• Title/Summary/Keyword: 마찰력 식별

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Friction Identification without Information of Acceleration (가속도 정보를 사용하지 않는 마찰계수 식별방법)

  • Kim, Sung-Yeol;Ha, In-Joong
    • The Transactions of the Korean Institute of Electrical Engineers D
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    • v.51 no.3
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    • pp.89-95
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    • 2002
  • This paper describes a new identification method for friction in motion control systems, in which the friction model is not necessarily linear in parameters. The proposed method works well with any measurement data of velocity and input control force, as long as the initial and final velocities are identical. Most importantly, the proposed method does not require the information of acceleration for its implementation, in contrast with the previously known methods. This is due to the orthogonality property between acceleration and a function of velocity. In particular, if the parametric model is linear in parameters, its friction parameters can be identified in closed form without resorting to numerical search methods. To illuminate further the generality and practicality of the proposed friction identification method, we show good performance of the proposed method through some simulation results.

Performance Enhancement of Motion Control Systems Through Friction Identification and Compensation (마찰력 식별과 보상을 통한 운동제어 시스템의 성능 개선)

  • Lee, Ho Seong;Jung, Sowon;Ryu, Seonghyun
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.19 no.6
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    • pp.1-8
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    • 2020
  • This paper proposes a method for measuring friction forces and creating a friction model for a rotary motion control system as well as an autonomous vehicle testbed. The friction forces versus the velocity were measured, and the viscous friction, Coulomb friction, and stiction were identified. With a nominal PID (proportional-integral-derivative) controller, we observed the adverse effects due to friction, such as excessive steady-state errors, oscillations, and limit-cycles. By adding an adequate friction model as part of the augmented nonlinear dynamics of a plant, we were able to conduct a simulation study of a motion control system that well matched experimental results. We have observed that the implementation of a model-based friction compensator improves the overall performance of both motion control systems, i.e., the rotary motion control system and the Altino testbed for autonomous vehicle development. By utilizing a better simulation tool with an embedded friction model, we expect that the overall development time and cost can be reduced.

A Comparative Study on the Characteristics of Friction with/without shoes by Analyzing Bio-signals during walking (보행 시 생체신호분석을 통한 신발 착용 유무에 따른 마찰 특성 비교)

  • Oh, Seong-geun;Kim, Jin-Hyun
    • Journal of Convergence for Information Technology
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    • v.8 no.6
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    • pp.59-66
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    • 2018
  • The utilized coefficient of friction (UCOF) as a ratio of the shear force to the normal force on the ground during walking is used to identify the point at which slip is likely to occur. Shoe walking will change the utilized coefficient of friction by shoe design such as sole thickness and hardness, heel shape, and outsole pattern. In this study, subjects are 21 adults (10 female, 11 male, age: $25.2{\pm}2.3yrs$, height: $165.6{\pm}7.2cm$), analysis variables were walking speed, GRF, when the UCOF is maximal, and Tangent of CoP-CoM angle, and correlation analysis with the utilized friction coefficient (UCOF). As a result, First, for the shod walking the time point which UCOF is maximum about heel strike was faster and the magnitude was larger than for barefoot walking. Second, the correlation between the tangent of CoP-CoM and UCOF of right foot was higher at the left heel striking point (UCOF2_h) which occurred in the post propulsion phase than at the right heel striking point (UCOF1_h). This suggests that the right foot UCOF is related to the braking phase of left foot( which is the propulsion phase of right foot) rather than the braking phase of right foot.

Real-time Road Surface Recognition and Black Ice Prevention System for Asphalt Concrete Pavements using Image Analysis (실시간 영상이미지 분석을 통한 아스팔트 콘크리트 포장의 노면 상태 인식 및 블랙아이스 예방시스템)

  • Hoe-Pyeong Jeong;Homin Song;Young-Cheol Choi
    • Journal of the Korea institute for structural maintenance and inspection
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    • v.28 no.1
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    • pp.82-89
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    • 2024
  • Black ice is very difficult to recognize and reduces the friction of the road surface, causing automobile accidents. Since black ice is difficult to detect, there is a need for a system that identifies black ice in real time and warns the driver. Various studies have been conducted to prevent black ice on road surfaces, but there is a lack of research on systems that identify black ice in real time and warn drivers. In this paper, an real-time image-based analysis system was developed to identify the condition of asphalt road surface, which is widely used in Korea. For this purpose, a dataset was built for each asphalt road surface image, and then the road surface condition was identified as dry, wet, black ice, and snow using deep learning. In addition, temperature and humidity data measured on the actual road surface were used to finalize the road surface condition. When the road surface was determined to be black ice, the salt spray equipment installed on the road was automatically activated. The surface condition recognition system for the asphalt concrete pavement and black ice automatic prevention system developed in this study are expected to ensure safe driving and reduce the incidence of traffic accidents.

Evaluation of CPT-based Pile Load Capacity Factors with Cylindrical and Taper Pile (원통형 및 테이퍼말뚝의 하중-침하특성 및 CPT지지력상관계수)

  • Lee, Jun-Hwan;Paik, Kyu-Ho;Kim, Dae-Hong;Kim, Min-Kee;Hwang, Sung-Wuk
    • Journal of the Korean Geotechnical Society
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    • v.23 no.4
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    • pp.59-68
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    • 2007
  • In this study, evaluation of load capacity and CPT-load capacity parameters were performed using calibration chamber tests for different types of piles including straight-side and tapered piles. Various soil conditions were considered in the investigation, aiming at establishing design procedure for foundation of electronic transmission tower structures. Test results show that no significant difference of total load capacity from straight-side and tapered piles, while individual components of base and shaft load capacities were quite different. Based on the test results, values of CPT-load capacity correlation parameters for different pile types were analyzed for the evaluation of both base and shaft load capacities.

Geometrical Analysis on Parts of Load Limit Valve for Static Structural Test of Aerospace Flight Vehicles (항공우주 비행체 정적구조시험용 하중제한밸브 부품 형상 분석)

  • Shim, Jae-Yeul
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.9
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    • pp.607-616
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    • 2019
  • Free body diagram analysis is done for key parts of pilot stage of LLV (Load Limit Valve) which is used to protect overload for static structural test of aerospace flight vehicle. It is shown through the analysis that diameter ratio($D_2)^{ten}/D_2)^{comp}$) of two poppets in a pilot stage must be equal to piston area ratio($A_{comp}/A_{ten}$) of a hydraulic actuator for making a poppet open consistently at constant force applied by an actuator. The result of the analysis is verified by measuring geometries of the poppets in the four different LLVs which are corresponding to four actuators with different capacity and have been used after being imported in this laboratory. Results of "Adjuster resolution tests" with two different pilot stages show the max. deviation of Fi(actuator force in instant of opening poppet) from average Fi obtained for each turn of adjuster is 0.3KN and max. deviation of the Fi normalized by average Fi of each turn of adjuster is 3.7%. From the results, it is verified that the two pilot stages with same poppet diameter ratio make a poppet consistently open at Fis within ${\pm}3.7%$ deviation from the average Fi. The deviation is shown to be caused from frictional force of O-ring in the poppet. Additionally, design factors for poppet spring and adjuster, which are also key parts of the pilot stage, are distinguished and procedure for deciding the factors are also shown in this study.