• Title/Summary/Keyword: 유도성능

Search Result 2,254, Processing Time 0.041 seconds

Improvement of Speed Control for Spindle Induction Motor in the Field Weakening Region using a Fuzzy Controller (퍼지 제어기를 이용한 약계자 영역에서 스핀들 유도전동기의 속도제어 개선)

  • Yu, Jae-Sung;Sin, Soo-Cheol;Yoon, Ju-Man;Won, Chung-Yuen;Kim, Sang-Hoon
    • Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
    • /
    • v.19 no.8
    • /
    • pp.48-55
    • /
    • 2005
  • This paper presents a new speed control scheme of the spindle induction motor(IM) using fuzzy controller(FC) in field weakening region. The implementation of the proposed FC based spindle Induction Motor(IM) is compared to those obtained from the conventional PI controller based drive system. The simulation and experimental results show that the FC is the high performance more than the conventional PI speed controller in the spindle drive systems.

Flame deflector design of test facility to propulsion system model (추진기관 시스템 시험설비의 화염유도로 설계)

  • Jeon, Sung-Bok;Lee, Jae-Ho;Lee, Kwang-Jin;Cho, Nam-Kyung
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2012.05a
    • /
    • pp.597-602
    • /
    • 2012
  • Flame deflector is an important plan item for protecting propulsion system model, test facility, and life. This study suggests the way of flame deflector design in test facility evaluating performance of 75 ton and 300ton PSM. The flame deflector height was designed as 30m using a slope way in establishment location of facility. The flame deflector suitability was considered according to the shape of open and closed type. Also the cooling duct was made as modeling in accordance with core and side injection type.

  • PDF

Optimal Soft Landing Guidance and Attitude Control for Reusable Launch Vehicles (재사용 발사체를 위한 최적 연착륙 유도 및 자세 제어 연구)

  • Jeon, Ho-Young;Cho, Jun-Hyon;Kim, Jong-Han
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.50 no.4
    • /
    • pp.251-257
    • /
    • 2022
  • We formulated the convex optimization based minimum energy soft landing problem for reusable launch vehicles, and obtained the minimum time trajectory via the bisection search. In order to implement the the optimal guidance command and complete the flight control architectures on the soft landing stage, we designed the classical attitude control loops, and formulated and solved the optimal actuator allocation problem. The obtained soft landing guidance performance was analyzed via nonlinear 6-DOF simulation.

Performance of Adaptive Maximum Torque Per Amp Control at Multiple Operating Points for Induction Motor Drives (유도전동기 드라이브에서의 단위전류당 최대토크적응 제어기의 다운전점에서의 성능 연구)

  • Kwon, Chun-Ki;Kong, Yong-Hae
    • Journal of the Korea Academia-Industrial cooperation Society
    • /
    • v.19 no.3
    • /
    • pp.584-593
    • /
    • 2018
  • The highly efficient operation of induction motors has been studied in the past years. Among the many attempts made to obtain highly efficient operation, Maximum Torque Per Amp (MTPA) controls in induction motor drives were proposed. This method enables induction motor drives to operate very efficiently since it achieves the desired torque with the minimal stator current. This is because the alternate qd induction motor model (AQDM) is a highly accurate mathematical model to represent the dynamic characteristics of induction motors. However, it has been shown that the variation of the rotor resistance degrades the performance of the MTPA control significantly, thus leading to its failure to satisfy the maximum torque per amp condition. To take into consideration the mismatch between the actual value of the rotor resistance and its parameter value in the design of the control strategy, an adaptive MTPA control was proposed. In this work, this adaptive MTPA control is investigated in order to achieve the desired torque with the minimum stator current at multiple operating points. The experimental study showed that (i) the desired torque was accurately achieved even though there was a deviation of the order of 5% from the commanded torque value at a torque reference of 25 Nm (tracking performance), and (ii) the minimum stator current for the desired torque (maximum torque per amp condition) was consistently satisfied at multiple operating points, as the rotor temperature increased.

Assessment of Power Generation by Pressure Retarded Osmosis Process from Spiral-Wound Membrane Pilot-Plant (나권형 모듈을 이용한 압력지연삼투 공정의 에너지생산에 관한 연구)

  • Go, Gil hyun;Park, Tae shin;Kang, Lim seok
    • Journal of Korean Society of Environmental Engineers
    • /
    • v.38 no.9
    • /
    • pp.476-481
    • /
    • 2016
  • Pressure retarded osmosis (PRO) is a quite new technique for power generation using an osmotically driven membrane process. In the PRO process, water permeates through a semipermeable membrane from a low concentration feed solution to a high concentration draw solution due to osmotic pressure. This study carried out to evaluate the performance of the 8 in spiral wound membrane module using reverse osmosis concentrate for a draw solution and reverse osmosis permeate for a feed solution. Three different flowrates of draw and feed solution, such as 2.4 L/min, 5.0 L/min, and 10.0 L/min were used to estimate the power density and water flux under various range of hydraulic pressure differences between 5 bar and 30 bar. In addition, the effects of feed and draw solution concentration, flowrate, and mixing ratio on 8 in spiral wound PRO membrane module performance were investigated in this study. As major results, increases of the draw solution concentration lead to the improvement of power denstiy, and water flux. Also, increase of flowrate resulted in the improvement of power density and water flux. In addition, optimal mixing ratio of draw and feed solution inlet flowrate was found to be 1:1 to attain a maximum power denstiy.

Development of the Inductive Proximity Sensor Module for Detection of Non-contact Vibration (비접촉 진동 검출을 위한 유도성 근접센서모듈 개발)

  • Nam, Si-Byung;Yun, Gun-Jin;Lim, Su-Il
    • Journal of the Korea Society of Computer and Information
    • /
    • v.16 no.5
    • /
    • pp.61-71
    • /
    • 2011
  • To measure the fatigue of metallic objects at high speed vibration while non-contact precision displacement measurement on how to have a lot of research conducted. Noncontact high-speed vibration detection sensor of the eddy current sensors and laser sensors are used, but it is very expensive. Recently, High-speed vibrations detection using an inexpensive inductive sensor to have been studied, but is still a beginner. In this paper, a new design of an inexpensive inductive proximity sensor has been suggested in order to measure high frequency dynamic displacements of metallic specimens in a noncontact manner. Detection of the existing inductive sensors, detection, integral, and amplified through a process to detect the displacement noise due to weak nature of analog circuits and integral factor in the process of displacement detection is slow. The proposed method could be less affected by noise, the analog receive and high-speed signal processing is a new way, because AD converter (Analog to Digital converter) without using the vibration frequency signals directly into digital signals are converted. In order to evaluate the sensing performance, The proposed sensor module using non-contact vibration signals were detected while shaker vibration frequencies from 30Hz to 1,100 Hz at intervals of vibrating metallic specimens. Experimental results, Vibration frequency detection range of the metallic specimins within close proximity to contactless 5mm could be measured from DC to 1,100Hz and vibration amplitude of the resolution was $20{\mu}m$. Therefore, the proposed non-contact inductive sensor module for precision vibration detection sensor is estimated to have sufficient performance.

Model-Based Design and Enhancement of Operational Procedure for Guided Missile Flight Test System (유도무기 비행시험 시스템을 위한 모델 기반 운용절차의 설계 및 개선)

  • Park, Woong;Lee, Jae-Chon
    • Journal of the Korea Academia-Industrial cooperation Society
    • /
    • v.20 no.4
    • /
    • pp.479-488
    • /
    • 2019
  • The flight test operational procedure artifact includes mission planning, execution methods, and safety measures for each step of test progress. As the development of guided missiles has become more advanced and strategic, flight test has become increasingly complex and broadened. Therefore, increased reliability of the flight test operation procedures was required to ensure test safety. Particularly, the design of the flight test operational procedures required verification through M&S to predict and prepare for the uncertainty in a new test. The relevant studies have published the optimal framework development for flight tests and the model-based improvements of flight test processes, but they lacked the specificity to be applied directly to the flight test operational procedures. In addition, the flight test operational procedures, which consist of document bases, have caused problems such as limitations of analysis capabilities, insensitive expressions, and lack of scalability for the behavior and performance analysis of test resources. To improve these problems, this paper proposes how to design operational procedure of guided missile flight test system by applying MBSE(Model-based Systems Engineering). This research has improved reliability by increasing the ability to analyze the behavior and performance of test resources, and increased efficiency with the scalability applicable to multiple flight tests. That can be also used continuously for the guided missile flight tests that will be developed in the future.

Performance analysis of TR-UWB systems using Frequency-components (주파수 성분을 이용한 TR-UWB 시스템의 성능분석)

  • Jang, Dong-Heon;Yang, Hoon-Gee
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
    • /
    • 2008.05a
    • /
    • pp.985-988
    • /
    • 2008
  • This paper introduces a new TR-UWB system, using frequency-domain components of UWB pulses. This is achieved by separating converted frequency-components into real and imaginary parts, and both parts are correlated and effectively combined. We make an analysis that the new scheme improves performance compared with a conventional by complex correlation computing. The simulation results confirmed that the proposed scheme has better performance than existing system.

  • PDF

Study on Improvement of Deperming Performance Applied Dead Time (Dead Time 적용에 따른 탈자 성능향상에 관한 연구)

  • Kim, Jong-Wang;Kim, Ji-Ho;Chung, Hyun-Ju;Lee, Hyang-Beom
    • Proceedings of the KIEE Conference
    • /
    • 2011.07a
    • /
    • pp.1065-1066
    • /
    • 2011
  • 본 논문에서는 함정의 피탐지 성능 개선을 위한 기초 연구로 dead time 적용시 탈자 프로토콜 변화에 따른 탈자 성능 분석에 관한 연구를 하였다. 함정의 재질은 SM45C로 원통의 형태이다. 자기장 측정에 사용한 자기센서는 영국 Bartington Instruments사의 MAG-03MCB70(Three-Axis Fluxgate Magnetometer)을 사용하였으며, inter-cardinal run 방법을 이용하여 유도자기장과 영구자기장을 분리하였다. Anhyteretic deperm 프로토콜을 적용하여 탈자를 진행하였고 전류의 지속시간이 증가하는 경우에 비하여 dead time을 적용하였을 경우 탈자 성능이 향상된 결과를 얻을 수 있었다.

  • PDF

Closed-form BER expressions for performance of Alamouti STC (Alamouti 공간시간부호의 성능분석을 위한 closed-form BER 표현)

  • Kong Hyung-Yun;Khuong Ho Van
    • The KIPS Transactions:PartC
    • /
    • v.12C no.5 s.101
    • /
    • pp.673-678
    • /
    • 2005
  • Alamouti STC (Space-Time Code) is a part of the UMTS-WCDMA standard. However, up to the best of our knowledge no closed-form BER formula for this famous code exists. Evaluating its performance through simulations is time-consuming and therefore, there should be analytical BER graphs to serve as a reference which are derived in this paper for coherently BPSK-modulated data.