• Title/Summary/Keyword: Propulsion control

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Development and Revenue Service of Propulsion System Using IPM (IPM 소자를 사용한 추진제어장치 개발 및 상용화)

  • LEE K.K.;KIM D.M.;KWON I.D.
    • Proceedings of the KSR Conference
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    • 2005.11a
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    • pp.671-675
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    • 2005
  • In this paper, Development of propulsion system using IPM(Intelligent Power Module) for DC electric vehicle is proposed. Designed propulsion system is comprised of inverter stack which includes 6 IPM, BCH(Breaking Chopper) unit, FC(Filter Capacitor), Control unit. IPM can compose propulsion system simple by including gate drive circuit and protection circuit. Inverter stack is designed as a simple structure using IPM and non clamp capacitor. VVVF Inverter control is used the vector control strategy at low velocity region and slip frequency-control strategy at high velocity region. Designed propulsion system proves the performance through test and revenue service.

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THE CRYOGENIC REGULATOR DESIGN FOR LIQUID PROPULSION SYSTEM

  • Kil Gyoung-sub;Lee Joong-Youp;Na Han-Bee;Kim Byung-Hun;Chung Young-Gaph
    • Bulletin of the Korean Space Science Society
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    • 2004.10b
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    • pp.227-230
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    • 2004
  • The regulator that was designed for space use must be operating on the severe circumstance. For example, operating temperature is below 90K and operating pressure is 20.7 MPa. The design of regulator for liquid propulsion system was accomplished and dynamic characteristic was analyzed successfully.

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Pressure Control of a Variable Thrust Solid Propulsion System Using On-Off Controllers (On-Off 제어기를 이용한 가변추력 고체추진 기관의 압력제어)

  • Kwon, Soon-Kyu;Kim, Young-Seok;Ko, Sang-Ho;Suh, Seok-Hoon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.942-948
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    • 2011
  • Solid propulsion systems have simple structures compared to other propulsion systems and are suitable for long-term storage. However the systems generally have limits on control of thrust levels. In this paper we introduce controllers for combustion chamber pressure using on-off control techniques which have been known for relatively easy implementation and energy efficiency. For this, we use a simple pressure change model by considering only mass conservation within the combustion chamber and we design a classical controllers and on-off controllers with are Pulse Width Modulation(PWM) and Pulse Width Pulse Frequency Modulation (PWPFM). Then we compare the performance results of the controllers through numerical simulations.

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A Study of Telegraph Lever Control System for a ship Propulsion Thruster System Operation (선박 추진제어 운용을 위한 속도전달장치 구현에 관한 연구)

  • Kim, Jong-Duk;Kim, Jeong-Hwan;Kim, Ok-Soo;Kim, Young-Kil
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.14 no.9
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    • pp.1965-1971
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    • 2010
  • A ship propulsion thruster platform which is used by safety sailing takes charge of remote control of a main engine in ship. This system not only guarantees safety and reliable flight sailing but also require remote control technology of a ship. Accordingly, in this paper it deals with a telegraph lever control unit system which is a part of propulsion thruster system as localization technology. Also it makes sure of knowledge and core technology through analysis and designing and developing a telegraph lever control unit system. Moreover, it is sure of acquisition of base technology for integration of a ship propulsion thruster platform.

PMSM Propulsion Control System Development and Test for Rolling Stock (철도 차량용 PMSM 추진제어시스템 개발 및 시험)

  • Ro, Ae-Sook;Kim, Tae-Yun;Chung, Eun-Sung;Han, Jeong-Soo;Lee, Jang-Moo
    • Proceedings of the KSR Conference
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    • 2011.10a
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    • pp.1845-1850
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    • 2011
  • Permanent Magnet Synchronous Motor(PM motor) of Advanced EMU is the direct drive morot(DDM) without using reduction gear and Interior buried Permanent Magnet Synchronous Motor(IPMSM). Propulsion system for IPMSM control is composed 1C1M. 1C1M is good for each motor control and anti slip/slide. Propulsion control system have completed running test on field and reliability test is in progress.

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Propulsion Force Coefficient of Injection Nozzle Size on Air Levitation Type Wafer Transfer System (공기부상방식 웨이퍼 이송시스템의 추진 노즐 크기에 따른 추진력계수에 관한 연구)

  • Moon, In-Ho;Cho, Sang-Joon;Hwang, Young-Kyu
    • Journal of the Semiconductor & Display Technology
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    • v.4 no.1 s.10
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    • pp.35-41
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    • 2005
  • An air levitation type wafer transfer system is composed of control and transfer track. Wafer transfer speed is mainly affected by air velocity of propulsion nozzle. In this study, the propulsion force coefficient was evaluated experimentally for the nozzle with 0.5mm, 0.8mm, and 1.0mm diameter. As a result, the propulsion force was largest in the smallest size of nozzle at same air velocity. The propulsion force coefficient of nozzle increases with reducing diameter of nozzle. This increment of propulsion force coefficient was enlarged remarkably at the 0.5mm diameter of nozzle.

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An Overview: Current Control Technique for Propulsion Motor for EV (전기자동차 구동용 모터를 위한 전류 제어 기술)

  • Lee, Hee-Kwang;Nam, Kwang-Hee
    • The Transactions of the Korean Institute of Power Electronics
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    • v.21 no.5
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    • pp.388-395
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    • 2016
  • Electric vehicles (EV) and hybrid EVs (HEV) are designed and manufactured by GM, Toyota, Honda, and Hyundai motors. The propulsion system design process for EV requires integrating subsystem designs into an overall system model to maximize the performance of a given propulsion architecture. Therefore, high-power density and high-torque density are important attributes required for EV applications. To improve torque and power density, propulsion motors are designed for saturation during high-torque operation. The nonlinearity associated with core saturation is modeled by incorporating the cross-coupling inductances, which also behave nonlinearly. Furthermore, in EV environments, the battery is directly connected to the DC link, and the battery changes depending on the state of charge. It will be onerous if as many optimal current commands as different $V_{dc}$ were made. This paper presents the optimal current commands in the various operating condition and the current control technique in EV environments.

A Study on the Speed and Torque Control of Propulsion Motor for Electric Propulsion Ship by Direct Torque Control (직접토크제어에 의한 전기추진선박의 추진전동기 속도 및 토크제어에 관한 연구)

  • Kim, Jong-Su;Oh, Sae-Gin;Kim, Seung-Hwan
    • Journal of Advanced Marine Engineering and Technology
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    • v.33 no.6
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    • pp.946-951
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    • 2009
  • An induction motor based on DTC(Direct Torque Control) is being increasingly used in various industrial applications. DTC offers faster torque response and better speed control with lesser hardware and processing costs in compared with other controlled drives. This study was to evaluate performance of DTC for induction motor of electric propulsion ship. The simulation results indicated good speed and torque response from the low to middle speed range. Also, DTC has advantages such as the independency on motor parameter.

A Study On Design of propulsion and control system for Korean High Speed Train (한국형 고속전철의 추진 및 제어 시스템 설계에 관한 연구)

  • Lee, Won-Ki;Park, Kwang-Bok
    • Proceedings of the KSR Conference
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    • 2000.05a
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    • pp.576-588
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    • 2000
  • The study was carried out about the design of the propulsion and the control systems for Korean High Speed Train. The propulsion system was studied to run the maximum operating speed of 350km/h, The capacity of the main equipment is decided for the train to run tile maximum operating speed of 350km/h with the configuration of 2 power cars, 4 motorized trailers and 14 intermediate trailers. The control system was studied to two parts the supply and the control of high and low voltages used at train, The performance study of control system would be continued to update through system analysis according to propulsion system developing.

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Development and Performance Characteristic of Propulsion System (Converter/Inverter) for 120km/h AC Electric Vehicle (120km/h급 교류 전동차용 추진제어장치(Converter/Inverter) 개발 및 성능 특성)

  • Kim, Tae-Yun;Kno, Ae-Sook;Kim, Myung-Ryong;Baik, Kwang-Sun;Lee, Sang-Jun;Choi, Jong-Mook
    • Proceedings of the KSR Conference
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    • 2006.11b
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    • pp.1214-1221
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    • 2006
  • In this paper, development and performance characteristic of propulsion system(Converter/Inverter) using IPM(Intelligent Power Module) for 120km/h AC electric vehicle is proposed. The proposed propulsion system is comprised of IPM converter and inverter stack which uses natural air-cooling system, DC-Link, OVCRf unit and control unit. And also 2-Parallel operation of two PWM converter is adopted for increasing capacity of system and the VVVF inverter control is used a mixed control algorithm, where the vector control strategy at low speed region and slip-frequency control strategy at high speed region. The proposed propulsion system is verified by main line test results as well as combined test results.

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