• 제어로봇시스템학회논문지
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• 제6권1호
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• pp.81-90
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• 2000

Parallel manipulator is suitable for the high precise task because it than has higher stiffness, larger load capacity and more excellent precision, due to the closed-lop structure, than serial manipulator. But the controller design for parallel manipulator is difficult because the parallel manipulator has both the complexity of structure and the interference of actuators. The precision improvement of parallel manipulator using a classical linear control scheme is difficult because the parallel manipulator has the tough nonlinear characteristics. In this paper, firstly, the kinematic analysis of a parallel manipulator used at the experiments is performed so as to show the controllability. The analysis of internal singular configuration of the workspace is performed using the kinematic isotropic index so a sto show the limitation of control performance of a simple linear controller with fixed control gains. Secondly, a control scheme is designed by using an adaptive fuzzy logic controller so that active joints of the parallel manipulator track more precisely the desired input trajectory. This adaptive fuzzy logic controller so that active joints of the parallel manipulator track more precisely the desired input trajectory. This adaptive fuzzy logic controller is often used for the control of nonlinear system because it has both the inference ability and the learning ability. Lastly, the effeciency of designed control scheme is demonstrated by the real-time control experiments with IBM PC interface logic H/W and S/W of my won making. The experimental results was a success.

• International Journal of Naval Architecture and Ocean Engineering
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• 제13권1호
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• pp.758-771
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• 2021

This paper presents a novel control scheme for the three-dimensional (3D) path following of underactuated Autonomous Underwater Vehicle (AUVs) subject to unknown internal and external disturbances, in term of the time scale decomposition method. As illustration, two-time scale motions are first artificially forced into the closed-loop control system, by appropriately selecting the control gain of the integrator. Using the singular perturbation theory, the integrator is considered as a fast dynamical control law that designed to shape the space configuration of fast variable. And then the stabilizing controller is designed in the reduced model independently, based on the time scale decomposition method, leading to a relatively simple control law. The stability of the resultant closed-loop system is demonstrated by constructing a composite Lyapunov function. Finally, simulation results are provided to prove the efficacy of the proposed controller for path following of underactuated AUVs under internal and external disturbances.

• 한국항공우주학회지
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• 제46권11호
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• pp.952-960
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• 2018

지구관측용 인공위성에서 고기동성이 많이 요구되고 있다. 고기동성을 만족시키기 위해 고토크 구동기가 인공위성 설계에서 필수적이다. 본 연구에서 고기동 소형위성 설계를 위해 한국항공우주연구원에서 연구되고 있는 5Nm급 소형 제어모멘트자이로(CMG, Control Moment Gyro) 개발 결과를 소개하였다. 구동로직 활용을 위해, 잘 알려진 Elliptic internal singularity를 성공적으로 회피하는 등으로 Singular Direction Avoidance (SDA) 방법에서 향상된 Designated Direction Escape (DDE) CMG 클러스터 구동로직에 대한 간단한 성능 검증과 상세한 로직 방법이 제시되었고, CMG가 피라미드 형태로 장착되었을 경우와 지붕 형태로 장착되었을 경우에 대해 5Nm급 소형 CMG가 고기동 소형위성 설계에 적절한지를 검증하기 위한 시뮬레이션이 수행되었다. 시뮬레이션 결과를 바탕으로 CMG 개발시 고려해야 할 의미있고 중요한 사항들을 제시하였다.