• 제목/요약/키워드: roll to roll system

검색결과 904건 처리시간 0.031초

소형어선의 전복방지화 안정장치 시스템 개발에 관한 연구 (Development of a Stability System to prevent a Capsize of a Small Fishing Vessel)

  • 천승현;전호환;김창훈;김시영
    • 한국해양공학회지
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    • 제13권1호통권31호
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    • pp.130-137
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    • 1999
  • The wing-flap stabilizing system attached under the hull bottom of a small fishing vessel to prevent the capsize by controlling the roll motions has been developed. This paper describes the background of the system design together with the experimental results. The effectiveness of the system is proven by the towing tank tests with a 1/4 scale model, showing that the roll motions of the model are much reduced by the active flap control in multidirectional irregular waves forward speeds.

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ROLL CENTER ANALYSIS OF A HALF-CAR MODEL USING POLE FOR SMALL DISPLACEMENT

  • Lee, J.K.;Shim, J.K.
    • International Journal of Automotive Technology
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    • 제7권7호
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    • pp.833-839
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    • 2006
  • In this paper, roll behavior of three planar half car models are compared. The first model is a simple model whose contact point between a wheel and the ground is assumed to be fixed with a revolute joint. The second model is a modified model of the fIrst model, whose wheel tread width can vary. In this model, the instant center of a wheel with respect to the ground, which is crucial to find the roll center, is assumed to be at the contact point of a wheel and the ground. The last model uses the pole of a wheel with respect to the ground for small displacement as the instant center of a wheel with respect to the ground. Loci of the center of gravity point, the fixed and the moving centrodes which are traces of roll center position in the ground and the body frame respectively, wheel contact points, and instant centers of a wheel with respect to the ground are calculated.

선회 조향시 강건 제어에 의한 롤 안정성 개선 (Improving the Roll Stability of a Vehicle by H$_{\infty}$ Control)

  • 김효준;양현석;박영필
    • 한국자동차공학회논문집
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    • 제9권3호
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    • pp.92-99
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    • 2001
  • This paper presents a simulation study using a robust controller to improve the roll stability of a vehicle. The controller is designed in the framework of an output feedback H$_{\infty}$ control scheme based on the 3DOF linear vehicle model, solving the mixed-sensitivity problem to guarantee the robust stability and disturbance rejection with respect to parameter variations due to laden and running vehicle conditions. In order to investigate the feasibility of the active roll control system in a real car, its performance is evaluated by simulation in a 10DOF full vehicle model with actuator dynamics and tire characteristics.

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무궁화위성의 정상운용모드에서의 자세제어 시스팀 (KOREASAT On-Orbit Normal Mode Attitude Control System)

  • 김동환;원종남;김성중;강성수;김한돌;이명수
    • 한국통신학회논문지
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    • 제19권3호
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    • pp.505-514
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    • 1994
  • 무궁화 위성체는 10년 수명기간 동안 통신 및 직접방송 위성서비스에 필요한 빔의 지향성을 유지하기 위하여 정확하고 신뢰성있는 자세제어 시스팀을 요구하고 있다. 본고에서는 무궁화 위성체가 정지궤도에서 정상운용모드로 동작하는데 요구되는 자세제어부속시스팀에 대한 상세설계기법 및 성능에 대해서 기술하고자 한다.

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채널 내를 비행하는 가변스팬 날개 공력특성 II (비대칭 날개 펼침) (Aerodynamic Characteristics of a Variable-Span Wing Flying Inside a Channel II (Effect of Asymmetric Wing Extensions))

  • 한철희
    • 항공우주시스템공학회지
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    • 제10권3호
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    • pp.39-43
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    • 2016
  • In this paper, a wind-tunnel test is accomplished to investigate the roll characteristics of a variable-span wing flying inside a channel. The factors that affect the roll characteristics of the wing were identified by analyzing the measured data; accordingly, when the wing is flying without both the ground and sidewall effects, the asymmetric wing extension causes the roll moment. Both the ground and the sidewall can increase the roll moment, but when the wing is affected by both the ground and the sidewall, the roll moment does not increase as much as the case where the wing is only affected by the ground. Also, the aerodynamic characteristics of the flying wing inside a channel are the nonlinear function of the wing height and the gap between the wingtip and the sidewall, both of which should be considered in a study of the stability and the flight control of the wing-in-ground effect of the vehicle flying inside a channel.

좌우 대칭 모자형 단면이 길이 방향으로 선형적으로 변하는 롤 포밍 공정의 개발 (Development of a Roll-Forming Process of Linearly Variable Symmetric Hat-type Cross-section)

  • 김광희;윤문철
    • 한국기계가공학회지
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    • 제14권4호
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    • pp.118-125
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    • 2015
  • The roll-forming process is a highly productive incremental forming process and is suitable for manufacturing thin, high-strength steel products. Recently, this process has been considered one of the most productive processes in manufacturing high-strength steel automotive structural parts. However, it is very difficult to develop the roll-forming process when the cross-sectional shape of the product changes in the longitudinal direction. In this study, a roll-forming process for manufacturing high-strength steel automotive parts with a linearly variable symmetric hat-type cross-section was developed. The forming rolls were designed by the 3D CAD system, CATIA. Additionally, the designed forming rolls were modified by the simulation through the 3D elastic-plastic finite element analysis software, MARC. The results of the finite element analysis show that the final roll-forming roll can successfully produce the desired high-strength steel automotive part with a variable cross-section.

볼과 소켓의 정밀 체결을 위한 회전성형 장치 (Rotary Forming Equipment for Precision Joining of the Ball and the Socket)

  • 전병윤;엄재근;전만수
    • 소성∙가공
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    • 제16권2호
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    • pp.132-137
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    • 2007
  • A double roll rotary forming equipment is presented in this paper. The equipment is developed for joining the socket with the ball of a concave piston assembly with its geometrical tolerance requirements satisfied. The equipment is composed of a lathe, a double roll system and a roll pressing unit driven by the hydraulic system. The workpiece rotates by spindle chuck of the lathe while the double roll system approaches perpendicularly to the central line of the workpiece. The equipment is successfully applied to precision joining of the ball and the socket fur the concave piston assembly of a high pressure hydraulic pump.

고속 롤투롤 인쇄기의 장력제어시스템 안정도 해석 (Stability Analysis of the Tension Control System of a High-speed Roll-to-Roll Printing Machine)

  • 강철구;이봉주
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회A
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    • pp.873-878
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    • 2007
  • Stability of high-speed roll-to-roll printing machines is one of the most important factors that are required for the printing machines to operate properly and to obtain reasonable printing performance. This paper proposes a new model for the web-tension system of a high-speed gravure printing machine considering span-length variations due to dancer rollers, and analyzes the stability of plant dynamics of the printing machine using the proposed model. Span-length variations due to dancer motions are considered for the modeling of plant dynamics in two ways; one is to include the effect of span-length variations without considering dancer inertias and viscous frictions, and the other is to include the effect of span-length variations with considering dancer inertias and viscous frictions. The stability of the plant model is analyzed for various web-speeds using the eigenvalues of the linearized model about operating points.

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칼만필터를 이용한 농용 균평헬리콥터의 살포비행자세 평가 (Evaluation of Spray Flight Attitude for Agricultural Roll-balanced Helicopter using Kalman Filter)

  • 박희진;구영모
    • Journal of Biosystems Engineering
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    • 제37권6호
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    • pp.342-351
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    • 2012
  • Purpose: Aerial spraying with an agricultural unmanned helicopter became a new paradigm in the agricultural practice. Laterally tilting behavior of a conventional agricultural helicopter, resulting in the biased down-wash and uneven spray deposit is a physically intrinsic phenomenon while hovering and cruise flights. Authors studied and developed a roll-balanced agricultural helicopter with a raised pylon tail rotor system. In this study, the attitude of the roll-balanced helicopter was determined using the Kalman filter algorithm, and the quality of roll balancing of a bare-airframe helicopter was evaluated. Methods: Instantaneous attitudes were estimated using the advantage of gyroscope, followed by the long term correction and prediction using accelerometer data for the advantage of convergence. The attitudes of the fuselage were calculated by applying the Kalman filter algorithm. The spraying maneuver of the helicopter was performed at a field of 50 m long, and the attitude data were acquired and evaluated. Results: The determination of attitude using the inertial measurement unit(IMU) and Kalman filter was reliable and practical. The intrinsic attitude of the developed helicopter was stable and roll-balanced. The deviation of roll angle was ${\pm}6.3^{\circ}$ with an average of $0^{\circ}$, referring to roll-balanced. Conclusions: Handling quality of the roll attitude determined to be steadily balanced. The balancing behavior of the developed helicopter would result in an even spray pattern during aerial application.

롤투롤 인쇄전자 시스템에서 인쇄패턴의 두께와 표면조도에 관한 통계적 분석 (Statistical Analysis for Thickness and Surface Roughness of Printed Pattern in Roll-to-Roll Printed Electronics System)

  • 이창우;김남석;김창완
    • 대한기계학회논문집A
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    • 제37권3호
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    • pp.287-294
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    • 2013
  • 롤투롤 인쇄전자 시스템은 높은 생산성과 낮은 원가를 이점으로 인쇄전자 산업에서 가장 각광을 받고 있는 인쇄기술 중 하나이다. 이러한 롤투롤 인쇄전자 시스템에서 인쇄패턴의 특성은 인쇄물의 기능적 성질을 결정짓는 중요한 문제라 할 수 있다. 따라서 본 연구에서는 인쇄패턴의 특성을 결정짓는 주요 인자들이 특별히 인쇄패턴의 두께와 표면 조도에 미치는 영향성에 대한 분석이 수행되었다. 실험계획법을 적용하여 인쇄패턴의 두께와 표면조도에 대한 각 인자의 주효과 및 교호작용 효과를 정량적으로 제시하였고, 분산분석을 통해 유의한 인자를 찾아내었다. 또한 이에 따르는 통계적 모델이 주요 인자의 함수로서 개발되었다. 이러한 결과는 롤투롤 전자인쇄 시스템의 특징에 따라 요구되는 인쇄패턴의 특성을 얻는데 활용될 수 있을 것이다.