• 한국태양에너지학회 논문집
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• 제31권6호
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• pp.111-124
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• 2011

The objective of this study is to develop the blind control strategy and method which reduce negative effect of incoming daylight on visual comfort of occupants, minimize psychological anxieties caused by frequent motions of a blind, and maximize positive effect of incoming daylight by opening/closing of a blind. In previous researches on blind controls, major problem is that the time interval and amount of blind movement do not meet the control objective at the inflected zone of solar profile curve. To overcome these limitations revealed in theprevious researches, following tasks were performed in this study. i)To establish the control objective to accomplish the goal of this study. ii)To develop the control methods and algorithms which prevent glare on the work-plane at any time and which control the time interval and amount of blind movement to follow the control objective at various solar profile angle curves. This study proposed the control strategy and method that define the base control section implying the inflection point within the control objective zone and subsequently, divide the control sections for the residual time zones. The proposed strategy and method are found to increase the incoming daylight and solar irradiation by 0 to 15 %.

• 한국항공우주학회지
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• 제43권6호
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• pp.497-506
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• 2015

본 논문은 기동이 없는 이동표적에 대하여 탐색기의 FOV(field-of-view) 및 기동가속도 제한 내에서 충돌각 제어를 위한 복합 유도법칙을 제안한다. 제안하는 유도법칙은 비례 항법(proportional navigation)의 특성을 이용하는 것으로 총 두 단계의 유도 명령을 생성하게 된다. 첫 번째 유도명령은 초기 유도단계에서 표적에 대한 지향각(look angle)을 일정하게 유지하게 하고, 특정한 시선각 조건을 만족하면 두 번째 비례 항법 유도로 전환하여 원하는 충돌각으로 표적을 타격하게 된다. 충돌각 설정을 용이하게 하기 위하여 제한된 유도탄의 성능 조건을 가지고 달성 가능한 최대 충돌각 계산방법을 제시한다. 수치 시뮬레이션을 통해 설계된 유도법칙의 성능 및 실제 유도탄 환경에 대한 적용가능성을 분석한다.

• International Journal of Aeronautical and Space Sciences
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• 제11권2호
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• pp.131-135
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• 2010

We report on the design of a three-axis missile autopilot using multi-objective control synthesis via linear matrix inequality techniques. This autopilot design guarantees $H_2/H_{\infty}$ performance criteria for a set of finite linear models. These models are linearized at different aerodynamic roll angle conditions over the flight envelope to capture uncertainties that occur in the high-angle-of-attack regime. Simulation results are presented for different aerodynamic roll angle variations and show that the performance of the controller is very satisfactory.

• Maxillofacial Plastic and Reconstructive Surgery
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• 제16권3호
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• pp.390-395
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• 1994

The author evaluated the nasal asymmetry after primary operations in the patients with unilateral cleft lip using full face photographs. The results are as follows : 1. Nasal deviation angle is average 2.98+3.01 degree(ranged from 0 to 10 degree), significantly different from control group(p<0.05). 2. Nasal deviation angle is average 5.1% when inter-medial canthal distance is 100%, significantly different from control group(p<0.05). 3. Difference in nostril size between cleft and noncleft side is 2.1% when inter-medial canthal distance is 100%, significantly different from control group(p<0.05). 4. Nasal attractiveness analysis shows higher points in difference in nostril size, nasal deviation, nasal form in that order. 5. Nasal asymmetry after primary operations in the patients with unilateral cleft lip using full face photographs is related with Nasal deviation angle, Nasal deviation distance and Difference in nostril size between cleft and noncleft side.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2001년도 ICCAS
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• pp.152.1-152
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• 2001

This paper presents a high performance and cost effective way by using an FPGA circuit to implement torque controller so that the SRM can operate at high speed. In order to increase the operating speed, we need to implement both the torque and the current controllers by using an FPGA. However, it is difficult to implement all of the torque controller in the FPGA. Moreover, implementation of a time critical part is sufficient for improving the performance. One of the time critical part is the switching angle control. In this study, torque controller which calculate the switching on and commutation angles is implemented in PC because these angle are a function of rotor velocity which is varied slowly, and switching angle controller ...

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1999년도 제14차 학술회의논문집
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• pp.181-184
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• 1999

Leading vehicle states are useful and essential elements in adaptive cruise control (ACC) system, collision warning (CW) and collision avoidance (CA) system, and automated highway system (AHS). There are many approaches in ACC using Kalman filter. Mostly only distance to leading vehicle and velocity difference are estimated and used for the above systems. Applications in road vehicle in curved road need to obtain more informations such as yaw angle, steering angle which can be estimated using vision system. Since vision system is not robust to environment change, we used Kalman filter to estimate distance, velocity, yaw angle, and steering angle. Application to active tracking of target vehicle is shown.

• 한국자동차공학회논문집
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• 제20권2호
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• pp.15-20
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• 2012

This study is to propose and develop an integrated dynamics control system to improve and enhance the lateral stability and handling performance. To achieve this target, we integrate an AFS and a 4WS systems with a fuzzy logic controller. The IDCS determines active additional steering angle of front wheel and controls the steering angle of rear wheel. The results show that the IDCS improves the lateral stability and controllability on dry asphalt and snow paved road when double lane change and step steering inputs are applied. Yaw rate of the IDCS vehicle tracks reference yaw rate very well and body slip angle is reduced about by 50%. Response time of the IDCS vehicle is also decreased.

• Journal of Power Electronics
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• 제12권5호
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• pp.748-757
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• 2012

In a sensorless control system with a Permanent Magnet Synchronous Motor (PMSM), the angular position of the rotor flux can be estimated by a voltage equation. However, the estimated angle may be inaccurate due to various causes. In this paper, it was comprehensively analyzed how various causes affect the angle error. As a result of the analysis, an error equation intuitively describing these relationships was derived. The parameter errors of a PMSM and the non-ideal properties of the driving system were identified as error-causing factors. To demonstrate the validity of the error equation, PMSMs were tested at various operating points. The variations in angle errors could be well explained with the error equation.

• 한국기계가공학회지
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• 제21권5호
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• pp.22-27
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• 2022

An integrated front steering system and front brake system (FSFB) is developed to improve the stability and controllability of an SUV. The FSFB simultaneously controls the additional steering angle and front brake pressure. An active front steering system (AFS) and an active front brake system (AFB) are designed for comparison. The results show that the FSFB enhances the lateral stability and controllability regardless of road and running conditions compared to the AFS and AFB. As a result, the yaw rate of the SUV tracks the reference yaw rate, and the side slip angle decreases. In addition, brake pressure control is more effective than steering angle control in improving the stability and steerability of the SUV on a slippery road. However, this deteriorates comfort on dry or wet asphalt.

• 전력전자학회논문지
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• 제15권5호
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• pp.361-368
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• 2010

본 논문에서는 스테핑 전동기의 고속 위치제어기를 제안하였다. 제안된 위치제어기는 폐루프 및 오픈루프 제어모드를 모두 가지고 있으며, 위치 제어를 위해 직접 토크 각도를 제어하는 방식을 적용하였다. 제안된 스테핑 전동기의 위치제어기는 고속 운전상태에서 위치결정 오차를 감소시키기 위해 메모리에 속도에 따른 내장된 토크 각도와 PI 제어기를 통하여 토크각도를 결정하는 폐루프 제어모드로 동작한다. 제안된 폐루프 제어모드에서 메모리에 내장된 토크각도는 선행적으로 속도에 따른 전동기의 토크각도를 룩-업 테이블로 저장하여 제어량을 결정하게 되므로, 빠른 응답특성을 가지게 되며, 부하 및 관성에 따른 위치오차는 PI 제어기의 제어량에 의해 보상되어질 수 있다. 또한, 저속 운전상태와 정지상태에서는 3가지로 구분된 오픈루프 제어모드가 각각 잔여 위치오차를 보정하게 되며, 급속 정지상태에서의 다이나믹 브레이크 동작을 지원하게 된다. 제안된 위치제어기는 2상 스테핑 전동기의 실시험을 통하여 그 성능을 검증하였다.