• Title/Summary/Keyword: Model-based engine control

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Control of throttle actuator system based on time delay control (시간지연제어에 기초한 스로틀액츄에이터 시스템의 제어)

  • Song, Jae-Bok;Byeon, Kyeong-Seok
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.21 no.12
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    • pp.2081-2089
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    • 1997
  • Accurate positioning of the throttle valve of a gasoline engine is required to implement various systems such as traction control system(TCS), cruise control system and drive-by-wire system. In this research, position control system has been developed for the throttle actuator system that uses one throttle actuation for small volume and DC servo motor for fast response. In order to drive the DC motor, PWM signal generator and PWM amplifier were built and interfaced to the motor and controller. Also, time delay control(TDC) law has been used as a basic control algorithm. A method of varying the reference model of the TDC according to the size of change in target throttle angle is proposed here. The simulation and experimental results show that both overshoot prevention and fast response are achieved by the TDC technique with this variable reference model.

A Research on Control Method Design for the Intake Flow of a Dual Combustion Ramjet Engine using Multiple Control Inputs (다중의 제어입력을 이용한 이중연소 램제트 엔진의 흡입구 유동 제어기법 연구)

  • Park, Jungwoo;Park, Iksoo;Kim, Junghoe;Hwang, Kiyoung
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.5
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    • pp.49-58
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    • 2018
  • This paper introduces a research on the control method design for the subsonic intake flow of a dual-combustion ramjet engine. To design the control method, the intake flow dynamic response characteristics, based on a designated flow condition and intake geometry, are investigated, and a control method concept considering the intake flow characteristics is established. Using a dynamic simulation model of a dual-combustion ramjet, control input/output linearized models are obtained such that a control loop design based on linearized models can be accomplished. Finally, from various control loop simulations, the performance of the control method, including its control loop stability, is evaluated.

Improved 3-DOF Attitude Control of a Model Helicopter using Fuzzy-Tuning PID Controller (퍼지 동조 PID 제어기를 이용한 모형 헬리콥터의 개선된 3자유도 자세제어)

  • Park, Mun-Soo;Park, Duck-Gee;Jung, Won-Jae;Kim, Byung-Do;Hong, Suk-Kyo
    • Proceedings of the KIEE Conference
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    • 2001.07d
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    • pp.2470-2472
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    • 2001
  • This paper describes the application of a fuzzy-tuning PID controller to a 3-DOF attitude control of a small model helicopter in hover for the compensation of coupling effects between each axis and system uncertainties due to the variation of engine RPM. A Low-level PID controller is designed by Ziegler-Nichols method and its gains are tuned by a high-level fuzzy system based on error states and its time derivatives. The experimental results show that the attitude control performance of fuzzy-tuning PID controller is improved comparing with that of a Ziegler-Nichols PID controller and fuzzy controller.

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An RDF Ontology Access Control Model based on Relational Database (관계형 데이타베이스 기반의 RDF 온톨로지 접근 제어 모델)

  • Jeong, Dong-Won
    • Journal of KIISE:Databases
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    • v.35 no.2
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    • pp.155-168
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    • 2008
  • This paper proposes a relational security model-based RDF Web ontology access control model. The Semantic Web is recognized as a next generation Web and RDF is a Web ontology description language to realize the Semantic Web. Much effort has been on the RDF and most research has been focused on the editor, storage, and inference engine. However, little attention has been given to the security issue, which is one of the most important requirements for information systems. Even though several researches on the RDF ontology security have been proposed, they have overhead to load all relevant data to memory and neglect the situation that most ontology storages are being developed based on relational database. This paper proposes a novel RDF Web ontology security model based on relational database to resolve the issues. The proposed security model provides high practicality and usability, and also we can easily make it stable owing to the stability of the relational database security model.

Development of a Real-time Driving Simulator for ACC(Adaptive-Cruise-Control) Performance Evaluation (적응 순항 제어기 성능 평가를 위한 실시간 차량 시뮬레이터 개발)

  • Han, Dong-Hoon;Yi, Kyong-Su
    • Transactions of the Korean Society of Automotive Engineers
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    • v.14 no.3
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    • pp.28-34
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    • 2006
  • An ACC driving simulator is a virtual reality device which designed to test or evaluate vehicle control algorithm. It is designed and built based on the rapid control prototyping(RCP) concept. Therefore this simulator adopt RCP tools to solve the equation of a vehicle dynamics model and control algorithm in real time, rendering engine to provide real-time visual representation of vehicle behavior and CAN communication to reduce networking load. It can provide also many different driving test environment and driving scenarios.

Coordinated Droop Control for Stand-alone DC Micro-grid

  • Kim, Hyun-Jun;Lee, Yoon-Seok;Kim, Jae-Hyuk;Han, Byung-Moon
    • Journal of Electrical Engineering and Technology
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    • v.9 no.3
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    • pp.1072-1079
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    • 2014
  • This paper introduces a coordinated droop control for the stand-alone DC micro-grid, which is composed of photo-voltaic generator, wind power generator, engine generator, and battery storage with SOC (state of charge) management system. The operation of stand-alone DC micro-grid with the coordinated droop control was analyzed with computer simulation. Based on simulation results, a hardware simulator was built and tested to analyze the performance of proposed system. The developed simulation model and hardware simulator can be utilized to design the actual stand-alone DC micro-grid and to analyze its performance. The coordinated droop control can improve the reliability and efficiency of the stand-alone DC micro-grid.

Variable stability system control law development for in-flight simulation of pitch/roll/yaw rate and normal load

  • Ko, Joon Soo;Park, Sungsu
    • International Journal of Aeronautical and Space Sciences
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    • v.15 no.4
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    • pp.412-418
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    • 2014
  • This paper describes the development of variable stability system (VSS) control laws for the KFA-i to simulate the dynamics of KFA-m aircraft. The KFA-i is a single engine, Class IV aircraft and was selected as an in-flight simulator (IFS) aircraft, whereas the KFA-m is a simulated aircraft that is based on the F-16 aircraft. A 6-DoF math model of KFA-i aircraft was developed, linearized, and separated into longitudinal and lateral motion for VSS control law synthesis. The KFA-i aircraft has five primary control surfaces: two flaperons, two all movable horizontal tails, and one rudder. Flaperons are used for load control, the horizontal tails are used for pitch and roll rate control, and the rudder is used for yaw rate control. The developed VSS control law can simulate four parameters of the KFA-m aircraft simultaneously, such as pitch, roll, yaw rates, and load. The simulation results show that KFA-i follows the responses of KFA-m with high accuracy.

A 3D Audio-Visual Animated Agent for Expressive Conversational Question Answering

  • Martin, J.C.;Jacquemin, C.;Pointal, L.;Katz, B.
    • 한국정보컨버전스학회:학술대회논문집
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    • 2008.06a
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    • pp.53-56
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    • 2008
  • This paper reports on the ACQA(Animated agent for Conversational Question Answering) project conducted at LIMSI. The aim is to design an expressive animated conversational agent(ACA) for conducting research along two main lines: 1/ perceptual experiments(eg perception of expressivity and 3D movements in both audio and visual channels): 2/ design of human-computer interfaces requiring head models at different resolutions and the integration of the talking head in virtual scenes. The target application of this expressive ACA is a real-time question and answer speech based system developed at LIMSI(RITEL). The architecture of the system is based on distributed modules exchanging messages through a network protocol. The main components of the system are: RITEL a question and answer system searching raw text, which is able to produce a text(the answer) and attitudinal information; this attitudinal information is then processed for delivering expressive tags; the text is converted into phoneme, viseme, and prosodic descriptions. Audio speech is generated by the LIMSI selection-concatenation text-to-speech engine. Visual speech is using MPEG4 keypoint-based animation, and is rendered in real-time by Virtual Choreographer (VirChor), a GPU-based 3D engine. Finally, visual and audio speech is played in a 3D audio and visual scene. The project also puts a lot of effort for realistic visual and audio 3D rendering. A new model of phoneme-dependant human radiation patterns is included in the speech synthesis system, so that the ACA can move in the virtual scene with realistic 3D visual and audio rendering.

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Development of a Work Management System Based on Speech and Speaker Recognition

  • Gaybulayev, Abdulaziz;Yunusov, Jahongir;Kim, Tae-Hyong
    • IEMEK Journal of Embedded Systems and Applications
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    • v.16 no.3
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    • pp.89-97
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    • 2021
  • Voice interface can not only make daily life more convenient through artificial intelligence speakers but also improve the working environment of the factory. This paper presents a voice-assisted work management system that supports both speech and speaker recognition. This system is able to provide machine control and authorized worker authentication by voice at the same time. We applied two speech recognition methods, Google's Speech application programming interface (API) service, and DeepSpeech speech-to-text engine. For worker identification, the SincNet architecture for speaker recognition was adopted. We implemented a prototype of the work management system that provides voice control with 26 commands and identifies 100 workers by voice. Worker identification using our model was almost perfect, and the command recognition accuracy was 97.0% in Google API after post- processing and 92.0% in our DeepSpeech model.

Flight Attitude Control of using a Fuzzy Controller (퍼지제어기를 이용한 비행 자세제어)

  • Park, Jong-Oh;Sul, Jae-Hoon;Kim, Sung-Chul;Lim, Young-Do
    • Journal of the Korean Institute of Intelligent Systems
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    • v.13 no.1
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    • pp.91-96
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    • 2003
  • The forces and moments at the aircraft c.g. have components due to aerodynamic effects and to engine thrust. For the flight stability and autopilot systems we present a attitude control method using an intelligent control algorithm Which is based on the control rules from experts knowledge concerning the motion equations and other experiences. Then a robust fuzzy controller is developed to control the flight attitude. The controller can deal with multiple inputs and outputs. We have made an aircraft model and the orientation sensor for experimental flights. The control rules based on the flight expert s experience and knowledge can be programmed by fuzzy rules, and determined control rules by experimental flight. We can be stable attitude control by fuzzy controller.