• Journal of Mechanical Science and Technology
• /
• 제18권4호
• /
• pp.535-549
• /
• 2004

This paper proposes a sliding mode controller with fuzzy adaptive perturbation compensator(FAPC) to get a good control performance and reduce the chatter, The proposed algorithm can reduce the chattering because the proposed fuzzy adaptive perturbation compensator compensates the perturbation terms. The compensator computes the control input for compensating unmodeled dynamic terms and disturbance by using the observer-based fuzzy adaptive network(FAN) The weighting parameters of the compensate. are updated by on-line adaptive scheme in order to minimize the estimation error and the estimation velocity error of each actuator. Therefore, the combination of sliding mode control and fuzzy adaptive network gives the robust and intelligent routine to get a good control performance. To evaluate the control performance of the proposed approach, tracking control is experimentally carried out for the hydraulic motion platform which consists of a 6-DOF parallel manipulator.

• 대한기계학회논문집A
• /
• 제25권3호
• /
• pp.339-352
• /
• 2001

The inverse kinematics problem of Stewart platform is straightforward, but no closed form solution of the forward kinematic problem has been presented. Since we need the real-time forward kinematic solution in MIMO control and the motion monitoring of the platform, it is important to acquire the 6 DOF displacements of the platform from measured lengths of six cylinders in small sampling period. Newton-Raphson method a simple algorithm and good convergence, but it takes too long calculation time. So we reduce 6 nonlinear kinematic equations to 3 polynomials using Nairs method and 3 polynomials to 2 polynomials. Then Newton-Raphson method is used to solve 3 polynomials and 2 polynomials respectively. We investigate operation counts and performance of three methods which come from the equation reduction and Newton-Raphson method, and choose the best method.

• 대한기계학회논문집
• /
• 제18권7호
• /
• pp.1632-1642
• /
• 1994

The Stewart Platform is a six-degree-of-freedom in-parallel-actuated manipiulator mechanism. The kinematic behavior of parallel mechanisms shows inverse characteristics as compared that of serial mechanisms; i.e, the inverse kinematic problem of Stewart Platform is straightforward, but no closed form solution of the forward kinematic problem has been previously presented. Thus it is difficult to calculate the 6 DOF displacement of the platform from the measured lengths of the six actuators in real time. Here, a real-time estimation algorithm which solves the Stewart Platform kinematic problem is proposed and tested through computer simulations and experiments. The proposed algorithm shows stable convergence characteristics, no estimation errors in steady state and good estimation performance with higher sampling rate. In experiments it is shown that the estimation result is the same as that of simulation even in the presence of measurement noise.

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

• Wind and Structures
• /
• 제18권3호
• /
• pp.267-279
• /
• 2014

Hydrodynamic analyses of classic and truss spar platforms for floating offshore wind turbines (FOWTs) were performed in the frequency domain, by considering coupling effects of the structure and its mooring system. Based on the Morison equation and Diffraction theory, different wave loads over various frequency ranges and underlying hydrodynamic equations were calculated. Then, Response Amplitude Operators (RAOs) of 6 DOF motions were obtained through the coupled hydrodynamic frequency domain analysis of classic and truss spar-type FOWTs. Truss spar platform had better heave motion performance and less weight than classic spar, while the hydrostatic stability did not show much difference between the two spar platforms.

• 대한기계학회논문집A
• /
• 제40권1호
• /
• pp.1-8
• /
• 2016

본 논문에서는 기존의 관성안정화 플랫폼에서 보편적으로 사용됐던 PID 제어에 외란관측기를 적용하는 알고리즘 제안한다. 외란관측기 알고리즘을 적용하기 위하여 직접구동 모터로 구동되는 안정화 플랫폼 축의 관성모멘트와 축 마찰 특성을 실험적으로 구하고, 시뮬레이션과 실험결과를 비교하여 정확도를 검증하였다. 또한 차수와 상대차수가 다른 여러 가지 Q-filter 적용실험을 통하여 필터 특성에 따른 시스템의 안정성을 확인하였다. 본 논문에서 제안한 알고리즘은 6 자유도 시뮬레이터를 이용하여 차량 모션 인가실험을 통해 이중 PID 제어 루프의 결과와 비교/검증하였다.

• 한국항공우주학회지
• /
• 제46권5호
• /
• pp.368-375
• /
• 2018

본 연구에서는 부유식 플랫폼의 6자유도 방향으로의 주기 운동이 로터 공력 성능에 미치는 영향을 확인하기 위해 부유식 해상 풍력터빈에 대한 공력 해석이 수행되었다. 수치 해석을 위해 블레이드 요소 운동량 방법을 이용하였으며, 유동 박리와 후류 영향에 의한 비정상 공력 효과를 포착하기 위해 인디셜 응답 방법에 기반한 동적 실속 모델을 이용하였다. 로터에 의해 유도되는 내리 흐름은 운동량 이론과 난류 후류 상태에 대한 경험적 모델을 연계하여 계산하였다. heave, sway, surge 방향으로의 병진 운동과 roll, pitch, yaw 방향으로의 회전 운동을 포함한 플랫폼 주기 운동을 고려하였으며, 각각의 모션은 사인함수 형태로 적용되었다. 수치해석을 위한 대상 풍력터빈으로는 NREL 5MW 풍력터빈이 사용되었다. 해석 결과로부터 세 방향 병진 운동 모드 중, surge 운동 시 로터 공력 변화가 상대적으로 크게 나타났으며, 회전 운동 모드의 경우, pitch 운동에 의해 로터 공력이 크게 변화됨을 확인할 수 있었다.

• 한국군사과학기술학회지
• /
• 제22권4호
• /
• pp.517-526
• /
• 2019

In the present study, unsteady flows around a projectile ejected from an aircraft platform have been numerically investigated by using a three dimensional compressible RANS flow solver based on unstructured meshes. The relative motion between the platform and projectile was described by six degrees of freedom(6DOF) equations of motion with Euler angles and a chimera technique. Initial behavior of the projectile for varying conditions, such as roll and pitch-yaw command on the control surface of the projectile, flight Mach number, and platform pitch angle, was investigated. The ejection stability of the projectile was degraded as Mach number increases. In the transonic condition, the initial behavior of the projectile was found to be unstable as increase of platform pitch angle. By applying the command to control surfaces of the projectile, initial stability was highly enhanced. It was concluded that the proposed simulation data are useful for estimating the ejection behavior of a projectile in design phase.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 2005년도 ICCAS
• /
• pp.296-301
• /
• 2005

This paper describes the kinematics, dynamics and control of a 6-DOF shaking table with a bell crank structure, which converts the direction of reciprocating movements. In this shaking table, the bell crank mechanism is used to reduce the amount of space needed to install the shaking table and create horizontal displacement of the platform. In kinematics, joint design is performed using $Gr{\ddot{u}}bler's$ formula. The inverse kinematics of the shaking table is discussed. The derivation of the Jacobian matrix is presented to evaluate singularity conditions. Considering the maximum stroke of the hydraulic actuator, collision between links and singularity, workspace is computed. In dynamics, computations are based on the Newton-Euler formulation. To derive parallel algorithms, each of the contact forces is decomposed into one acting in the direction of the leg and the other acting in the plane orthogonal to the direction of the leg. Applying the Newton-Euler approach, the solution of inverse dynamics is almost completely parallel. Only one of the steps-the application of the Newton-Euler equations to the platform-must be performed on one single processor. Finally, the efficient control scheme is proposed for the tracking control of the motion platform.

• 대한기계학회논문집A
• /
• 제20권2호
• /
• pp.414-430
• /
• 1996

In this paper, a new kinematic structure of a parallel manipulator with six Cartesian degrees of freedom is proposed. It consists of a platform which is connected to a fixed base by means of 3-PPSP(parameters P, S denote the prismatic, spherical joints) subchains. Each subchain has a link which is concected to a passive prismatic joint at the one end and a passive spherical joint at the other. The spherical joint is then attached to perpendicularly arranged prismatic actuators which are fixed at the base. The spherical joint is then attached to perpendicularly arranged prismatic actuators which are fixed at the base. This arrangement provides a basis to control all six Cartesian degrees of motion of the platform in space. Due to its efficient architecture, the colsed-form solutions of the inverse and forward kinematics can be obtained. As a consequence, this new kinematic structure can be servo controlled using simple inverse kinematics becaese forward kinematics allows for measuring the platform's position and orientation in Cartesian space. Furthermore, the proposed structure provides an effective functional workspace. Series of simulations are performed to verify the results of the kinematics analyses.