• 한국공작기계학회논문집
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• 제13권3호
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• pp.68-75
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• 2004

Recently, need of the parallel manipulator requiring superior precision is increasing for medical application and precision manufacturing. In this study, we convert a given complex translation trajectory of the moving platform into a set of segments and hence a complex motion of the moving platform can be tractable and easily controled in a very limited workspace. In addition force exerted. to each link is minimized so that the minimized force can be transmitted to the end effector of the moving platform. An user friendly program is developed to design Gough-type 6DOF parallel manupulator based on the proposed method.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회A
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• pp.745-750
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• 2008

Uncertain dynamic parameters and joint flexibility have been problem to control robot manipulator precisely. Hence, even if the controller tracks the desired trajectory well with the feedback of the motor encoders, it is hard to achieve the desired behavior at the end-effector. In this paper, robot trajectory is taught by a general heuristic iterative learning control (ILC) algorithm in order to reduce tracking error of the tool center point (TCP) and the results of tracking with 6 DOF industrial robot manipulator are presented. The performance is verified based on ISO 9283.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 추계학술대회논문집
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• pp.306-309
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• 2005

This parer describes the tracking control simulation of 6-DOF shaking table with a bell crank structure, which converts the direction of reciprocating movements. For the Joint coordinate-based control which uses lengths of each actuator, the trajectory conversion process inverse kinematics is performed. Applying the Newton-Euler approach, the dynamic equation of the shaking table is derived. To cope with nonlinear problems, time-delay control(TDC) is considered, which has been noted for its exceptional robustness to parameter uncertainties and disturbance, in addition to steady-state accuracy and computational efficiency. If the nominal model is equal to the real system, joint coordinate-based control can be very efficient. However, manufacturing tolerances installation errors and link offsets contaminate the nominal values of the kinematic parameters used in the kinematic model of the shaking table. To compensate differences between the nominal model and the real system. the joint coordinate-based control using acceleration feedback in the Cartesian coordinate space is proposed.

• 한국시뮬레이션학회논문지
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• 제33권2호
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• pp.13-25
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• 2024

무기체계의 연구개발에 앞서 예상되는 효과를 분석하는 것은 개발의 목표와 방향 설정을 위해 중요한 요소이다. 하지만 개발 과정에서 완성 단계를 가정하고 효과를 분석하는 것은 쉬운 일이 아니며, 특히 기존에는 없던 새로운 개념의 무기체계의 경우 이러한 어려움은 더욱 크다. 본 연구에서는 기준 시점에서 완료된 설계내용과 개발된 파편탄두의 기폭실험결과를 반영하여 개인용 소형 유도무기에 대한 효과분석을 하였다. 전투효과 분석을 위해 모의도구에서 요구되는 탄의 정확도 도출을 위하여 설계된 탄 형상이 반영된 6-DOF 시뮬레이터를 활용한 몬테카를로 시뮬레이션을 통해 정확도를 산출하였으며, 대인 효과도 도출을 위하여 파편탄두 기폭실험을 수행 후 대인효과도를 도출하였다. 이후 전투모의 도구인 OneSAF(One Semi-Automated Forces)에 도출된 결과를 반영하기 위한 모의논리 개발 방법론을 제시하였다. 제안된 방법론의 적용성을 확인하여 위하여, 적용 무기체계의 테스트 시나리오들로 모의실험을 진행하여 반영한 모의논리가 의도한 대로 작동함을 확인하였다.

• 제어로봇시스템학회논문지
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• 제10권9호
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• pp.833-839
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• 2004

This paper proposes a method that minimizes the consumed energy by searching the optimal locations of the mass centers of links composing of a biped robot using Real-Coded Genetic Algorithm. Generally, in order to utilize optimization algorithms, the system model and design variables must be defined. Firstly, the proposed model is a 6-DOF biped robot composed of seven links, since many of the essential characteristics of the human walking motion can be captured with a seven-link planar biped walking in the saggital plane. Next, Fourth order polynomials are used for basis functions to approximate the walking gait. The coefficients of the fourth order polynomials are defined as design variables. In order to use the method generating the optimal gait trajectory by searching the locations of mass centers of links, three variables are added to the total number of design variables. Real-Coded GA is used for optimization algorithm by reason of many advantages. Simulations and the comparison of three methods to generate gait trajectories including the GCIPM were performed. They show that the proposed method can decrease the consumed energy remarkably and be applied during the design phase of a robot actually.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.690-699
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• 2008

In this paper a conventional approach for design and analysis of subsonic air vehicle is used. First of all subsonic aerodynamic coefficients are calculated using Computational Fluid Dynamics(CFD) tools and then wind-tunnel model was developed that integrates vehicle components including control surfaces and initial data is validated as well as refined to enhance aerodynamic efficiency of control surfaces. Experimental data and limited computational fluid dynamics solutions were obtained over a Mach number range of 0.5 to 0.8. The experimental data show the component build-up effects and the aerodynamic characteristics of the fully integrated configurations, including control surface effectiveness. The aerodynamic performance of the fully integrated configurations is comparable to previously tested subsonic vehicle models. Mathematical model of the dynamic equations in 6-Degree of Freedom(DOF) is then simulated using MATLAB/SIMULINK to simulate trajectory of vehicle. Effect of altitude on range, Mach no and stability is also shown. The approach presented here is suitable enough for preliminary conceptual design. The trajectory evaluation method devised accurately predicted the performance for the air vehicle studied. Formulas for the aerodynamic coefficients for this model are constructed to include the effects of several different aspects contributing to the aerodynamic performance of the vehicle. Characteristic parameter values of the model are compared with those found in a different set of similar air vehicle simulations. We execute a set of example problems which solve the dynamic equations to find the aircraft trajectory given specified control inputs.

• 플랜트 저널
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• 제17권3호
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• pp.42-46
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• 2021

드릴 스트링의 진동 문제는 수년간 드릴링 성능 저하의 주요 원인 중 하나로 인식되어 왔으며, 굴착 작업 시 발생하는 과도한 진동은 드릴링의 효율성, 파이프 피로, 비트의 수명 단축으로 인하여 고장을 초래할 수 있다. 이러한 진동의 원인은 드릴 스트링이 굴착 작업 중 궤적에 따라 파이프의 굽힘과 wellbore와의 접촉으로 인해 마찰이 발생하고 이러한 진동은 일반적으로 축 방향, 굴곡 및 비틀림 변형을 일으킨다. 본 연구에서는 Khulief와 Al-Naser가 제시한 모델을 바탕으로 드릴 스트링에 6자유도(DOF)의 구성요소를 갖는 모델을 적용하여 curved beam의 수치해석 값과 Analytical값을 비교하여 검증하고 드릴 스트링에 hookload와 WOB 경계조건을 주어 각 element 마다 동적 거동을 분석하였다. 실제 궤적을 적용하여 드릴 파이프의 굽힘이나 중력으로 인하여 Wellbore와 접촉되는 부분에 마찰을 적용하였고, 또한 마찰 작용 시 일정한 축 방향 속도를 유지하기 위한 PI제어 값을 설계하여 drillstring 전체의 각속도 변화와 실제 드릴 굴착 작업 중 발생하는 stick slip현상을 관찰하였다.

• 한국정밀공학회지
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• 제20권3호
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• pp.89-96
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• 2003

An electro-hydraulic manipulator using hydraulic actuators has many nonlinear abetments, and its parameter fluctuations are greater than those of an electrically driven manipulator. So it is relatively difficult to realize not only stable but also accurate trajectory control for the autonomous assembly tasks using hydraulic manipulators. In this report, we propose a two-degree-of-freedom control including parallel feedforward compensator (PFC) where PFC plays a very important role in the stability of a proposed control system. In the experimental results of the 6-link electro hydraulic manipulator, it is verified that the stability and the model matching performance are improved by using the proposed control method.

• 한국항공우주학회지
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• 제49권8호
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• pp.681-688
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• 2021

본 논문은 시험발사체의 비행궤적 및 낙하점 분산 분석에 대해 다룬다. 2018년 11월의 시험발사체 비행시험 전/후에 수행한 비행궤적 및 낙하점 분산 분석 과정을 설명하고 비행시험 결과와의 비교를 통해 분산 분석 방안이 적절하였음을 보인다. 발사체의 궤적 및 낙하점 분산은 발사체 성능 오차 요인 및 대기권에서의 바람 영향을 고려한 6자유도 몬테카를로 시뮬레이션을 통해 이루어진다. 이와 같이 사전에 분석한 결과를 토대로 비행시험 전에 낙하 안전 영역을 설정한다. 결과적으로, 시험발사체는 사전에 분석한 궤적 및 낙하점 분산 범위 내에서 안전하게 비행하였다.

• 한국해양공학회지
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• 제34권3호
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• pp.180-193
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• 2020

In this study, the end-effector tracking performance of a manipulator installed on a remotely operated vehicle (ROV) for autonomous underwater intervention is verified. The underwater manipulator is an ARM 7E MINI model produced by the ECA group, which consists of six joints and one gripper. Of the six joints of the manipulator, two are revolute joints and the other four are prismatic joints. Velocity control is used to control the manipulator with forward and inverse kinematics. When the manipulator approaches a target object, it is difficult for the ROV to maintain its position and posture, owing to various disturbances, such as the variation in both the center of mass and the reaction force resulting from the manipulator motion. Therefore, it is necessary to compensate for the influences and ensure the relative distance to the object. Simulations and experiments are performed to track the trajectory of a virtual object, and the tracking performance is verified from the results.