• Title/Summary/Keyword: Embedded control unit

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FPGA based Dynamic Thresholding Circuit

  • Cho, J.U.;Lee, S.H.;Jeon, J.W.;Kim, J.T.;Cho, J.D.;Lee, K.M.;Lee, J.H.;Byun, J.E.;Choi, J.C.
    • 제어로봇시스템학회:학술대회논문집
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    • 2004.08a
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    • pp.1235-1238
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    • 2004
  • Thresholding has been used to reduce the number of gray values in images. Typically, a single threshold value has been used, resulting in two gray level images. Image reduction of one single threshold value, however, may lose too much of the high-frequency edge information. Thus, dynamic thresholding that uses a different threshold for each pixel is preferred instead of using a single threshold value. Dynamic thresholding can preserve high frequency details as well as reduce the size of images. Since it takes long time to perform existing software dynamic thresholding in an embedded system, this paper proposes and implements a circuit by using a FPGA in order to perform a real-time dynamic thresholding,. The proposed circuit consists of two counters, and threshold look-up table, and control unit. The values of two counters determine each pixel position, the threshold look-up table converts each pixel value into other value, and the control unit generates necessary control signals. On arriving from a camera to the proposed circuit, each pixel is compared with its threshold value and is converted into other gray value. An image processing system by using the proposed circuit will be implemented and some experiments will be performed.

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Autonomous Flight Experiment of a Foldable Quadcopter with Airdrop Launching Function (고공 비행개시가 가능한 접이식 쿼더콥터 자율비행 실험)

  • Lee, Cheonghwa;Chu, Baeksuk
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.17 no.2
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    • pp.109-117
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    • 2018
  • The experimental results are presented of an autonomous flight algorithm of a foldable quadcopter with airdrop launching functions. A foldable wing structure enabled the quadcopter to be inserted into a rocket container with limited space. The foldable quadcopter was then separated from the rocket in the air. The flight pattern was tracked using a global positioning system (GPS) with various sensors, including an inertial measurement unit (IMU) module until a designated target position was reached. Extensive field tests were conducted through an international rocket competition, ARLISS 2017, which was held in Black Rock Desert, Nevada, USA. The flight trajectory record of the experiments is stored in electrically erasable programmable read-only memory (EEPROM) embedded in the main control unit. The flight record confirmed that the quadcopter successfully separated from the rocket, executed flight toward the target for a certain length of time, and stably landed on the ground.

Embedded ARM based SoC Implementation for 5.8GHz DSRC Communication Modem (임베디드 ARM 기반의 5.8GHz DSRC 통신모뎀에 대한 SOC 구현)

  • Kwak, Jae-Min;Shin, Dae-Kyo;Lim, Ki-Taek;Choi, Jong-Chan
    • Journal of the Institute of Electronics Engineers of Korea TC
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    • v.43 no.11 s.353
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    • pp.185-191
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    • 2006
  • DSRC((Dedicated Short Range Communication) is dedicated short range communication for wireless communications between RSE(Road Side Equipment) and OBE(On-Board Unit) within vehicle moving high speed. In this paper, we implemented 5.8GHz DSRC modem according to Korea TTA(Telecommunication Technology Association) standard and investigated implementation results and design process for SoC(System on a Chip) embedding ARM CPU which control overall signal and process arithmetic work. The SoC is implemented by 0.11um design technology and 480pins EPBGA package. In the implemented SoC ($Jaguar^{TM}$), 5.8GHz DSRC PHY(Physical Layer) modem and MAC are designed and included. For CPU core ARM926EJ-S is embedded, and LCD controller, smart card controller, ethernet MAC, and memory controller are designed as main function.

TRANSFER ORBIT THERMAL ANALYSIS FOR COMS (통신해양기상위성의 전이궤도 열해석)

  • Jun, Hyoung-Yoll;Kim, Jung-Hoon;Kim, Sung-Hoon;Yang, Koon-Ho
    • Journal of computational fluids engineering
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    • v.13 no.2
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    • pp.48-54
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    • 2008
  • COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and has been developing by KARI for communication, ocean and meteorological observations. It will be launched by ARIANE 5. Ka-band components are installed on South panel, where single solar array wing is mounted. Radiators, embedded heat pipes, external heat pipe, insulation blankets and heaters are utilized for the thermal control of the satellite. The Ka-band payload section is divided several areas based on unit operating temperature in order to optimize radiator area and maximize heat rejection capability. Other equipment for sensors and bus are installed on North panel. The ocean and meteorological sensors are installed on optical benches on the top floor to decouple thermally from the satellite. During the transfer orbit operation, satellite will be under severe thermal environments due to low dissipation of components, satellite attitudes and LAE(Liquid Apogee Engine) firing. This paper presents temperature and heater power prediction and validation of thermal control design during transfer orbit operation.

TRANSFER ORBIT THERMAL ANALYSIS FOR SATELLITE (위성의 전이궤도 열해석)

  • Jun, Hyoung-Yoll;Kim, Jung-Hoon;Kim, Sung-Hoon;Yang, Koon-Ho
    • 한국전산유체공학회:학술대회논문집
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    • 2007.10a
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    • pp.227-231
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    • 2007
  • COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and has been developing by KARI for communication and ocean and meteorological observations. It will be launched by ARIANE 5. Ka-band components are installed on South panel, where single solar array wing is mounted. Radiators, embedded heat pipes, external heat pipe, insulation blankets and heaters are utilized for the thermal control of the satellite. The Ka-band payload section is divided several areas based on unit operating temperature in order to optimize radiator area and maximize heat rejection capability. Other equipment for sensors and bus are installed on North panel. The ocean and meteorological sensors are installed on optical benches on the top floor to decouple thermally from the satellite. During the transfer orbit operation, satellite will be under severe thermal environments due to low dissipation of components, satellite attitudes and LAE(Liquid Apogee Engine) firing. This paper presents temperature and heater power prediction and validation of thermal control design during transfer orbit operation.

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The Uplift Capacity of Plane and Corrugated Piles for Pipe Frame Greenhouse (파이프 골조온실의 민말뚝과 주름말뚝의 인발저항력)

  • Yong Cheol Yoon;Won Myung Suh;Jae Hong Cho
    • Journal of Bio-Environment Control
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    • v.10 no.3
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    • pp.148-154
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    • 2001
  • The uplift capacity of a pile for improving the wind resistance of the 1-2 W type plastic film pipe on greenhouses was tested using the plane and corrugated piles with various shapes and diameters. First, the resistant uplift capacity was measured by using the uplift loading on plane piles. As the uplift loading on plane piles increased, the resistant uplift capacity also increased until the loading was reached to ultimate uplift capacity. After ultimate uplift capacity was appeared the uplift displacement, the uplift capacity was decreased gradually. Secondly, the resistant uplift capacity was measured by using the uplift loading on corrugated piles. After the uplift capacity was reached the uplift displacement, the uplift capacity was continually increased or decreased. In general, the ultimate uplift capacity was independent of pile shapes, pile diameter length, and embedded pipe depth. However, the ultimate uplift capacity of a corrugated pile was twice more than that of a plane pile without regard to its diameter and embedded depth. The ultimate uplift capacity per unit pile area was increasing in deeper embedded depth. However, the longer a pile diameter was, the less ultimate uplift capacity. The uplift capacity of a plane pile, used in conjunction with the design wind velocity (26.9m.s$^{-1}$ ) of the project area, was unsatisfiable without regard to diameters and embedded depths of piles, while most of corrugated piles were well appeared uplift capacity under various experimental conditions.

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Control of Duration Model Parameters in HMM-based Korean Speech Synthesis (HMM 기반의 한국어 음성합성에서 지속시간 모델 파라미터 제어)

  • Kim, Il-Hwan;Bae, Keun-Sung
    • Speech Sciences
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    • v.15 no.4
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    • pp.97-105
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    • 2008
  • Nowadays an HMM-based text-to-speech system (HTS) has been very widely studied because it needs less memory and low computation complexity and is suitable for embedded systems in comparison with a corpus-based unit concatenation text-to-speech one. It also has the advantage that voice characteristics and the speaking rate of the synthetic speech can be converted easily by modifying HMM parameters appropriately. We implemented an HMM-based Korean text-to-speech system using a small size Korean speech DB and proposes a method to increase the naturalness of the synthetic speech by controlling duration model parameters in the HMM-based Korean text-to speech system. We performed a paired comparison test to verify that theses techniques are effective. The test result with the preference scores of 73.8% has shown the improvement of the naturalness of the synthetic speech through controlling the duration model parameters.

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Embedded Module for Searching Direction of Sounds (소리발생 근원지 방향을 탐지하는 임베디드 모듈)

  • Park, Jin-Seo;Oh, Se-Jong
    • Proceedings of the KAIS Fall Conference
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    • 2009.05a
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    • pp.680-683
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    • 2009
  • 본 논문에서는 소리발생 근원지 방향을 탐지하는 임베디드 모듈을 제작하였다. 로봇에게 다양한 정보를 제공하여 더 많은 기능을 수행할 수 있도록 도와 로봇의 활용분야를 넓히고자 한다. 해당 모듈은 ATMega128 MCU(Micro Control Unit), 두 개의 소리센서 그리고 서보모터를 사용하여 제작되었다. 두개의 소리센서가 회전축을 중심으로 180도 반동운동을 하면서 주기적으로 발생한 소리에 대해서 이격되어있는 두 개의 센서가 시간차이를 두고 반응하게 된다. 이 시간차이를 이용하여 소리발생 근원지의 방향을 계산하게 된다.

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The Research of System-On-Chip Design for Railway Signal System (철도신호를 위한 단일칩 개발에 관한 연구)

  • Park, Joo-Yul;Kim, Hyo-Sang;Lee, Joon-Hwan;Kim, Bong-Taek;Chung, Ki-Seok
    • Proceedings of the KSR Conference
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    • 2008.06a
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    • pp.572-578
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    • 2008
  • As the railway transportation is getting faster and its operation speed has increased rapidly, its signal control has been complicated. For real time signal processing it is very important to prohibit any critical error from causing the system to malfunction. Therefore, handling complicated signals effectively while maintaining fault-tolerance capability is highly expected in modern railway transportation industry. In this paper, we suggest an SoC (Sytem-on-Chip) design method to integrate these complicated signal controlling mechanism with fault tolerant capability in a single chip. We propose an SoC solution which contains a high performance 32-bit embedded processor, digital filters and a PWM unit inside a single chip to implement ATO's, ATC's, ATP's and ATS's digital signal-processing units. We achieve an enhanced reliability against the calculation error by adding fault tolerance features to ensure the stability of each module.

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Development of Sewage Treatment Equipment Control Unit by Embedded System (임베디드시스템에 의한 오수처리시설 제어장치 개발)

  • Jeung, Young-Dek;Kim, Gun-Ho;Park, Joo-Sik;Kang, Kyung-Sik
    • Proceedings of the Safety Management and Science Conference
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    • 2007.04a
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    • pp.51-59
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    • 2007
  • 오수처리시설물 제어하는 기존 제어장치는 PLC에 의한 것으로 조건제어, 유지관리, 기능확장에 따른 운영에 많은 어려움을 가지고 있다. 본 연구에서는 임베디드 시스템에 의한 제어장치를 개발하여 다양한 환경에 대한 유입수량, 농도상태에 따른 반응시간 및 전체 진행시간을 프로그램 하기 쉬운 구조로 하였다. 또한 효율적인 장비가동으로 설비보전을 할 수 있어 유지비용을 줄일 수 있다. 가장 큰 목적은 사용자와 관리자가 쉬운 유지관리를 위해 보다 더 신뢰할 수 있는 배출수 운영으로 하천 수질개선을 위함이다.

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