• 제목/요약/키워드: 6 Degree Freedom Motion

검색결과 141건 처리시간 0.029초

Rigid block coupled with a 2 d.o.f. system: Numerical and experimental investigation

  • Pagliaro, Stefano;Aloisio, Angelo;Alaggio, Rocco;Di Egidio, Angelo
    • Coupled systems mechanics
    • /
    • 제9권6호
    • /
    • pp.539-562
    • /
    • 2020
  • In this paper the linear elastic coupling between a 2 degree of freedom shear-type frame system and a rigid block is analytically and experimentally investigated. As demonstrated by some of the authors in previous papers, it is possible to choose a coupling system able to guarantee advantages, whatever the mechanical characteristics of the frame. The main purpose of the investigation is to validate the analytical model. The nonlinear equations of motion of the coupled system are obtained by a Lagrangian approach and successively numerically integrated under harmonic and seismic excitation. The results, in terms of gain graphs, maps and spectra, represent the ratio between the maximum displacements or drifts of the coupled and uncoupled systems as a function of the system's parameters. Numerical investigations show the effectiveness of the nonlinear coupling for a large set of parameters. Thus experimental tests are carried out to verify the analytical results. An electro-dynamic long-stroke shaker sinusoidally and seismically forces a shear-type 2 d.o.f frame coupled with a rigid aluminium block. The experimental investigations confirm the effectiveness of the coupling as predicted by the analytical model.

정상 해석 기반의 데이터베이스를 이용한 TST 비행체의 분리 궤도 예측 (PREDICTION OF SEPARATION TRAJECTORY FOR TSTO LAUNCH VEHICLE USING DATABASE BASED ON STEADY STATE ANALYSIS)

  • 조재현;안상준;권오준
    • 한국전산유체공학회지
    • /
    • 제19권2호
    • /
    • pp.86-92
    • /
    • 2014
  • In this paper, prediction of separation trajectory for Two-stage-To-Orbit space launch vehicle has been numerically simulated by using an aerodynamic database based on steady state analysis. Aerodynamic database were obtained for matrix of longitudinal and vertical positions. The steady flow simulations around the launch vehicle have been made by using a 3-D RANS flow solver based on unstructured meshes. For this purpose, a vertex-centered finite-volume method was adopted to discretize inviscid and viscous fluxes. Roe's finite difference splitting was utilized to discretize the inviscid fluxes, and the viscous fluxes were computed based on central differencing. To validate this flow solver, calculations were made for the wind-tunnel experiment model of the LGBB TSTO vehicle configuration on steady state conditions. Aerodynamic database was constructed by using flow simulations based on test matrix from the wind-tunnel experiment. ANN(Artificial Neural Network) was applied to construct interpolation function among aerodynamic variables. Separation trajectory for TSTO launch vehicle was predicted from 6-DOF equation of motion based on the interpolated function. The result of present separation trajectory calculation was compared with the trajectory using experimental database. The predicted results for the separation trajectory shows fair agreement with reference[4] solution.

표적 수정이 가능한 사용자 개입 통합 관리 모의 시스템 개발 (Development of the integrated management simulation system for the target correction)

  • 박우성;오태원;박태현;이용원;김기범;권기정
    • 한국항공우주학회지
    • /
    • 제45권7호
    • /
    • pp.600-609
    • /
    • 2017
  • 탐색기의 센서 영상을 이용하여 최종 표적에 대한 선정을 수동 또는 자동으로 할 수 있는 표적 관리 모의 시스템을 개발하였다. 모의 시스템은 비행체 시스템과 지상 시스템으로 구성하였다. 비행체 시스템은 비행체의 운동역학과 센서 영상을 모의하고 지상 시스템은 표적 템플릿 모의와 지상 제어기를 모의를 수행한다. 비행체의 운동역학은 의사 6자유도를 기반으로 비례항법유도기법을 사용한다. 탐색기의 센서 영상은 알려진 적외선 영상 렌더링 기법을 이용하여 직접 개발하였으며 상용 프로그램과 비교하여 검증하였다. 지상제어기는 사용자 편의를 위해 임무에 관련된 정보를 가능한 많이 전시할 수 있는 사용자 인터페이스로 구성하였다. 최종적으로 표적 격추 임무 모의를 통해 요구하는 성능에 만족함을 확인하였다.

기동형 경계로봇 안정화 시스템의 실험적 검증 (Experimental Verification of Effectiveness of Stabilization Control System for Mobile Surveillance Robot)

  • 김성수;이동염;권정주;박성호
    • 대한기계학회논문집A
    • /
    • 제35권4호
    • /
    • pp.359-365
    • /
    • 2011
  • 기동형 경계 로봇은 공항이나 항구 등의 공공 지역을 보호하기 위한 기동형 차량 시스템에 고정되어 있는 경계 로봇을 말한다. 이러한 기동형 경계 로봇은 사격 시스템, 카메라 시스템, 임베디드 시스템 그리고 AHRS 센서로 구성되어 있다. 또한 고각과 방위각을 위한 2 축 제어가 가능하도록 설계되었다. 안정화된 영상과 사격을 위해 이 시스템은 차량의 모션으로부터 발생하는 외란에 대한 보상을 통해 안정화가 되어야 한다. 본 논문에서는 ADAMS 와 Matlab/Simulink 를 이용해서 기동형 경계로봇의 가상 모델을 생성하고 제안한 안정화 알고리즘을 시뮬레이션을 통해 검증하였다. 또한 가상모델에 상응하는 모형의 기동형 경계 로봇과 6 축 모션 시뮬레이터를 이용하여 안정화 알고리즘을 실험적으로 검증하였다.

Development of a Biped Walking Robot Actuated by a Closed-Chain Mechanism

  • Choi, Hyeung-Sik;Oh, Jung-Min;Baek, Chang-Yul;Chung, Kyung-Sik
    • 제어로봇시스템학회:학술대회논문집
    • /
    • 제어로봇시스템학회 2003년도 ICCAS
    • /
    • pp.209-214
    • /
    • 2003
  • We developed a new type of human-sized BWR (biped walking robot), named KUBIR1 which is driven by the closed-chain type of actuator. A new type of the closed-chain actuator for the robot is developed, which is composed of the four-bar-link mechanism driven by the ball screw which has high strength and high gear ratio. Each leg of the robot is composed of 6 D.O.F joints. For front walking, three pitch joints and one roll joint at the ankle. In addition to this, one yaw joint for direction change, and another roll joint for balancing the body are attached. Also, the robot has two D.O.F joints of each hand and three D.O.F. for eye motion. There are three actuating motors for stereo cameras for eyes. In all, a 18 degree-of-freedom robot was developed. KUBIR1 was designed to walk autonomously by adapting small 90W DC motors as the robot actuators and batteries and controllers are on-boarded. The whole weight for Kubir1 is over 90Kg, and height is 167Cm. In the paper, the performance test of KUBIR1 will be shown.

  • PDF

해상감시용 NV 시스템의 추종 및 안정화 (Tracking and Stabilization of a NV System for Marine Surveillance)

  • 황승욱;김정근;송세훈;진강규
    • 한국항해항만학회지
    • /
    • 제35권3호
    • /
    • pp.227-233
    • /
    • 2011
  • 본 연구는 선박용 Night Vision 시스템을 개발하기 위한 선행연구로 2축 지그와 이를 구동할 수 있는 PCU 보드를 제작하고, 추종 및 안정화 제어루틴을 얻는 문제를 다룬다. 개발한 지그와 PCU 보드를 6DOF 모션 시뮬레이터와 결합하여 실험환경을 구축하고 RCGA를 이용하여 지그 모델의 파라미터를 얻고, 추정된 모델과 RCGA를 이용하여 2DOF PID 제어기를 동조한다. 실험과 시뮬레이션을 통해 제안하는 2자유도 PID 제어기의 유효성을 검토한다.

지중발파에 의한 건물의 진동 거동에 관한 연구 (A Study on the Vibration Behavior of Building Structures due to Undergroud Blasting)

  • 조병윤;문형구
    • 터널과지하공간
    • /
    • 제6권2호
    • /
    • pp.157-165
    • /
    • 1996
  • In order to analyze the effects of ground vibration caused by underground blasting having an effect on structure, the particle velocity and acceleration are calculated by using DYNPAK program. The DYNPAK program analyzes nonlinear transient dynamic problem and adopts the very popular and easily implemented, explicit, central difference scheme. In this program, the material behavior is assumed to be elasto-viscoplastic. Using the particle acceleration history, modal analysis method is applied to the forced vibration response of multiple-degree-of-freedom(MDOF) systems using unclupled equations of motion expressed in terms of the system's natural circular frequencies and modal damping factors. AS a means of evaluating the vibration behavior of building structure subjected to underground blasting, the time response of the displacements relative to the ground of five-story building is determined. It is concluded that the amount of explosives consumed per round, the location of structure, the properties of rock medium, the stiffness fo structure, etc. act on the important factors influencing on the safety of building and that the response of a structure subjected to a forced excitation can usually be obtained with reasonable accuracy by the modal analysis of only a few mode of the lower frequencies of the system.

  • PDF

Numerical simulation of 3-D probabilistic trajectory of plate-type wind-borne debris

  • Huang, Peng;Wang, Feng;Fu, Anmin;Gu, Ming
    • Wind and Structures
    • /
    • 제22권1호
    • /
    • pp.17-41
    • /
    • 2016
  • To address the uncertainty of the flight trajectories caused by the turbulence and gustiness of the wind field over the roof and in the wake of a building, a 3-D probabilistic trajectory model of flat-type wind-borne debris is developed in this study. The core of this methodology is a 6 degree-of-freedom deterministic model, derived from the governing equations of motion of the debris, and a Monte Carlo simulation engine used to account for the uncertainty resulting from vertical and lateral gust wind velocity components. The influence of several parameters, including initial wind speed, time step, gust sampling frequency, number of Monte Carlo simulations, and the extreme gust factor, on the accuracy of the proposed model is examined. For the purpose of validation and calibration, the simulated results from the 3-D probabilistic trajectory model are compared against the available wind tunnel test data. Results show that the maximum relative error between the simulated and wind tunnel test results of the average longitudinal position is about 20%, implying that the probabilistic model provides a reliable and effective means to predict the 3-D flight of the plate-type wind-borne debris.

공조용 압축기 배관계의 과도진동 예측 및 저감설계 (Prediction and Reduction of Transient Vibration of Piping System for a Rotary Compressor)

  • 유상모;정의봉;한형석
    • 한국소음진동공학회논문집
    • /
    • 제21권8호
    • /
    • pp.733-740
    • /
    • 2011
  • This paper deals with the process to identify the transient exciting force generated from a rotary compressor. The compressor was assumed to be a rigid body. The equation of motion of a rigid compressor supported by three mounts was derived with 6 degree-of-freedom. The exciting forces at the center of mass of the compressor were estimated from the acceleration data measured at compressor shell. Compressor-pipe system was modeled numerically. The accelerations of compressor and pipe were predicted numerically by using the estimated exciting force. A new shape of pipe model was proposed to reduce the vibration. In the prediction by the method in this paper, the maximum acceleration of the pipe could be reduced by 53.7 % at the steady-state and by 12 % at the transient process. In the real experiments, the maximum acceleration of the pipe was reduced by 54.2 % at steady-state and 14.7 % at the transient process. It was verified that the numerical results showed good agreement with experimental results.

Macpherson형 현가장치의 새로운 모델링과 최적극배치 제어 (A New Model and Optimal Pole-Placement Control for the Suspension System of Macpherson Type)

  • 홍금식;전동섭;김철민;유완석
    • 제어로봇시스템학회논문지
    • /
    • 제4권6호
    • /
    • pp.713-721
    • /
    • 1998
  • In this paper a new modeling and an optimal pole-placement control for the suspension system of Macpherson type are investigated. The rotational motion of the unsprung mass is emphasized in the new modeling. The two generalized coordinates selected in the new model are the vortical displacement of sprung mass and the angular displacement of control arm. Both variables are measured from their static equilibrium points. It is shown that the conventional model is a special case of the new model since the transfer function of the new model coincides with that of the conventional one if the lower support point of the shock absorber is located at the mass center of the unsprung mass. It is also shown that the resonance frequencies of the new model agree better with experimental results. Therefore, the new model is more general in the sense that it Provides an extra degree of freedom in determining the plant model for control system design. An optimal pole-placement control which combines LQ control and pole-placement technique is applied to the new model. Simulations are provided.

  • PDF