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MVC 상태에서의 무릎관절 모멘트 추정을 위한 모델 개발
남윤수,이우은,Nam, Yoon-Su,Lee, Woo-Eun 대한의용생체공학회 2008 의공학회지 Vol.29 No.3
This paper introduces a method of estimating the knee joint moment developed during MVC. By combining the Hill-type muscle model and analytic results on moment arm and musculotendon length change as a function of hip and knee joint angle, the knee joint moment at a specific knee joint angle during MVC is determined. Many differences between the estimated results and the experimental data are noted. It is believed that these differences originate from inaccurate information on the muscle-tendon parameters. The establishment of exact values for the subject's muscle parameters is almost impossible task. However, sensitivity analysis shows that the tendon slack length is the most critical parameter when applying the Hill-type muscle model. The effect of a change of this parameter on the muscle length force relationship is analyzed in detail.
남윤수,Nam, Yun-Su 대한기계학회 2001 大韓機械學會論文集A Vol.25 No.3
A dynamic load simulator(DLS) which can reproduce on-ground the aerodynamic hinge moment of control surface is an essential rig for the performance and stability test of aircraft actuation system. By setting up load actuator as counter acting with the control surface driving actuator and designing an appropriate force control system for load actuator, DLS can be mechanized. Obtaining an accurate mathematical model for the DLS is the first step to successfully design an aerodynamic load replicati on system. Two theoretical models are presented and tested for their validities with the experimental results, which turns out to be not successful. An alternative way of using system identification approaches in investigated to develop a good nominal model for DLS dynamics, and suitable uncertainty bounds for this nominal model are proposed with the consideration of experimental results.
스트레인 게이지 변위추정 센서를 사용한 유동공진 가진기 설계
남윤수,최재혁,강병하,Nam, Yun-Su,Choe, Jae-Hyeok,Gang, Byeong-Ha 대한기계학회 2002 大韓機械學會論文集A Vol.26 No.9
Heat dissipation technology using the flow resonant phenomenon is a kind of a new concept in the heat transfer area. A vibration exciter is needed to enhance air flow mixing which has the natural shedding frequency of thermal system. A mechanical vibrating device for the air flow oscillation is introduced, which is driven by a moving coil actuator with a displacement estimator using strain gage. An analytical dynamic model for this mechanical vibration exciter is presented and its validity is checked by the comparison with experimental data. Values of some unknown system parameters in the analytic model are estimated through the system identification approach. Based on this mathematical model, the vibration exciter using strain displacement estimator is developed. During the experimental verification phase, it turns out the high modal resonant characteristics of a vibrating plate are a major barrier against obtaining a high bandwidth vibration exciter.
남윤수(Yoonsu Nam),박종식(Jongsik Park),윤태준(Taejun Yoon),유능수(Neungsoo Yoo) 대한기계학회 2008 대한기계학회 춘추학술대회 Vol.2008 No.5
Design of control strategy and structure gives a direct impact on wind turbine's performance and life cycle. A variable rotor speed and variable pitch control strategy is introduced, and a mathematic model of wind turbine dynamics is derived. By using a numeric optimization algorithm, the steady state operating conditions of wind turbines are identified. Because aerodynamic interaction of winds with rotor blades is basically nonlinear, a linearization procedure is applied to analyze wind turbine dynamic variations for whole operating conditions.
FBW 항공기의 DDV 구동장치에 대한 구동전류 고장 모니터 설계
남윤수(Yoonsu Nam),박해균(Hae Kyoon Park),안종민(Jongmin Ahn),최섭(Sup Choi),권종광(Jongkwang Kwon) 한국항공우주학회 2006 韓國航空宇宙學會誌 Vol.34 No.3
본 논문은 유압 공급 변에서는 2중으로 전기제어 면에서는 3중으로 다중화된 DDV 구동장치에 대한 구동전류 고장 모니터 설계에 관한 논문이다. 다중화된 신호들 가운데 어느 한 채널에 고장이 발생한다면, 이 신호는 정확히 감지되어야 하고, 시기적절하게 제거 되어야 하며, 남겨진 정상채널들은 그 기능이 재조정되어야 한다. 조종면 구동장치의 고장 모니터 설계는 비행체 역학, 비행제어법칙, 그리고 유압 구동장치 운통특성이 모두 고려된 통합적 관점에서 수행되어야 한다. MIL-F-8785C에서 규정하고 있는 고장에 따른 비행체 천이 응답 요구조건으로부터 조종면 구동장치의 고장이탈 한계를 결정하는 설계 방법이 제시되었다. This paper deals with a driving current fault monitor design methodology for a DDV actuation system which has a dual hydraulic power supply system, and triplex electric control capability. A fault existing among these redundant channels should be detected accurately and removed timely, and the remaining channels are to be reconfigured in order to compensate the role of a removed faulty channel. An integrated analysis on the aerodynamics, flight control laws, and DDV actuation system is essential for the design of an actuation system fault monitor. A method to define a fault transient boundary which specifies a maximum travel of an actuation system caused by the first faulty operation is proposed based on the top level requirement on the fault effect specified in MIL-F-878SC.
남윤수(Yoonsu Nam),최한순(Han Soon Choi) 대한기계학회 2012 大韓機械學會論文集A Vol.36 No.5
요 제어는 풍력 터빈의 전력 생산과 구조물의 기계적인 하중 발생에 밀접한 관계를 갖고 있다. 풍력 터빈으로 불어오는 바람의 방향과 나셀(nacelle)의 방향이 일치하지 않을 경우 발생하는 요 오차에 의하여, 풍력 터빈의 에너지 회수 효율이 감소하고, 블레이드(blade)에는 비대칭/불평형 하중이 증가하게 된다. 따라서, 요 오차를 감소시키기 위한 요 제어 시스템은 풍력 터빈의 중요한 서브시스템 중에 하나이다. 그러나, 요 운동은 요 축 주위에 발생하는 여러 하중들에 의하여, 그 운동의 빠르기가 제약을 받게 된다. 본 논문에서는 기본적인 요 시스템의 원리에 대하여 간략히 살펴보고, 요 운동에 의하여 회전 날개에 발생된 기계적 하중이 어떻게 요 축 주위의 하중들로 전파되는지, 또한 이러한 하중들의 특성은 무엇인지에 대하여 살펴보았다. The yaw control, a major part of the wind turbine, is closely related to the efficiency of electric power production and the mechanical load. The yaw error, which results from the nacelle not being appropriately aligned in the wind direction, not only decreases the power output but also reduces the lifetime of the wind turbine as a result of large fatigue loads. However, the yawing rate cannot be increased indefinitely because of constraints on mechanical loads. This paper investigates the characteristics of an active yaw control system, the basic principle of the system, and mechanical loads around the yaw axis during yawing.
MW 규모 풍력 터빈의 기계적 하중 특성 해석 및 제어
남윤수(Yoonsu Nam),최한순(Hansoon Choi) Korean Society for Precision Engineering 2010 한국정밀공학회지 Vol.27 No.9
A multi-MW wind turbine is a huge mechanical structure, of which the rotor diameter is more or less than 100 m. Rotor blades experience unsymmetric mechanical loads caused by the interaction of incoming wind with the tower and wind shear effect. These mechanical loads are transferred to the entire structure of the wind turbine and are known as the major reasons for shortening the life span of the wind turbine. Therefore, as the size of wind turbine gets bigger, the mitigation of mechanical loads becomes more important issue in wind turbine control system design. In this paper, a concept of an individual pitch control(IPC), which minimizes the mechanical loads of rotor blades, is introduced, and simulation results using IPC are discussed.