• 한국항공우주학회지
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• 제50권5호
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• pp.325-332
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• 2022

우주탐사 임무를 수행하기 위해서는 탐사선에 수직이착륙 기능이 필수적으로 탑재되어야 한다. 수직이착륙을 위해서는 탐사선의 엔진이 적절한 추력제어 정확도와 짧은 응답시간을 가져야 한다. 하이브리드 로켓은 이러한 조건을 만족할 수 있는 높은 수준의 추력제어 능력을 갖고 있다. 이 연구는 개발한 하이브리드 로켓 엔진의 추력제어 성능이 수직이착륙에 적절한지 검증하는 것을 목적으로 하고 있다. 이를 위해 가압장치 없이 공급압력이 감소하는 산화제 공급시스템을 적용한 엔진을 사용하여 약 10초 내외의 임무를 수행하고자 하였고, 공급압력 감소가 추력제어 정확도와 응답시간에 미치는 영향을 확인하였다. 실험결과에 의하면 적절한 감소율과 초기 압력 수준이 추력제어 정확도와 응답시간에 중요한 영향을 미치는 인자로 확인되었으며 고도제어 시뮬레이션을 통해 추력제어 성능을 검증했다.

• 대한전자공학회논문지TC
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• 제43권8호
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• pp.84-90
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• 2006

최근 무선 인터넷 및 WLAN이 활성화되면서 3G 이동 통신망과 WLAN망의 연동으로 보다 넓은 서비스 영역에서 높은 데이터 전송 속도를 제공하기 위한 연구가 활발하게 이루어지고 있다. 3G와 WLAN 연동망에서 이동 단말이 서로 다른 망으로 이동할 경우 높은 데이터 전송을 제공하기 위해서 끊김 없는 vertical handoff를 수행한다. 이동 단말이 TCP 연결 상태에서 vertical handoff를 수행하여 대역폭이 다른 망으로 이동할 경우 기존의 TCP 정보를 그대로 이용하면 3G와 WLAN 망간의 서로 다른 대역폭으로 인하여 패킷 손실이 발생하고 이로 인하여 TCP 성능이 낮아지게 된다. 본 논문은 vertical handoff를 통해 새로운 망으로 이동하였을 경우 사용 가능한 대역폭을 측정하여 TCP에 적용함으로써 TCP의 성능향상을 위한 새로운 혼잡제어 알고리즘을 제안하였고, ns-2 시뮬레이션을 통해 기존에 제안되었던 알고리즘보다 vertical handoff 시 TCP 성능이 향상됨을 보였다.

• 대한조선학회논문집
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• 제46권4호
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• pp.382-390
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• 2009

The submerged body near the free surface is disturbed by the 1st and 2nd order wave forces, which results in unstable movements when no control is applied. In this paper, the vertical motions of the submerged body are analyzed, and the time-variant nonlinear system for the vertical motions of the submerged body is transformed to the time-invariant linear system in state space. Next, depth controller of the submerged body is designed by using LQR control, one of the modern optimal control technique. Numerical simulation shows that effective depth controls can be achieved by LQR control.

• 한국태양에너지학회 논문집
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• 제34권1호
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• pp.19-27
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• 2014

Exterior vertical illuminance is an important factor for lighting control. But, there are not many researches about the exterior illuminance on a vertical surface. In this study, we predicted the exterior illuminance on a vertical surface using vertical luminous efficacy. First, we calculated the vertical luminous efficacy according to the sky clearness category. And we performed the statistical analysis of the measured and the calculated illuminance with luminous efficacy. The MBE and RMSE of the predicted exterior illuminance were-1.2% and 15.5%, respectively. Second, the annual illuminance on a vertical surface calculated with the luminous efficacy and the short-term measured solar irradiance was suggested in this study.

• 한국운동역학회지
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• 제17권4호
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• pp.57-64
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• 2007

The purpose of this study was to investigate comparative analysis of the vertical ground reaction force variables during landing from vertical jump blocking in volleyball through GRF analysis system. The subjects participated in this study were 6 male university volleyball player and 6 male acted as a control group. The results are as follows: 1. The skilled group was longer than the unskilled group in flight time during vertical jump blocking. 2. The skilled group was faster than the unskilled group in tFz2 during landing from vertical jump blocking. 3. The skilled group was higher than the unskilled group in Fz2 during landing from vertical jump blocking. 4. The skilled group was higher than the unskilled group in Fz2LR during landing from vertical jump blocking. 5. The skilled group was higher than the unskilled group in impulse during landing from vertical jump blocking. Consequently, during landing from vertical jump, the landing strategy of the skilled group was found as a form of a stiff landing. Therefore, this landing strategy will be required to strengthen of hip and knee extensors and ankle plantar flexors for injury prevention.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2002년도 가을 학술발표회 논문집
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• pp.362-369
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• 2002

This paper mainly propose the new passive vibration control device, named BRV(the bridge reduced vibration), for reducing excessive traffic-induced vibration of bridges and for measuring performance of BRV numerical example was simulated. The purpose of BRV is mainly on reducing vertical acceleration and displacement of bridge. In BRV we can control the stiffness and damping coefficient to accept the performance we want. The result of simulation showed that the vertical acceleration and displacement was effectively diminished. It would be concluded that BRV can be used to improve the serviceability of bridge and fatigue life etc.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1998년도 제13차 학술회의논문집
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• pp.47-52
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• 1998

This study deals with guidance and control laws for an optimal reentry trajectory of a vertical landing reusable launch vehicle (RLV) in the future. First, a guidance law is designed to create the reference trajectory which minimizes propellant consumption. Then, a nonlinear feedback controller based on a linear quadratic regulator is designed to make the vehicle follow the predetermined reference trajectory, The proposed method is simulated for the first stage of the H-II scale rocket.

• 제어로봇시스템학회논문지
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• 제9권11호
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• pp.937-942
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• 2003

We present a self-localization method for mobile robots using vertical line features of indoor environment. When a 2D map including feature points and color information is given, a mobile robot moves to the destination, and acquires images from the surroundings having vertical line edges by one camera. From the image, vertical line edges are detected, and pattern vectors meaning averaged color values of the left and right regions of the each line are computed by using the properties of the line and a region growing method. The pattern vectors are matched with the feature points of the map by comparing the color information and the geometrical relationship. From the perspective transformation and rigid transformation of the corresponded points, nonlinear equations are derived. Localization is carried out from solving the equations by using Newton's method. Experimental results show that the proposed method using mono view is simple and applicable to indoor environment.

• 제어로봇시스템학회논문지
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• 제19권12호
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• pp.1111-1118
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• 2013

In this paper, the disturbance applied to launcher hatch by ship motions is introduced to identify the vertical ship motion disturbance. Basically, ship motions are comprised of 6 degrees of freedom: roll, pitch, yaw, heave, surge and sway. In the case of the shipboard launcher hatch the coupled pitch, heave and roll are significant motions to be transformed to a vertical direction motion. The maximum acceleration values are obtained from the vertical motion model and the ship motion data in accordance with ship type and hatch location on the ship. We verify that the maximum pitch motion mainly influences the launcher hatch and also present the quantity of the maximum load disturbance by the ship's motion acceleration.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.1082-1087
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• 2003

In this paper, we address the development of magnetic levitation positioning system. This planar magnetic levitator employs four permanent magnet liner motors. Each motor generates vertical force for suspension against gravity, as well as horizontal force for drive levitation object called a platen This stage can generate six degrees of freedom motion by the vertical and horizontal force. We derived the mechanical dynamics equation using lagrangian method and used coenergy to express an electromagnetic force. We proposed control algorithm for the position and posture control from its initial value to its desired value using sliding mode control. Some simulation result is provided to verify the effectiveness of the proposed control scheme.