• Smart Structures and Systems
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• 제21권3호
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• pp.373-387
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• 2018

Semi-active isolation systems based on leverage-type stiffness control strategies have been widely studied. The main concept behind this type of system is to adjust the stiffness in the isolator to match the fundamental period of the isolated system by using a simple leverage mechanism. Although this system achieves high performance under far-field earthquakes, it is unsuitable for near-fault strong ground motion. To overcome this problem, this study considers the potential energy effect in the control law of the semi-active isolation system. The minimal energy weighting (MEW) between the potential energy and kinetic energy was first optimized through a series of numerical simulations. Two MEW algorithms, namely generic and near-fault MEW control, were then developed to efficiently reduce the structural displacement responses. To demonstrate the performance of the proposed method, a two-degree-of-freedom structure was employed as a benchmark. Numerical results indicate that the dynamic response of the structure can be effectively dampened by the proposed MEW control under both far-field and near-fault earthquakes, whereas the structural responses resulting from conventional control methods may be greater than those for the purely passive control method. Moreover, according to experimental verifications, both the generic and near-fault MEW control modes yielded promising results under impulse-like earthquakes. The practicability of the proposed control algorithm was verified.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2000년도 추계학술대회 논문집
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• pp.144-147
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• 2000

In this paper, ANFIS intelligence control of a semi-active suspension system is investigated. The strength of the ER damper is controlled by a high voltage power supply. This paper deals with a two-degree-of-freedom suspension using the damper with ERF for a quarter vehicle system. The control law for semi-active suspensions modeled in this study is developed using passive and ANFlS control method. Computer simulation results show that the semi-active suspension with ERF damper has good performances of ride quality

• 항공우주기술
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• 제10권1호
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• pp.98-106
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• 2011

본 논문에서는 롤 자세운동이 발생하는 상황에서 안정적인 피치/요 자세제어를 위한 항법쿼터니언 기반 자세제어기 구조를 설계하고, 발사체 6자유도 시뮬레이션을 통해 설계된 제어기의 성능평가를 수행하였다. 항법쿼터니언 자세제어기는 기존 KSR-III, KSLV-I 상단부 자세제어기 설계 경험을 기반으로 고안되었고, 탑재소프트웨어 내에서 효율적인 자세제어 변수 사용 및 KSR-III, KSLV-I 상단부 제어기와 동일한 성능 확보 관점에서 설계되었다. 제안된 새로운 자세제어기 타당성 분석을 위하여 방위각 전환을 위한 롤 기동, 롤 자세제어가 수행되지 않는 두 비행조건에 대해 6자유도 시뮬레이션을 수행, 자세제어 성능을 평가하고 탑재 소프트웨어로서 적용 가능성을 확인하였다.

• 대한기계학회논문집A
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• 제21권8호
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• pp.1209-1217
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• 1997

This paper proposes the modeling of the dynamics of two cooperating robot manipulators performing the assembly job such as peg-in-hole while coordinating the payload along the desired path. The mass and moment of inertia of the manipulators and the payload are assumed to be unknown. To control the uncertain system, a robust control algorithm based on the computed torque control is proposed. Usually, the robust controller requires high input torques such that it may face input saturation in actual application. In this reason, the robust control algorithm includes fuzzy logic such that the magnitude of the input torque of the manipulators is controlled not to go over the hardware saturation while keeping path tracking errors bounded. A numerical example using dual three degree-of-freedom manipulators is shown.

• 대한전자공학회논문지TE
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• 제42권4호
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• pp.47-52
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• 2005

본 논문에서는 다변수 제어시스템 설계시 효과적인 제어를 어렵게 만드는 요인 중의 하나인 입력과 출력의 결합문제를 해결하기 위해서 각 채널의 출력변수는 대응되는 입력 신호에 의해서만 독립적으로 조정되도록 하는 비결합 제어기를 설계하였다. 설계된 제어기는 비결합 조건뿐만 아니라 제어계의 강인성을 동시에 고려할 수 있는 특성을 2자유도 구조에 적용하였다. 또한 제어기를 구하는 경우 계산을 용이하게 하기 위해서 플랜트를 표준모델로 확장시킨 후 전달행렬을 이용하여 상태공간계수로 표현하였다. 이 경우 비결합제어기의 자유매개변수를 구하는데 있어서 지능형탐색방법의 일종인 유전알고리즘을 적용하였다. 일반적으로 유전알고리즘을 특정한 문제에 적용할 경우 그 문제가 가지고 있는 최적화 특징을 잘 파악하여 이것을 이용하는 것이 유전알고리즘 적용시 성공여부를 결정하는 중요한 요인이 된다. 따라서 본 논문에서는 유전알고리즘을 이용하여 고정 차수의 정방 비결합제어기의 $H_{\infty}$설계시 효율적인 방법을 제시하였다.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1997년도 봄 학술발표회 논문집
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• pp.147-151
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• 1997

The dynamic characteristics of Control Element Drive Mechanism (CEDM) in Korea standard Nuclear Power Plant was reviewed as a secondary mass in a simplified two degree of freedom system, while the reactor vessel as a primary mass. The design improvement stratege to minimize each displacement amplitude of these primary and secondary masses was proposed. According to this stratege the designs of CEDM components, the shroud and the pressure housing, respectively, were changed using optimization technique.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1989년도 하계종합학술대회 논문집
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• pp.693-697
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• 1989

In this paper, force control for a multi-legged walking robot is investigated. For stable but relatively rapid walking, a simple force control algorithm is proposed in conjunction with the position control system. The proposed control method is tested on an experimental one leg system of two degree of freedom with a force controller using a position controller and a monoboard microcomputer to implement the proposed control algorithm. The experimental results shows that the control algorithm can be applied for walking in a terrain with wide range variation.

• 한국정밀공학회지
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• 제14권4호
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• pp.104-109
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• 1997

A robust controller design to corrdinate a robot manipulator under unknown system parameters and bounded disturbance inputs is presented in this paper. Generally, robust controllers require high input torque so that they may face input saturation in actual application due to the power limitation of the actuator. To solve this problem, an improved robust controller with saturated input torque using a fuzzy logic control is proposed. Numerical examples are shown to validate the proposed controller using two degree-of-freedom planar arm.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1994년도 Proceedings of the Korea Automatic Control Conference, 9th (KACC) ; Taejeon, Korea; 17-20 Oct. 1994
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• pp.82-87
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• 1994

In this study, dynamic optimal design far a two degree-of-freedom anthropomorphic robot module is performed. Several dynamic design indices associated with the inertia matrix and the inertia power array are introduced. Analysis for the relationship between the dynamic parameters and the design indices shows that trade-offs exist between the isotropy and the dynamic design indices related to the actuator size. A composite design index is employed to deal with multi-criteria based design with different weighting factors, in a systematic manner. We demonstrate the fact that dynamic optimization is another significant step to enhance the system performances, followed by kinematic optimization.

• 전자공학회논문지S
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• 제34S권12호
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• pp.41-49
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• 1997

This paper deals with the attitude control of a self-made VTOL vehicle which is round shape and has four fans and motors. Although hovering mechanisms are suitable for field work at a mountainous region or a building site etc., it is known that modeling the structure of the plant is quite difficult due to its unstable or uncertain characteristics. So, a robust controller is requried in order to cope with these uncertainties. WE first model the structure of the plant under the actual hovering setting and then determine the uncertainty of the acquired mathematical model by using system identification method as exactly as possible. We adopt the $H^{\infty}$ theory as a control algorithm because of its availability, and the structure of two-degree-of-freedom is used as a basic feedback control system to improve the transient response of the plant. Finally, we show the appropriateness of the designed controller through simulations and experiments. That is, the proposed VTOL system is able to maintain its roubust performance in spite of parameter variations and existing disturbances..