• Title/Summary/Keyword: Adams

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Effectiveness of a Vehicle Restraint System in Frontal Crash (정면 충돌시 차량 구속 시스템의 효과)

  • Lee, Dong-Jae;Oh, Kwang-Seok;Son, Kwon
    • 제어로봇시스템학회:학술대회논문집
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    • 2000.10a
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    • pp.314-314
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    • 2000
  • This study deals with the analysis of the effectiveness of a safer belt in frontal crash. ATB, Articulated Total Body, program is used as a dynamics solver of the occupant model. ATB is a public code, however, the program is somewhat cumbersome to use due to lack of sufficient user interface. A preprocessor and a postprocessor are, therefore, developed for a user friendly graphic interface in Windows environment. Dialog boxes are used for an interface with GEBOD, Generator of Body Data, for human anthropometry and with ADAMS for vehicle dynamics. It is found through three test simulations that simulated results are in good agreement with those obtained by ATB. The effect of the initial slack of safety belt is investigated for frontal crash using the developed program.

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Mobility Stabilization of a $6\times6$ Robot Vehicle by Suspension Kinematics Reconfiguration (현가장치 기구 재구성에 의한 $6\times6$ 로봇차량의 기동성 안정화)

  • Baek, W.K.;Lee, J.W.
    • Journal of Power System Engineering
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    • v.14 no.3
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    • pp.39-45
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    • 2010
  • The dynamic stability of a robot vehicle can be enhanced by the Force-Angle Stability Margin concept that considers a variety of dynamic effects. To evaluate the robot vehicle stability, a SPI(stability performance index), which is a function of the suspension arm angles, was used. If the SPI has a minimum value, the robot vehicle has maximum stability. The FASM and SPI concepts were incorporated in the mobility simulation by using ADAMS and MATLAB/Simulink. The simulation results using these concepts showed significant improvements of the vehicle stability on rough terrains.

A Study on the Effect of a Stabilization Error of the Line-Of-Sight Stabilization System according to the Isolation Properties (방진성능에 따른 시선 안정화 장치의 안정화오차 영향성 검토)

  • Park, Jae-Hoon;Park, Jong-Chul
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2011.10a
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    • pp.186-190
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    • 2011
  • The Line-Of-Sight stabilization system is designed to minimize the error of Line-Of-Sight under the disturbing circumstances. In order to control this system more accurately and reduce the level of the disturbance, adding an isolator is mostly considered. However, it is difficult to predict the exact the behavior of the isolator and the effect of a stabilization Error. Therefore, the simulation model of the control system using co-simulation with Adams and matlab simulink is presented and the effects of the isolation properties are reviewed.

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Improvement of Fatigue-Proof Characteristics of Link Members Under Impact Loadings by a Spring-Actuated Mechanism (스프링구동 메커니즘의 충격 하중을 받는 링크부재의 내피로 특성 향상)

  • 안길영;박상후;이부윤;김원진;오일성
    • Journal of the Korean Society for Precision Engineering
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    • v.20 no.4
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    • pp.158-164
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    • 2003
  • The air circuit breaker (ACB) with the spring-actuated mechanism was studied to improve the fatigue-proof characteristics of its link. The low-cycle fatigue fracture phenomenon occurred on the critical link, called h-link, of ACB from the repeated rapid closing and opening operations. To analyze the cause of failure, dynamic FE-analysis on the b-link part of ACB was performed considering tile velocity and acceleration of the links per time as boundary conditions, which were obtained by using ADAMS. Also, the S-N curve obtained by experiments was used to investigate requirement on the fatigue-proof characteristics. Then, to reduce the maximum tensile stress on the h-link, three types of h-link were examined and one of them was selected.

The Effect on the Launching Stability due to the Initial Missile Detent Force (발사시 초기 구속력이 유도탄 발사안정에 미치는 영향)

  • 심우전;임범수
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1996.11a
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    • pp.1017-1022
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    • 1996
  • This paper presents results of dynamic analysis of the missile initial motion arising from the missile detent force. Using ADAMS (Automatic Dynamic Analysis of Mechanical System) software, a non-linear 46-DOF (Degree of Freedom) model is developed for the launcher system including missile and launch tube contact problem. From the dynamic analysis, it is found that initial angular velocity of the missile increases when the missile detent force increases (more than 18 g) and also rocket exhaust plume is taken into account. To achieve the missile launching s ability, it needs to reduce the missile initial detent force and exhaust plume area of the launcher. Results of the dynamic analysis on the system natural frequency agree well with those obtained from experimental modal tests. The overall results suggest that the proposed method is a useful tool for prediction of initial missile stability as well as d :sign of the missile launcher system.

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Optimization of the Spring Design Parameters of a Circuit Breaker to Satisfy the Specified Dynamic Characteristics

  • Gil Young;Kwang Young
    • International Journal of Precision Engineering and Manufacturing
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    • v.5 no.4
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    • pp.43-49
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    • 2004
  • A spring-actuated linkage system is used to satisfy the desired opening and closing characteristics of the electric contacts of a vacuum circuit breaker. If the type of a circuit breaker and the structure of the linkage system are predetermined, then design parameters such as stiffness, free length and attachment points of the spring become the important issues. In this paper, based on the energy conservation, the total system energy is constant throughout the operating range of the mechanism; a systematic procedure to optimize the spring design parameters is developed and applied to a simplified mechanism of a circuit breaker. The developed procedure is converted to the environment of the multi-body dynamics program, ADAMS for an in-depth consideration of the complex dynamics of a circuit breaker mechanism.

Vibration Analysis of Driveline with Propeller Shaft Supported by Center Bearing when the Vehicle Starts (추진축이 센터베어링으로 지지된 차량 구동계의 출발시 진동해석)

  • 이창노;김효준
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2002.05a
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    • pp.1043-1048
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    • 2002
  • This paper considers the vibration problem of vehicle driveline which consists of two propeller shafts and the center bearing. The excessive vibration occurs at the center bearing when the vehicle starts to run. Using the kinematic constraints at the universal joint between two propeller shafts, we develop an one d.o.f model which describes the radial motion of the center bearing. We find out the vibration occurs at the specific vehicle speed corresponding to the natural frequency of the model. Comparing the simulation results with test results we also show that the vibration at low vehicle speed is caused primarily by the joint angle and secondarily by the mis-aligned yoke flange rather than by the unbalance.

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A Study on Human Body Impact Characteristics of the Human-rifle System on Shooting (인체-화기시스템의 인체충격특성에 관한 연구)

  • Lee Young-Shin;Lee Jang-Won;Choi Young-Jin;Chae Je-Wook;Choi Eui-Jung;Kim In-Woo
    • Journal of the Korean Society for Precision Engineering
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    • v.23 no.7 s.184
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    • pp.159-167
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    • 2006
  • The impact time history of human body with K2 rifle on stand shooting posture is analyzed and compared with experimental results. Analysis model is Korean 50% tile of twenties and height, weight is 174 cm, 62 kgf respectively. The muscle and bone human model of Korean man's twenties 50% tile is applied. ADAMS program is used for kinematic analysis and human model is developed by Life Mod program. The effect of the ground support condition, grip position and human weight factor are studied. Maximum impact force of shoulder is 784 N. The horizontal displacement of K2 rifle muzzle is 2.9 cm.

The Determination of Control Limit and Testing Interval in the On-Line Quality Control of Taguchi Method (Taguchi Method의 On-Line Quality control에 있어서 관리한계 및 검사간격 결정에 대한 연구)

  • Kim, Uk-Il;Gang, Chang-Uk
    • Journal of Korean Society for Quality Management
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    • v.20 no.2
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    • pp.11-20
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    • 1992
  • We discuss the feed back control of the on-line QC in the Taguchi method. Taguchi(1982) used the assumptions that the quality characteristics follow an uniform distribution and the Brownian motion to draw the loss function and proposed ${\Delta}/3$ or ${\Delta}$ for the initial control limit. Adams and Woodall(1989) also proposed a different procedure but using the same loss function. We propose, in this paper the new loss function under the assumption of mainly Brownian motion and compare the results with the results of the above.

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Introduction to the NREL Design Codes for System Performance Test of Wind Turbines - Part II : Simulators (풍력터빈 시스템 성능평가를 위한 NREL 프로그램군에 관한 소개 - 해석기를 중심으로)

  • Bang, Je-Sung;Rim, Chae Whan;Chung, Tae Young
    • 한국신재생에너지학회:학술대회논문집
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    • 2011.11a
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    • pp.42.1-42.1
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    • 2011
  • NREL NWTC Deside codes are analyzed and introduced to develop the system performance simulation program for wind turbine generator systems. In this paper, The FAST performing multi-body and flexible body dynamics, control and the AeroDyn calculating aerodynamic forces with airfoil data and wind data are explained. Furthermore, initialization and process for transfer of aerodynamic force between AeroDyn and FAST at each time step are also introduced.

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