• Journal of Mechanical Science and Technology
• /
• 제17권11호
• /
• pp.1725-1731
• /
• 2003

A high level CVT ratio control algorithm is proposed to improve the engine performance by considering the powertrain response lag. In this algorithm, the desired CVT speed ratio is modified from the vehicle velocity, which is estimated after the time delay due to the powertrain response lag. In addition, the acceleration map is constructed to estimate the vehicle acceleration from the throttle pedal position and the CVT ratio. Using the CVT ratio control algorithm and the acceleration map, vehicle performance simulations are performed to evaluate the engine performance and fuel economy. It is found that the fuel economy can be improved about 3.6% for FUDS by the ratio control algorithm for the target vehicle. In selecting the appropriate time delay, compromise between the fuel economy and the acceleration performance is required.

• 한국자동차공학회논문집
• /
• 제5권2호
• /
• pp.120-126
• /
• 1997

In this study, an effective estimation method of wheel acceleration is presented. The wheel acceleration is mainly used in the ABS(anti-lick brake system) and the TCS(traction control system). The wheel acceleration is a derivative term of the wheel speed which is generally measured by the wheel speed sensors. The results of a simple differentiation of the signal and an observation of the signal by Kalman filter show that Kalman filter has better performance than the simple differentiation. The differentiated sine signal which is contaminated with random noise shows a rugged signal compared with the signal which is filtered by the Kalman filter. The covariance of the differentiated signal is higher than that of the Kalman-filtered signal, too. The presented Kalman filter technique shows an effective way of solution to get the estimated wheel acceleration value which is sufficient to be applied to ABS or TCS control algorithms.

• 소음진동
• /
• 제6권2호
• /
• pp.215-224
• /
• 1996

Active vibration control is generally used to reduce vibration level by the actuators based on measured signal. Dynamic properties of a structure can be easily modified by the active vibration control, so that the vibration level may be effectively reduced to the magnitude below the allowable limit over a wide frequency rangs. In this paper, an instantaneous optimal control algorithm including acceleration feedback is presented for the active vibration control of large structures considering facts that the acceleration response can be easily measured, but the displacement and velocity response are obtained by numerically integrating the measured acceleration response with some errors. The adverse effect of the time delay is overcomed by taking into account the dynamic characteristics of an actuator and filters in the design of controller. Performance test is carried out using a hydraulic active mass driver on a test structure$(L{\times}W{\times}H;=;1200mm{\times}800mm{\times}1600mm, about;500kg)$ supported by four columns under base excitations. It is confirmed that the vibration level of the test structure are reduced to about 1/6 near resonance.

• 한국지능시스템학회논문지
• /
• 제5권4호
• /
• pp.101-110
• /
• 1995

본 연구에서는 직류 서보전동기의 위치, 속도 및 토오크 등의 제어기법중 외란에 대해 강인한 것으로 평가되고 있는 기존의 가속도 제어기법을 해석하고 그 결과 적용상의 문제점으로 판단되는 계통 파라미터 변화에 대한 강인성을 개선하기 위한 대책으로서 변경된 가속도제어 루프를 포함한 위치제어계를 제안하고 이를 직류전동기의 위치제어게 적용하였다. 제안된 제어계는 가속도제어기와 자기종조 퍼지 PID 제어기로 구성되어 있으며 제안된 제어계와 기존의 가속도제어계와의 근복적 차이점은 이 제어기법의 핵심 요소라 할 수 있는 가속도 기준입력 정정량의 발생기구로서 고전적 PID제어기를 자동조정하는 자기동조 PID 제어방식을 채택하였다는 점이다. 이 기준입력 발생기구를 도입한 직류전동기 위치제어계의 성능을 검토하기 위하여 그 응답특성을 기존의 가속도제어 위치제어계의 응답특성과 비교한 결과 파라미터 변화에 대한 강인성, 과도 특성 및 정상상태 특성면에서 제안된 제어계가 매우 우월한 성능을 가짐을 확인하였다. 따라서 제안된 제어기법은 기존의 가속도제어에 근거한 위치제어계의 성능을 개선시켜줌으로써 이 제어기법의 적용범위 확대에 기여하며 특히 모델의 불확정성이 크거나 부하등 운전환경이 크게 변화하는 악조건 하에서의 정밀한 위치제어에 적용될 수 있다.

• 한국항공우주학회지
• /
• 제37권12호
• /
• pp.1217-1224
• /
• 2009

고정익 항공기가 3차원의 복잡한 경로를 추종하기 위해 필요한 비교적 간단하며 효과적인 유도 제어 방법을 제시한다. 소개되는 방법은 비선형 경로 추종 유도 기법을 외부 루프로 사용한다. 외부 루프는 원하는 경로와 함께 항공기의 현재 위치와 속도를 바탕으로 비행 경로를 변화하기 위한 가속도 명령을 생성한다. 가속도 명령은 중력과 벡터적으로 결합되어 Specific Force Acceleration을 만든다. 이렇게 생성된 Specific Force Acceleration은 내부 루프를 위한 명령으로 쓰이는데, 이는 항공기가 가속도 자체보다는 Specific Force Acceleration을 더 직접적으로 제어할 수 있기 때문이다. 나아가 배면 비행이나 Slow Roll, Knife-Edge 등과 같은 옆미끄럼짐 기동을 하기 위해 필요한 롤 자세 제어 기법도 제시한다. 마지막으로 표준이 되는 여러 가지 곡예비행 경로들에 대한 시뮬레이션을 수행함으로써 제시된 기법의 성능을 검증한다.

• 제어로봇시스템학회논문지
• /
• 제19권5호
• /
• pp.462-467
• /
• 2013

This paper presents a modified disturbance observer (MDOB) for controlling two arms of a manipulator designed for a home service robot. The MDOB is slightly different from the original DOB in that it uses an accelerometer to measure acceleration of the robot arm. Then it uses the acceleration to estimate the disturbance to cancel out in the control loop. Relying on the acceleration information of the robot arm, a partial model-based control structure is formed. Experimental studies of position control of 2 DOF robot arm are conducted to evaluate the performance of the proposed position control by an MDOB method.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 2003년도 ICCAS
• /
• pp.1387-1391
• /
• 2003

The fundamental aim of this paper is to present a solution algorithm to achieve cooperative contour controlling, under joint acceleration constraint with maximum cooperative speed. Usually, the specifications like maximum velocity of cooperative trajectory are determined by the application itself. In resolving the cooperative trajectory into two complementary trajectories, an optimum task resolving strategy is employed so that the task assignment for each robot is fair under the joint acceleration constraint. The proposed algorithm of being an off-line technique, this could be effectively and conveniently extended to the existing servo control systems irrespective of the computational power of the controller implemented. Further, neither a change in hardware setup nor considerable reconfiguration of the existing system is required in adopting this technique. A simulation study has been carried out to verify that the proposed method can be realized in the generation of complementary trajectories so that they could meet the stipulated constraints in simultaneous maneuvering.

• 전자공학회논문지SC
• /
• 제48권4호
• /
• pp.108-113
• /
• 2011

본 논문에서는 손목 부근에 장착한 근전도 및 가속도 센서를 통하여 기존 로봇의 차대 제어와 다른 새로운 방식의 제어 방법을 제안한다. 제안 하는 방법은 자동차를 운전하는 듯이 직관적인 팔의 움직임만으로 로봇을 원격 제어한다. 근전도 센서로부터 얻은 신호를 통하여 로봇 제어 여부를 결정하고 가속도 센서로부터 얻은 신호로부터 동작을 추론하여 추론된 동작에 해당되는 명령에 따라 전진, 후진, 좌회전, 우회전으로 제어한다. 4가지 동작에 대한 정확성은 99% 이상이며 실시간 지연 없이 자연스러운 제어가 가능하였다. 전체 시스템을 직접 구현하고 시현을 통하여 성능 및 유용성을 확인하였다

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2002년도 추계학술대회논문집
• /
• pp.1028-1033
• /
• 2002

This paper concerns on a non-rotating axis-active magnetic bearing (AMB) system subject to base motion. In such a system, it is desirable to retain the axis within the predetermined air-gap. Motivated from this, an optimal acceleration feedforward control is proposed to reduce the base motion response without deteriorating other feedback control performances. Experimental results demonstrate that the proposed feedforward control reduces the air-gap deviation to 29% that by feedback control alone.

• International Journal of Automotive Technology
• /
• 제8권3호
• /
• pp.351-359
• /
• 2007

In this study, a hierarchical switching control scheme based on robust control theory is proposed for tracking control of vehicle longitudinal acceleration in the presence of large uncertainties. A model set consisting of four multiplicative-uncertainty models is set up, and its corresponding controller set is designed by the LMI approach, which can ensures the robust performance of the closed loop system under arbitray switching. Based on the model set and the controller set, a switching index function by estimating the system gain of the uncertainties between the plant and the nominal model is designed to determine when and which controller should be switched into the closed loop. After theoretical analyses, experiments have also been carried out to validate the proposed control algorithm. The results show that the control system has good performance of robust stability and tracking ability in the presence of large uncertainties. The response time is smaller than 1.5s and the max tracking error is about $0.05\;m/S^2$ with the step input.