• 제목/요약/키워드: Anti-torque

검색결과 81건 처리시간 0.025초

Steady-State Integral Proportional Integral Controller for PI Motor Speed Controllers

  • Hoo, Choon Lih;Haris, Sallehuddin Mohamed;Chung, Edwin Chin Yau;Mohamed, Nik Abdullah Nik
    • Journal of Power Electronics
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    • 제15권1호
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    • pp.177-189
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    • 2015
  • The output of the controller is said to exceed the input limits of the plant being controlled when a control system operates in a non-linear region. This process is called the windup phenomenon. The windup phenomenon is not preferable in the control system because it leads to performance degradation, such as overshoot and system instability. Many anti-windup strategies involve switching, where the integral component differently operates between the linear and the non-linear states. The range of state for the non-overshoot performance is better illustrated by the boundary integral error plane than the proportional-integral (PI) plane in windup inspection. This study proposes a PI controller with a separate closed-loop integral controller and reference value set with respect to the input command and external torque. The PI controller is compared with existing conventional proportional integral, conditional integration, tracking back calculation, and integral state prediction schemes by using ScicosLab simulations. The controller is also experimentally verified on a direct current motor under no-load and loading conditions. The proposed controller shows a promising potential with its ability to eliminate overshoot with short settling time using the decoupling mode in both conditions.

임플란트 보철물 나사의 전하중 유지에 나사 표면에 따른 혐기성 나사 고정제의 효과 (Effects of anaerobic sealing agents on preload maintenance of screw-retained implant prosthesis with surface of screws)

  • 류승범;허성주;곽재영;김성균
    • 대한치과보철학회지
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    • 제58권2호
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    • pp.103-109
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    • 2020
  • 목적: 본 연구의 목적은 임플란트 지대주 나사에 혐기성 나사 고정제의 적용 유무와 나사 종류에 따른 풀림 토크 값의 차이를 평가하는 것이다. 재료 및 방법: 외부 육각형 임플란트 고정체를 사용하였고, 동일한 제조사의 지대주와 지대주 나사가 사용되었다. 지대주 나사는 두 종류로 티타늄 재질의 나사(티타늄 나사)와 텅스텐 카바이드 코팅된 나사(Ebony 나사)가 사용되었다. 티타늄 나사에 아무 처리하지 않은 군(TI군)과 티타늄 나사에 나사 고정제를 사용한 군(TI_AS군), Ebony 나사에 아무 처리하지 않은 군(EB군)과 Ebony 나사에 나사 고정제를 사용한 군(EB_AS군)에 대해 실험을 진행하였다. 총 4가지 군에서 각 10개씩의 임플란트 고정체-지대주 복합체가 사용되었다. 디지털 토크 측정 장비를 사용하여 풀림 토크 값을 측정한 뒤 통계 처리하여 각 군별 비교하였다. 정규성 분포를 만족하여 Two-way ANOVA test (α = .05)를 이용하여 통계 분석하였다. 결과: 각 군에 대한 결과를 살펴보면 TI 군은 20.3 ± 1.6 N.cm, TI_AS 군에서 32.4 ± 6.7 N.cm, EB 군은 20.2 ± 1.5 N.cm, EB_AS 군에서 30.4 ± 4.5 N.cm의 풀림 토크 값을 나타냈다. 결론: 혐기성 나사 고정제를 사용한 경우 티타늄 나사와 ebony 나사 모두에서 고정제를 사용하지 않은 경우 보다 풀림 토크 값이 높게 나타났다. 하지만 두 나사 군 간의 차이는 존재하지 않았다.

변형된 Brostrom 수술 후, Anti-gravity treadmill 가속재활운동이 만성발목불안정성 환자의 발목기능 회복에 미치는 영향 (Effect of Accelerated Rehabilitation with Anti-Gravity Treadmill Exercise on Ankle Joint Function After Surgery of Modified Brostrom Operation in Chronic Ankle Instability Patients)

  • 최인혁;이장규
    • 한국산학기술학회논문지
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    • 제20권7호
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    • pp.228-235
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    • 2019
  • 이 연구의 목적은 만성발목불안정성 환자의 변형된 Brostrom 수술 후, 6주간의 Anti-gravity treadmill을 이용하여 조기체중부하를 포함하는 가속재활운동 프로그램이 발목관절의 통증지수와 발목 관절가동범위, 등속성 근기능, 동적 안정성에 어떠한 영향을 미치는지에 대하여 구명하고자 실시되었다. 연구대상자는 만성발목불안정성에 의해 변형된 Brostrom 수술을 받은 환자 12명을 대상으로 하였으며, 6주간의 가속재활운동 프로그램은 매일 60분씩 실시되었고 Anti-gravity treadmill 프로그램 또한 매일 15~30분간 실시되었다. 이 연구의 결과에서, 시각적 사상척도(VAS)를 이용한 주관적 통증지수는 가속재활운동 프로그램 적용 후, 유의하게 감소한 것으로 나타났으며(p<.001) 발목 관절가동범위 또한 가속재활운동 후, 배측 굴곡과 저측 굴곡, 내번, 외번 모두에서 유의하게 증가하였다(p<.05). 등속성 근기능은 가속재활운동 후, 내반력과 외반력 모두 $60^{\circ}/sec$(p<.001, p<.01)와 $180^{\circ}/sec$(p<.001)에서 유의하게 증가하였으며 건측에 대한 환측의 근결손율은 $60^{\circ}/sec$의 내반력(p<.01)과 외반력(p<.001), $180^{\circ}/sec$(p<.01)의 내반력에서 유의하게 감소하였고 외반력에서는 다소 감소하는 경향을 보였지만 통계적으로 유의한 차이는 보이지 않았다. 동적 안정성은 6주간의 가속재활운동 프로그램 적용 후, 유의하게 증가한 것으로 나타났다(p<.001). 이러한 결과는 6주간의 Anti-gravity treadmill을 이용하여 조기체중부하를 포함하는 가속재활운동 프로그램이 변형된 Brostrom 수술을 받은 만성발목불안정성 환자들의 통증과 발목 관절가동범위, 등속성 근기능, 동정 안정성에 긍정적인 효과가 있는 것으로 사료되며 또한 Anti-gravity treadmill을 이용한 조기체중부하의 재활운동 보다 안전하고 빠르게 발목의 안정성을 회복하여 일상생활 및 스포츠 현장으로의 빠른 복귀를 가능하게 할 것으로 사료된다.

비고정식 피스톤 핀의 회전운동에 관한 연구 (Study on the Rotating Motion of a Piston Pin of Full Floating Type)

  • 전상명
    • Tribology and Lubricants
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    • 제23권3호
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    • pp.95-102
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    • 2007
  • In recently designed diesel engines, the running conditions for piston pin bearings have become very severe due to combustion pressure and temperature increase. Moreover, the lead removal from the bush material has strongly reduced the capability of the anti friction material to accept asperity contacts. In this paper, before trying to find the pressure distributions on the oil film of piston pin bearings by the unsteady two dimensional thermohydrodynamic lubrication analysis in order to do the optimum design of the bearings of piston pin, it will be investigated the tendancy of piston pin rotating motion by calculating the friction coefficient at piston pin bearings, the oil film thickness and the frictional torques induced by hydrodynamic shear stress.

퍼지 제어기를 이용한 이동 로봇의 재점착 제어 (Re-adhesion Control for Wheeled Robot Using Fuzzy Logic)

  • 권선구;허욱렬;김학일
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2004년도 하계학술대회 논문집 D
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    • pp.2423-2425
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    • 2004
  • Mobility of an indoor wheeled robot is affected by adhesion force that is related to various floor conditions. When the adhesion force between driving wheels and the floor decreases suddenly, the robot has slip state. First of all, this paper models adhesion characteristics and slip in wheeled robot. Secondly, the paper proposes estimation method of adhesion force coefficient(AFC) according to slip velocity. In order to overcome this slip problem, optimal slip velocity must be decided for stable movement of wheeled robot. The paper proposes an anti-slip control system based on an ordinary disturbance observer, that is, the re-adhesion control is achieved by reducing the driving torque enough to give maximum adhesion force coefficient. fuzzy logic controller(FLC) is petty useful with slip through that compare fuzzy with PI control for the controller performance. These procedure is implemented using a Pioneer 2-DXE parameter.

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지게차 전용 동력전달시스템의 설계 및 개발에 관한 연구 (A Study on the Design and Development of the Power Transmission System for Lift Truck)

  • 장경열;박중순;유우식
    • 산업경영시스템학회지
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    • 제32권1호
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    • pp.34-43
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    • 2009
  • In this thesis, we explain developing processes of the power transmission system for lift truck. Conventional power transmission system had some problems such as spatial constraints or low speed and high torque problem. Because conventional power transmission system was mainly designed for high speed vehicles. In this paper we developed power shift drive axle specialized for $2.0{\sim}3.5$ ton lift truck. Innovative structure of transmission which is built in inside axle, enables to reduce system weight and size by 40% compared to the conventional power transmission system. Also, it is possible to do additional functions such as auto parking system and anti-roll back system.

MTM OIL의 변속성능과 내구성에 대한 연구 (A Study for Shift Qulity and Durability of Manual Transmission Oil)

  • 차상엽;양시원
    • 한국윤활학회:학술대회논문집
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    • 한국윤활학회 2003년도 학술대회지
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    • pp.185-190
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    • 2003
  • Synchronizer ring performance is strictly required in order to extend manual transmission oil drain interval. Zn type additive, which is used as dispersant and anti-wear additive instead of SP additives in manual transmission oil, is applied to improve Synchronizing function and durability. But only Zn type additive is not suitable for high torque transmission because it has not good extreme pressure characteristics. We research on the synchronizer friction and extreme pressure properties in according to change additive types. As a result, it was found that the use of non-active extreme pressure and friction modifier additives has benefit in the improvement of synchronizer friction characteristics and durability.

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중형 헬리콥터 로터 시스템 개념설계 연구 (A Study of the Conceptual Design of Medium Size Utility Helicopter Rotor System)

  • 김준모
    • 한국군사과학기술학회지
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    • 제8권3호
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    • pp.33-41
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    • 2005
  • This paper describes the conceptual design of medium size helicopter rotor system. Based on assumed design requirements, trade-off study for rotor configuration has been conducted in terms of rotor tip speed, disk loading, blade area, solidity, etc for estimated primary mission gross weight. For the main rotor, four-blade and five-blade rotors are studied with the conventional tail rotor. The performance analysis for baseline configuration is conducted using a helicopter performance analysis program. The analysis shows design results satisfy the design requirements.

결합부 유연성에 따른 감쇠거동에 관한 고찰 : 히스테레틱 감쇠 (Estimations of the Hysteretic Damping by Controlled Joint Flexibilities)

  • 윤성호
    • 소음진동
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    • 제9권2호
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    • pp.258-264
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    • 1999
  • The purpose of this paper is to investigate the damping behavior of a flexible joint. The slip at a structrual joint is selected at the tips of two identical cantilever beams adjoining each other. Both the direction of normal force and its magnitude varies due to the global deformation of the structure from mode to mode in the friction model. The friction dependent on vibration displacements resultsin the same functional behavior of the hysteretic material damping. Linearized energy loss factors are obtained as functions of both linear and torsional spring stiffness for their groups of symmetric and anti-symmetric modes, respectively. Experimental measurements as made for comparisons with analytical estimations by controlling the magnitude of fastening torque in the fastener, Hi-Lite. Trends on damping levelsmeasured in a very common vibration test method make an excellent agreement on the estimated damping levels.

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테일팬 성능시험장치의 운용과 진동특성 (The Operation and Vibration Characteristics of Tail-Fan Performance Test System)

  • 송근웅;김준호;강희정;이욱;심정욱
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2004년도 추계학술대회논문집
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    • pp.508-512
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    • 2004
  • This paper described operation and vibration characteristics of 'Tail-Fan' performance test system. KARI(Korea Aerospace Research Institute) developed 'Tail-Fan' system as a kind of helicopter anti-torque system(ATS) and designed ATS performance test-rig for Tail-Fan system performance test. Test-rig consists of driving parts, supporting parts and rotating parts. For Tail-Fan system performance tests, firstly, test-rig operation tests were carried out for verification of design specifications. Secondly, natural frequencies of fan blade and test-rig were measured respectively. Lastly, to find the operation rotating speed for performance tests, vibration tests using accelerometers on tail gear box(TGB) were carried out. Through the fanplot and vibration test results, Tail-Fan performance test conditions to avoid a resonance were found and performance tests were well done safely.

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