• Title/Summary/Keyword: 엘리베이터 동특성

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A study on the Development of the Device for Portable Safety Diagnosis and Dynamic Characteristics Analysis of Elevator using Fuzzy Algorithm (Fuzzy 알고리즘을 이용한 엘리베이터 포터블 안전진단 및 동특성 분석장치 개발)

  • 김태형;김훈모
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2000.11a
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    • pp.123-126
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    • 2000
  • An elevator system which is a essential equipment for a vertical movement of object, as a property of building, have been drove by various expenditure and purpose. Since developing electrical control technology, control systems are highly developed. An elevator equipment is expended to wide, but a data accuracy acquisition technique and safety predict technique for securing system safety is still basic level. So, objective verification for elevator confidence condition is required absolutely accuracy measurement technique. Therefore, this study is accomplished in order to conquer a method of depending on sense of a manager with a simple numeric measurement data, and construct a logical, analytical foresight system for more efficient elevator management system.

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A study on the Development of the Portable Device for Safety Diagnosis and Dynamic Characteristics Analysis of Elevator using Fuzzy Algorithm (Fuzzy 알고리즘을 이용한 엘리베이터 안전진단 및 동특성 분석 포터블 장비 개발)

  • 김태형;김훈모
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2001.04a
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    • pp.199-202
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    • 2001
  • An elevator system, which is essential equipment for vertical movement of an object, as a property of building, has been driven by various expenditures and purposes. Since developing electrical control technology, control system are highly developed. The elevator system has expanded widely, but a data accuracy acquisition technique and safety predict technique for securing system safety is still at a basic level. So, objective verification for elevator confidence condition requires an absolute accuracy measurement technique. Therefore, this study is executed in order to acquire a method of depending on sense of a manager with simple numeric measurement data, and to construct a logical, analytical foresight system for more efficient elevator management system. As an artificial intelligence for diagnosis, the fuzzy inference algorithm is used for foreseeing the system in this thesis, because the fuzzy algorithm is the most useful method for resolving subjective ideas and a vague judgment of humans. The fuzzy inference algorithm is developed for each sensor signal(i.e. vibration, velocity, current).

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Dynamic Characteristic Evaluation of the Bucket Elevator Chain Pin and Plate (버킷 엘리베이터 체인의 동특성 평가)

  • Kim, Chang Uk;Lee, Dong Woo;Park, Seung Bin;Song, Jung Il
    • Journal of the Korean Society for Precision Engineering
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    • v.34 no.3
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    • pp.211-215
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    • 2017
  • This research analyzes bucket elevator roller chain pins by finite element (FE) analysis and static structural analysis for a lightweight pin design. The stress distribution of light weight roller chain pins under static load is analyzed for safety factors and damping effect. The results show that the stress distribution is higher on the plate than on the bush pin. In order to compare experimental and FE analysis results, a light weight design approach was used to produce a prototype base pin. Because the inner diameter of the pin was different, the impact damping effect was most appropriate when the inner diameter was 34.05 mm, and it is used as basic research data on the impact of the roller chain and sprocket.

Pitch-axis Maneuver of UAVs by Adaptive Control Approach (무인항공기의 적응제어 법칙을 이용한 피치 기동 연구)

  • Bang, Hyo-Choong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.12
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    • pp.1170-1176
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    • 2010
  • This study addresses adaptive control of UAVs(Unmanned Aerial Vehicles) pitch-axis maneuver. The MRAC(Model Referenced Adaptive Control) approach is employed to accommodate uncertainties which are introduced by feedback linearization of pitch attitude control by elevator input. The model uncertainty is handled by adaptation laws which update model parameters while the UAV is under control by the feedback control law. Steady-state pitch attitude achieved by the stabilizing control law is derived to provide insight on the closed-loop behavior of the controlled system. The proposed idea is free of linearization, gain-scheduling procedures, so that one can design high maneuverability of UAVs for pitching motion in the presence of significant model uncertainty.