• Title/Summary/Keyword: Propulsion control

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A Study on the Relationship of Ship Automation System and Safety (선박운항시스템 자동화와 안전의 연관성에 관한 연구)

  • Kim, Bi-A;Lee, Jae-Sik;Oh, Jin-Seok
    • Journal of the Korean Society of Safety
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    • v.22 no.6
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    • pp.69-73
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    • 2007
  • The recent huge maritime casualties and their environmental impacts showed that human error in ship navigation is one of the primary causes leading to accidents. In order to reduce maritime accidents and human errors in ship navigation, it is very important and urgent to improve the skills of navigators and develop advanced navigation support system for ship operations. For example, a SCMS(Ship Control and Management System), INS(Integrated Navigation System) and PCS(propulsion Control System) which are considered as a ship automation system was operated in ship. Furthermore, the most recent automation ships collision incidents warn us that only making automation ships alone is not sufficient for improving ship safety. Effective interaction between officer and ship automation system is essential for safety. In this paper, the interactive relationship between officer and the ship automation system was studied, then the research result for reducing maritime casualties will be presented.

Study on Variable Systems for Compressor and Turbine and its Control Scheme (압축기 정익, 터빈 노즐 가변 메카니즘 및 제어기법 연구)

  • Kim, Sangjo;Kim, Donghyun;Bae, Kyoungwook;Kim, Dae-il;Son, Changmin;Kim, Kuisoon;Lee, Daewoo;Go, Jeungsang;Choi, Dong-Whan;Kim, Myungho;Min, Seongki
    • Journal of the Korean Society of Propulsion Engineers
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    • v.19 no.5
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    • pp.1-14
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    • 2015
  • In case of a gas turbine engine for supersonic operation, the engine have a wide range of operating inlet mass flow rate and required high performance such as thrust and fuel consumption. Therefore, variable system and its optimal control logic are essentially needed. In this work, a method for performance prediction of a gas turbine engine with variable system compressor and its control scheme were developed. Conceptual design of compact acuation system for the operation of the variable system was also conducted. The performance of a low-bypass ratio mixed flow turbofan engine was analyzed, and it was observed that the surge margin of the engine is improved at off-design condition by applying the control scheme.

Development of a Small, Remote Controlled Ship for Observation of Marine Environment (소형 무인 해양 계측선 개발)

  • Lim, Jong-Hwan;Kang, Chul-Wong;Kim, Seong-Gun;Lee, Sang-Moo;Kim, Sang-Chul;Choi, Min-Ho;Kang, Chang-Mo
    • Proceedings of the Korea Committee for Ocean Resources and Engineering Conference
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    • 2002.05a
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    • pp.209-214
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    • 2002
  • We developed a small, remote controlled observation ship that can reduce the cost of gathering data for marine and coastal environments. The control system is composed of three microprocessors, one is for overall mission control, another for control of propulsion motors, and the other for sensor operation. For communication system, we adopt direct and indirect methods based on the wireless modem of commercial cellular telephone. The former is a direct communication between the modems of the ship and the server, and the latter is an indirect communication via internet between the ship and the server. The performance of the ship is demonstrated with the results produced by sets of experiments.

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Active Vibration Control System Using Electromagnet Actuator (전자기 액츄애이터를 이용한 능동 진동제어시스템)

  • Lee, Joo-Hoon;Jeon, Jeong-Woo;Hwang, Don-Ha;Kang, Dong-Sik;Choi, Young-Kiu
    • Proceedings of the KIEE Conference
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    • 2005.07d
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    • pp.2809-2811
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    • 2005
  • In this paper, we address an active vibration control system, which suppresses the vibration engaged by magnetically levitated stage. The stage system consists of a levitating platen with four permanent magnetic linear synchronous motors in parallel. Each motor generates vertical force for suspension against gravity and propulsion force horizontally as well. This stage can generate six degrees of freedom motion via the vertical and horizontal forces. In the stage system, which represents the settling-time critical system, the motion of the platen vibrates mechanically. We designed an active vibration control system for suppressing vibration due to the stage moving. The command feedforward with inertial feedback algorithm is used for solving stage system's critical problems. The components of the active vibration control system are accelerometers for detecting stage tables's vibrations, a digital controller with high precise signal converters, and electromagnetic actuators.

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Sensorless Control of Rotor Field Oriented Induction Motor for Traction Application (견인 유도전동기의 새로운 센서리스 벡터제어)

  • Ryu, Hong-Je;Kim, Jong-Su;Im, Geun-Hui;Won, Chung-Yeon;Dragos, K
    • The Transactions of the Korean Institute of Electrical Engineers B
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    • v.49 no.9
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    • pp.626-634
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    • 2000
  • The paper describes a new and rigorous mathematical model using counter-EMF for the rotor field oriented system with induction motor which uses the estimated speed and rotor flux based on a Model Reference Adaptive System as well as the real-time approach. The estimated speed and rotor flux is used for the speed and flux feedback control. The stability and the convergence of the estimator are improved on the basis of hyperstability theory for non-linear systems. The validity of the proposed method is verified by simulation and also the sensorless control was tested on the propulsion system simulator used for the development of Korean High-Speed Railway Train(KHSRT).

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Study of Thrust-Vectoring Control Using Fluidic Counterflow Concept (Fluidic Counterflow 개념을 이용한 추력벡터제어에 관한 연구)

  • Jung, Sung-Jae;Lim, Chae-Min;Kim, Heuy-Dong
    • Proceedings of the KSME Conference
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    • 2003.04a
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    • pp.1948-1954
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    • 2003
  • The thrust vector control using a fluidic counterflow concept is achieved by applying a vacuum to a slot adjacent to a primary jet which is shrouded by a suction collar. The vacuum produces a secondary reverse flowing stream near the primary jet. The shear layers between the two counterflowing streams mix and entrain mass from the surrounding fluid. The presence of the collar inhibits mass entrainment and the flow near the collar accelerates causing a drop in pressure on the collar. For the vacuum asymmetrically applied to one side of the nozzle, the jet will vector toward the low-pressure region. The present study is performed to investigate the effectiveness of thrust vector control using the fluidic counterflow concept. A computational work is carried out using the two-dimensional, compressible Navier-Stokes equations, with several kinds of turbulence models. The computational results are compared with the previous experimental ones. It is found that the present fluidic counterflow concept is a viable method to vector the thrust of a propulsion system.

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Design, Implementation and Navigation Test of Manta-type Unmanned Underwater Vehicle

  • Kim, Joon-Young;Ko, Sung-Hyub;Cho, So-Hyung;Lee, Seung-Keon;Sohn, Kyoung-Ho
    • International Journal of Ocean System Engineering
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    • v.1 no.4
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    • pp.192-197
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    • 2011
  • This paper describes the mathematical modeling, control algorithm, system design, hardware implementation and experimental test of a Manta-type Unmanned Underwater Vehicle (MUUV). The vehicle has one thruster for longitudinal propulsion, one rudder for heading angle control and two elevators for depth control. It is equipped with a pressure sensor for measuring water depth and Doppler Velocity Log for measuring position and angle. The vehicle is controlled by an on-board PC, which runs with the Windows XP operating system. The dynamic model of 6DOF is derived including the hydrodynamic forces and moments acting on the vehicle, while the hydrodynamic coefficients related to the forces and moments are obtained from experiments or estimated numerically. We also utilized the values obtained from PMM (Planar Motion Mechanism) tests found in the previous publications for numerical simulations. Various controllers such as PID, Sliding mode, Fuzzy and $H{\infty}$ are designed for depth and heading angle control in order to compare the performance of each controller based on simulation. In addition, experimental tests are carried out in a towing tank for depth keeping and heading angle tracking.

Characteristic Analysis of Air-gap Control System in Performance Test Machine of a LIM for Railway Transit (철도차량용 선형유도전동기 성능시험기의 공극조절 시스템 특성 연구)

  • Park, Chan-Bae;Lee, Hyung-Woo;Lee, Byung-Song;Park, Hyun-June;Kwon, Sam-Young;Han, Kyung-Hee
    • Proceedings of the KSR Conference
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    • 2008.06a
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    • pp.1955-1961
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    • 2008
  • A lot of researches on a linear induction motor(LIM) have been advanced to realize a traction system with high efficiency and performance for railway transit for a long time. However, most of them are limited in design of a LIM part such as Primary and Secondary. At a LIM which is traveling, the change of an air-gap(It occurs by a construction tolerance of a secondary reaction plate) becomes the cause which decreases a smoother ride and the efficiency of railway transit system. Therefore, uniform air-gap operation of LIM is important issue to improve the system efficiency. However, the researches which control the air-gap length of the LIM with technical and high-cost problem have been not advanced a lot. Therefore, in this research, it is introduced an air-gap control system for performance test machine of a scale-downed LIM which is able to control the air-gap length of the LIM and monitor a variety of performance changes of the propulsion system, and conducted a research on feasibility of the system based on characteristic analysis.

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SENSORLESS CONTROL FOR INDUCTION MOTOR USED IN TRACTION APPLICATION (견인용 유도전동기의 센서리스 제어)

  • Ryoo, Hong-Je;Kim, Jong-Soo;Rim, Geun-Hie;Kisck, Dragos Ovidiu;Won, Chung-Yuen
    • Proceedings of the KIEE Conference
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    • 2000.07b
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    • pp.1136-1139
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    • 2000
  • The paper describes a new and rigorous mathematical model for the rotor field oriented system with induction motor which uses the estimated speed and rotor flux based on a Model Reference Adaptive System, as well as the real-time approach. The estimated speed and rotor flux is used for the speed and flux feedback control. The stability and the convergence of the estimator are improved on the basis of hyperstability theory for non-linear systems. The real-time controller and estimator are implemented with a sampling period of $926{\mu}s$ using a dual TMS320C44 floating-point digital signal processor. The validity of the proposed method is verified by simulation, and also, the sensorless control was tested on the propulsion system simulator, used for the development of Korean High-Speed Railway Train (KHSRT) [5].

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A Study on the Design of Controller for Speed Control of the Induction Motor in the Train Propulsion System-1 (열차추진시스템에서 유도전동기의 속도제어를 위한 제어기 설계에 대한 연구-1)

  • Lee, Jung-Ho;Kim, Min-Seok;Lee, Jong-Woo
    • Journal of the Korean Society for Railway
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    • v.13 no.2
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    • pp.173-178
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    • 2010
  • Electric railroad systems consist of supply system of electric power and electric locomotive. The electric locomotive is adapted to high speed driving and mass transportation due to obtaining high traction force. The electric locomotive is operated by motor blocks and traction motors. Train speed is controlled by suppling power from motor blocks to traction motors according to reference speed. Speed control of the electric locomotive is efficient by spending minimum energy between motor blocks and traction motors. Recently, induction motors have been used than DC and synchronized motors as traction motors. Speed control of induction motors are used by vector control techniques. In this paper, speed of the induction motor is controlled by using the vector control technique. Control system model is presented by using Simulink. Pulse is controlled by PI and hysteresis controller. IGBT inverter is used for real-time control and system performance is demonstrated by simulating the induction motor which has 210[kW] on the output power.