is analyzed and proposed to act up to machine to man/mobile/machine.

• 한국항공우주학회지
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• 제39권6호
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• pp.553-558
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• 2011

본 논문에서는 현재 KAIST 인공위성연구센터(SaTReC)에서 개발 진행 중인 과학기술위성3호(STSAT-3) 위성체의 위성 상태정보 전송을 위한 S-대역 송신기 비행모델 개발 및 시험에 관하여 서술하고 있다. STSAT-3의 통신시스템은 크게 상태정보, 명령 송수신을 위한 통신채널과 임무데이터 전송을 위한 통신채널로 구성되며 상태 정보 및 명령 송수신을 위하여 S-대역을 사용하며 임무데이터 전송용으로 X-대역 주파수를 사용하고 있다. S-대역 송신기(S-band Transmitter, STX)는 기능적으로 변조기, 주파수 합성기, 파워 앰프 및 전력공급기 로 구성되어 제작되었다. 전송데이터 변조 방법으로는 주파수 천이방식(Frequency Shift Keying, FSK)을 사용 하며 위성본체와의 데이터 통신은 표준방식인 RS-422통신 방식을 사용하였다. STSAT-3의 STX는 기능적 모듈화에 근거하여 설계 및 제작 되었으며 1.5W(31.7dBm) 송신 출력에 $1{\times}10^{-5}$ 비트오율(BER) 성능을 만족한다. STX 비행모델은 성능시험, 환경시험(진동시험, 열진공시험)을 성공적으로 마치고 위성체 조립단계에 납품되었다.

• 한국자기학회지
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• 제24권4호
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• pp.123-127
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• 2014

본 연구에서는 함정을 자기소거시키는 과정에서 함정에 의한 자기장을 측정하기위한 3-축의 flux-gate 마그네토미터를 설계 제작하였다. 설계에서 고려한 사항은 자기장측정지점과 자기장 데이터를 수집하는 장치 사이의 거리가 수백미터로 멀기 때문에 입력전압의 변동이 커도 동작이 되게 전압 범위가 16~36 V까지 가능한 DC/DC 변환기를 사용하였고, 데이터의 전송은 자기장 측정값을 디지털로 변환 시킨 후 RS422통신으로 전송하게 하였다. 또한 함정을 자기소거 하는 과정에서 발생하는 ${\pm}1mT$ 자기장하에서도 0점의 변화가 ${\pm}2nT$ 이하가 되게 피측정자기장의 보상은 ${\pm}1mT$, 측정범위는 ${\pm}0.1mT$가 되게 제작을 하였다. 또한 수심 30 m에서도 동작되어야하는 조건을 고려하여 6기압 하에서 센서가 수밀이 되고 정상 작동이 되는 것을 확인 하였다. 마그네토미터의 일반특성으로는 선형도가 측정범위 ${\pm}0.1mT$에서 0.01 % 이상 이였고 센서의 노이즈는 1 Hz에서 $30pT/\sqrt{Hz}$이였다.

• 대한임베디드공학회논문지
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• 제8권3호
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• pp.129-136
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• 2013

In this paper, a motion control system based on 2-axis gimbal system is designed and implemented to drive a high speed and precision. The proposed system consists of the RS-422 interface, 2-axis gimbal platform, servo control unit integrated with a high speed DSP chip-set, servo amplifier unit, potentiometer sensor unit, and resolver sensor unit. The servo control unit using the high speed DSP firmware is designed to get a fast response without an overshoot with step input and a RMS error of low probability with ramp input. The servo amplifier unit using a voltage control is designed to resolve the zero-crossing distortion for precise motion. To verify the performance and stability of the implemented system, experiments are performed through a measurement of the time and frequency domain response in a laboratory environment by using a PXI(PCI eXtentions for Instrumentation).

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2002년도 하계종합학술대회 논문집(5)
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• pp.95-98
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• 2002

This paper presents a study on DSP(TMS320F240) controller design for multi-axes transportation system using BLDC servo motor. This BLDC servo motor controller was realized with DSP(Digital Signal Processor) and IPM (Intelligent Power Module). The multi-axes transportation system needs torque, speed, position control of servo motor for variable action. This paper implements those servo control with vector control and space vector modulation technique. As CPU of controller DSP(TMS320F240) is adopted because, it has PWM(Pulse Width Modulation) waveform generator, A/D(Analog to Digital) converter, SPI(Serial Peripheral Interface) port and input/output port etc. The controller of multi-axes transportation system consists of 3-level hierarchy structure that main host PC manages three sub DSP system which transfer downword command and are monitoring the states of end servo controllers. Each sub DSP system operates eight BLDC servo controllers which control BLDC servo motor using DSP and IPM Between host system and middle digital signal processor communicate with RS-422, between main processor and controller communicate with SPI port.

• 한국CDE학회논문집
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• 제4권4호
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• pp.339-349
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• 1999

The punose of this paper is to introduce the comprehensive CAM system (called PosCAM) supporting various function requested from shop floor operators. PosCAM is comported of two subsystems (PosCAM I and PosCAM II) which are designed to make up for the contemporary CAD/CAM systems. PosCAM I is mainly for : a) verifying the part programs written in both custom macros and standard G-codes, b) enhancing machining productivity and quality with built-in cutting conditions and feedrate optimization algorithm. PosCAM II is for : a) efficiently managing the numerous part programs and tool data stored in CNC memory, and b) integratively controlling and monitoring various CNCs from the control center through RS-422 with DNC 2 protocol. The developed systems have been tested via various experiments, and can be Applied for the industrial CNC machine shop as a means for enhancing productivity. The PosCAM system has been implemented and successfully used in the Machine Shop Department of PosCAM since march 1998.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2007년도 하계학술대회 논문집 Vol.8
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• pp.511-512
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• 2007

The monitoring system has won acceptance as a premium mark that identifies the highest standard of product quality in advanced industry. The TOP features with multi-I/O ports and VGA & RCA TV-out ports supporting mirroring & multiple dual-display modes by windows 0/5. With the choice of versatile stands, panel mount, or VESA wall-mount swing arm and connecting to modem. Wireless keyboard, Customer Display and Card Reader, is your idea Panel system for the application of TOP(Touch Operation Pannel), KIOSK, or Office / Factory Automation. TOP is the hardware and software product that transacts all kind of functions for advanced technology equipment to button, switch, voice and graph etc so that let consumer use easily Industrial HMI System Touch Panel. System characteristics: Easy of use and flexibility to the user, Present a high value solution and advanced function for many Application, Factory Automation, Office Automation, Building Automation System, Information Service System, etc. Analog Touch - 2MB Flash Memory for Saving Screen Data - RS-232C/422 Serial Port - Multi Language Support.

• 한국군사과학기술학회지
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• 제26권2호
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• pp.171-178
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• 2023

PCM data is result of air-vehicle flight test, this data is distributed for each engineers to analyze its condition. Since line-of-sight between the air-vehicle and the ground receiver cannot always be secured, remote PCM data recording system was claimed to be required. In this paper multi-function PCM data recorder has been described. This PCM data recorder was intended to place on inside of flight object. It can record about two hours in 32 GB SD card with maximum 7 Mbps data rate. RS-422/485 and RJ-45 interface enhanced accessibility for users. 5 V and 1 A power consumption and 19.5 mm × 152.5 mm × 102.3 mm allow to connect with mobile PCM devices. It acquired more than 190-minutes data in 12-times flight test. Also, it achieved military standard environmental test MIL-STD-810G to prove its stability and solidness.

• 항공우주기술
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• 제10권1호
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• pp.107-115
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• 2011

지상관제용 텔레메트리 데이터처리시스템(Line-telemetry DPS)은 나로호 발사체의 지상 운용 또는 비행시험 중 상단부에 탑재된 원격측정시스템으로부터 RS-422 인터페이스를 통해 PCM 데이터를 수신하고 데이터처리 후 9개의 TLM(Telemetry) 콘솔을 통해 상단시스템의 상태를 모니터링 하는 시스템이다. Line-telemetry DPS (Data Processing System)는 데이터 취득 및 decommutation을 위한 취득(Acquisition) 서버와 시스템을 관리하는 관리(Management) 서버 그리고 각 탑재 시스템을 모니터링하기 위한 9개의 콘솔로 구성된다. Line-telemetry DPS는 UTC(Universal Time Coordinated) 동기되어 상단부 탑재 원격측정 시스템의 원시(raw) 프레임과 decommutation된 온보드 파라미터를 실시간 검출, 저장, 분배 기능을 수행한다. 본 논문에서는 나로호 상단부의 원격측정시스템에 대한 간략한 소개, 지상 및 비행시험을 위한 Line-telemetry DPS의 기능 및 설계, 비정상 알람 파라미터 설정 정보, 지상/비행시험절차 및 결과에 대해 기술하고자 한다.

• 천문학회보
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• 제44권2호
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• pp.57.4-57.4
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• 2019

BITSE is a project of balloon-borne experiments for a next-generation solar coronagraph developed by a collaboration with KASI and NASA. The coronagraph is built to observe the linearly polarized brightness of solar corona with a polarization camera, a filter wheel, and an aperture door. For the observation, the coronagraph is supported by the power distribution unit (PDU), a pointing system WASP (Wallops Arc-Second Pointer), telemetry & telecommand system SIP (Support Instrument Package) which are developed at NASA's Goddard Space Flight Center, Wallops Flight Facility, and Columbia Scientific Balloon Facility. The BITSE Command and Data Handling (C&DH) system used a cost-off-the-shelf electronics to process all data sent and received by the coronagraph, including the support system operation by RS232/422, USB3, Ethernet, and digital and analog signals. The flight software is developed using the core Flight System (cFS) which is a reusable software framework and set of reusable software applications which take advantage of a rich heritage of successful space mission of NASA. The flight software can process encoding and decoding data, control the subsystems, and provide observation autonomy. We developed a python-based testing framework to improve software reliability. The flight software development is one of the crucial contributions of KASI and an important milestone for the next project which is developing a solar coronagraph to be installed at International Space Station.