• 제목/요약/키워드: control input saturation

검색결과 128건 처리시간 0.025초

Real Time Road Lane Detection with RANSAC and HSV Color Transformation

  • Kim, Kwang Baek;Song, Doo Heon
    • Journal of information and communication convergence engineering
    • /
    • 제15권3호
    • /
    • pp.187-192
    • /
    • 2017
  • Autonomous driving vehicle research demands complex road and lane understanding such as lane departure warning, adaptive cruise control, lane keeping and centering, lane change and turn assist, and driving under complex road conditions. A fast and robust road lane detection subsystem is a basic but important building block for this type of research. In this paper, we propose a method that performs road lane detection from black box input. The proposed system applies Random Sample Consensus to find the best model of road lanes passing through divided regions of the input image under HSV color model. HSV color model is chosen since it explicitly separates chromaticity and luminosity and the narrower hue distribution greatly assists in later segmentation of the frames by limiting color saturation. The implemented method was successful in lane detection on real world on-board testing, exhibiting 86.21% accuracy with 4.3% standard deviation in real time.

Dynamic Anti-Windup for Robot Systems with Friction

  • Yoon, S.S.;Yamada, Y.;Park, J.K.;Yoon, T.W.
    • 제어로봇시스템학회:학술대회논문집
    • /
    • 제어로봇시스템학회 2005년도 ICCAS
    • /
    • pp.1966-1971
    • /
    • 2005
  • Though several previous anti-windup techniques have been proposed, they are limited to linear systems or friction is not considered. Thus this paper proposes a compensation scheme for input-constrained robot systems with friction to cope with the windup phenomenon and shows its effectiveness by simulations. Given a feedback linearizing controller for a robot system designed without considering its input constraint, an additional dynamic compensator is proposed to account for the constraint. The dynamic anti-windup is based on the minimization of a reasonable performance index, and properties of the resulting closed-loop are presented.

  • PDF

A STUDY ON SIMPLE TIME VARYING FEEDFORWARD COMPENSATOR

  • Kwon, Byung-Moon;Son, Won-Kee;Kwon, Oh-Kyu
    • 제어로봇시스템학회:학술대회논문집
    • /
    • 제어로봇시스템학회 2000년도 제15차 학술회의논문집
    • /
    • pp.500-500
    • /
    • 2000
  • In this paper, we deal wit,11 a simple tim varying feedforward compensator in order to decrease the amount of undershoots and overshoots on the step response. This compensator makes the step type input be a ramp input with saturation for 0 $\leq$ t < $\alpha$. It will be shown that the system with the feedforward compensator has small amount of undershoot and overshoot at the price of rise time. Also, provided the system properly stable, the influence of the design parameter $\alpha$ on the step response of the system with the feedforward compensator is investigated in the current paper.

  • PDF

강인 내부 보상기를 이용한 새로운 강인 제어기 설계 (A Novel Robust Controller Design using Robust Internal-loop Compensator)

  • 최현택;서일홍
    • 대한전기학회논문지:전력기술부문A
    • /
    • 제48권8호
    • /
    • pp.987-995
    • /
    • 1999
  • A new robust controller design methodology for single-input single-output systems is proposed, where the proposed controller consists of a conventional or optimal servo controller at the outer loop as well as the robust internal-loop compensator(RIC) to eliminate the model uncertainty and external disturbance. It is shown that RIC with finite gain can make actual systems be nominal models within a prespecified error bound. And, it is also shown that RIC-based system is robustly stable regardless of input saturation. Several numerical examples are illustrated to show validities of the proposed robust controller.

  • PDF

Study of Flooding Prevention on Cathode Gas Diffusion Layer for Dynamic Load Fuel Cell

  • Choi, Dong-Won;You, Jin-Kwang;Rokhman, Fatkhur;Bakhtiar, Agung;Choi, Kwang-Hwan
    • 한국태양에너지학회:학술대회논문집
    • /
    • 한국태양에너지학회 2011년도 추계학술발표대회 논문집
    • /
    • pp.270-273
    • /
    • 2011
  • Water management is important in proton exchange membrane fuel cell because the water balance has a significant impact on the overall fuel cell system performance. In fuel cell vehicle, the vehicle's power demand is dynamic; therefore, the dynamic water management system is required. This present study proposes a method to control the humidity of the input air in cathode side of the fuel cell vehicle. The simulation using several driving cycles shows the proposed air humidification control obtains a relatively good result. The liquid saturation level is seen constant at the target level although still there are small deviations at driving cycles which having averagely high power demands.

  • PDF

적응 퍼지제어기를 이용한 서보 제어 시스템의 정밀제어 (High Precision Control of Servo Control System Using The Adaptive Fuzzy Controller)

  • 조정환
    • 조명전기설비학회논문지
    • /
    • 제16권3호
    • /
    • pp.110-115
    • /
    • 2002
  • 포화, 릴레이, 히스테리시스, 불감대와 같은 비선형성이 존재하는 자동화 시스템의 정밀제어를 위하여 마이크로프로세서를 이용한 적응 퍼지제어 시스템을 제안한다. 제안된 시스템은 제어 영역을 과도상태 영역과 적응제어 영역으로 분리하였다. 먼저 기준 입력신호와 귀환신호의 주파수 타이에 비례하는 출력전압을 발생시켜서 시스템을 구동하는 주파수 동기 방식을 이용하여 신속한 과도응답을 수행하고, 오차가 설정된 범위 안에 들어오면 퍼지논리를 이용한 적웅 퍼지제어 방식에 의해 시스템을 제어하여 정밀제어를 수행한다. 이론과 실험적인 연구가 수행되었고, 그 결과는 서보 제어 시스템의 정밀제어 성능이 개선되었음을 입증한다.

출력기반 적응제어기법을 이용한 틸트로터 항공기의 회전익 모드 설계연구 (Flight Control of Tilt-Rotor Airplane In Rotary-Wing Mode Using Adaptive Control Based on Output-Feedback)

  • 하철근;임재형
    • 한국항공우주학회지
    • /
    • 제38권3호
    • /
    • pp.228-235
    • /
    • 2010
  • 본 논문에서는 틸트로터 항공기의 회전익 모드에 대한 자율비행 유도제어 알고리즘을 적응제어기법을 이용하여 설계하는 것이다. 이를 위해 우선 출력기반 근사적 궤환선형화 기법을 통하여 알고리즘의 내부루프를 구성하고 그로부터 발생하는 모델오차를 단일 은닉층-신경망을 적용하여 상쇄하였다. 그리고 리아푸노프 안정성 이론에 따른 적응제어 갱신법칙은 선형 관측기를 기반으로 설계하였다. 나아가 외부루프는 경로점 유도법칙으로부터 생성되는 궤적을 추종하도록 하였으며 특히 엄밀한 자동착륙 궤적추종 성능 향상을 위하여 방향각 및 비행경로각 시선유도법칙을 설계하였다. 틸트로터 비선형 모델 시뮬레이션 결과는 콜렉티브 입력에서 보이는 순간적인 작동기 포화현상 이외에는 만족할 만한 안정성과 추종성능을 보여 주고 있다.

틸트로터 항공기의 경로점 추종 비행유도제어 알고리즘 설계 : 헬리콥터 비행모드 (Guidance and Control Algorithm for Waypoint Following of Tilt-Rotor Airplane in Helicopter Flight Mode)

  • 하철근;윤한수
    • 제어로봇시스템학회논문지
    • /
    • 제11권3호
    • /
    • pp.207-213
    • /
    • 2005
  • This paper deals with an autonomous flight guidance and control algorithm design for TR301 tilt-rotor airplane under development by Korea Aerospace Research Institute for simulation purpose. The objective of this study is to design autonomous flight algorithm in which the tilt-rotor airplane should follow the given waypoints precisely. The approach to this objective in this study is that, first of all, model-based inversion is applied to the highly nonlinear tilt-rotor dynamics, where the tilt-rotor airplane is assumed to fly at helicopter flight mode(nacelle angle=0 deg), and then the control algorithm, based on classical control, is designed to satisfy overall system stabilization and precise waypoint following performance. Especially, model uncertainties due to the tiltrotor model itself and inversion process are adaptively compensated in a simple neural network(Sigma-Phi NN) for performance robustness. The designed algorithm is evaluated in the tilt-rotor nonlinear airplane in helicopter flight mode to analyze the following performance for given waypoints. The simulation results show that the waypoint following responses for this algorithm are satisfactory, and control input responses are within control limits without saturation.

냉각 통풍홀 설계로 인한 견인 전동기 특성 및 제어 성능 영향 연구 (Effect on the Characteristics and Control Performance due to the Ventilation Hole Design of the Traction Motor)

  • 김기찬;이정일;권중록
    • 대한전기학회:학술대회논문집
    • /
    • 대한전기학회 2001년도 하계학술대회 논문집 B
    • /
    • pp.801-803
    • /
    • 2001
  • On this study the motor design method with fairly good characteristics and control capability as well as cooling capability is presented with considering the magnetic effect due to ventilation hole, which is installed to prevent the temperature rise. When the input voltage rises due to critical variation in traction power supply system, the final ventilation hole is presented by checking the inductance parameter with clarifying the relation between saturation of the motor core and the ventilation hole.

  • PDF

전산모사에 의한 공압구동장치의 비선형 해석 (Nonlinear analysis of a pneumatic actuation system by digital simulation)

  • 조택동;신효필;문의준
    • 제어로봇시스템학회:학술대회논문집
    • /
    • 제어로봇시스템학회 1991년도 한국자동제어학술회의논문집(국내학술편); KOEX, Seoul; 22-24 Oct. 1991
    • /
    • pp.1104-1109
    • /
    • 1991
  • Recently, Pneumatic Actuation System (PAS) has been used increasingly as a high performance fin-control servo actuation systems because of the special advantages of pneumatic units: primarily their low cost, small size, light weight, and tolerance to broad temperature extremes. In this study, a nonlinear model of PAS is derived through the detailed analysis of the major components in the typical system. The model includes nonlinear flow-pressure relationships of the flow through the solenoid valve openings and orifices, PWM algorithm for driving two solenoid valves as a closed-center 3-way valve for minimum gas consumption, solenoid valve dynamics, saturation, and friction. Simulation results are compared with the experimental ones for square and sinusoidal inputs to see the validity of the model. Independent of the shape and magnitude of the input signals, both results are in good agreements with minor difference.

  • PDF