• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1990년도 한국자동제어학술회의논문집(국내학술편); KOEX, Seoul; 26-27 Oct. 1990
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• pp.252-257
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• 1990

For the position control of BL-DC motors, 2.phi.-3.phi. conversion unit, hysteresis band device, and PWM pulse generation are required. By utilizing a single-chip processor INTEL 8097BH, we cover all required functions. As a result, no analogue device is employed in this control scheme, so that it makes BL-DC motor controller simple and flexible. Furthermore, the single-chip processor is utilized for the nonlinear coordinate transformation which is necessary for the linearization of the motor system.

• 한국철도학회논문집
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• 제10권6호
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• pp.685-691
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• 2007

건설교통부는 2007. 1. 1 (2009.12. 신구좌표병행) 세계측지계 전면 시행 방침에 따라 철도측량의 내실화 그리고 기술력 제고를 위하여 호남고속철도건설 사업수행에 요구되는 수치지도를 항공측량을 통해 제작하였으며 이와 함께 철도기준점(GPS 정밀 3등기준점)측량을 실시, 보다 정밀한 철도 중심선형 좌표값 과 수준값을 획득할 수 있었다. 또한 국토지리정보원은 세계측지계 변환지침에 의거 국가좌표변환계수 및 왜곡량 모델을 고시하였다. 호남고속철도의 경우 좌표변환을 위해 공통기준점을 새로이 설치하지 않고 중심측량 및 종횡단측량을 위해 이미 구축된 철도기준점을 공통기준점으로 가정하여 변환을 실시하고자 한다. 따라서 본 논문은 남북축으로 계획된 호남고속철도 사례를 통해 현재의 계획노선을 선형 중심축으로 가정하고 철도기준점을 이용한 좌표변환을 실시후 결과에 대한 분석을 통해 변환가능성 여부를 판단하고자 한다. 좌표변환 실시 후 분석결과 Y축 왜곡량 값이 최소 21cm에서 최대 40cm까지 완만한 직선축으로 감소함을 확인할 수 있었고, X축은 $14cm\sim29cm$의 왜곡량을 보였으며 이러한 왜곡량을 보정한 결과 좌표간 편차량이 $6mm{\sim}9mm$로 국토지리정보원의 세계측지계 변환 지침에 따른 허용오차 및 지적경계측량 허용오차인 10cm를 만족시켰다. 이러한 결과는 철도기준점을 공통기준점(Common Point)으로 이용한 중심선형좌표 변환이 가능함을 설명할 수 있으며 동시에 공통점의 데이터, 좌표데이터, 수치지도의 변환도 허용오차범위내에서 변환이 가능하다.

• International Journal of Aeronautical and Space Sciences
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• 제13권4호
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• pp.484-490
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• 2012

This paper is devoted to investigate the feasibility of using a medium power ground-based laser to produce a torque on LEO satellites of various shapes. The laser intensity delivered to a satellite is calculated using a simple model of laser propagation in which a standard atmospheric condition and linear atmospheric interaction mechanism is assumed. The laser force is formulated using a geocentric equatorial system in which the Earth is an oblate spheroid. The torque is formulated for a cylindrical satellite, spherical satellites and for satellites of complex shape. The torque algorithm is implemented for some sun synchronous low Earth orbit cubesats. Based on satellites perigee height, the results demonstrate that laser torque affecting on a cubesat has a maximum value in the order of $10^{-9}$ which is comparable with that of solar radiation. However, it has a minimum value in the order of $10^{-10}$ which is comparable with that of gravity gradient. Moreover, the results clarify the dependency of the laser torque on the orbital eccentricity. As the orbit becomes more circular it will experience less torque. So, we can conclude that the ground based laser torque has a significant contribution on the low Earth orbit cubesats. It can be adjusted to obtain the required control torque and it can be used as an active attitude control system for cubesats.

• International Journal of Aeronautical and Space Sciences
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• 제16권1호
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• pp.77-88
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• 2015

The dynamics of relative motion in a perturbed orbital environment are exploited based on Gauss' and Cowell's variational equations. The inertial coordinate frame and relative coordinate frame (Hill frame) are used, and a linear high fidelity model is developed to describe the relative motion. This model takes into account the primary gravitational and atmospheric drag perturbations. Then, this model is used in the design of a navigation, guidance, and control system of a chaser vehicle to approach towards and to depart from a target vehicle in proximity operations. Relative navigation uses an extended Kalman filter based on this relative model to estimate the relative position/velocity of the chaser vehicle with respect to the target vehicle. This filter uses the range and angle measurements of the target relative to the chaser from a simulated LIDAR system. The corresponding measurement models, process noise matrix, and other filter parameters are provided. Numerical simulations are performed to assess the precision of this model with respect to the full nonlinear model. The analyses include the navigation errors and trajectory dispersions.

• 제어로봇시스템학회논문지
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• 제19권12호
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• pp.1145-1151
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• 2013

Kinematic modeling is a prerequisite for motion planning and the control of mobile robots. In this paper, we proposed a new method of kinematic modeling for a type of mobile robot based on differential motion transformation. The differential motion implies a small translation and rotation in three-dimensional space in a small time interval. Thus, transformation of the differential motion gives the velocity relationship, i.e., Jacobian between two coordinate frames. Since the theory of the differential motion transformation is well-developed, it is useful for the systematic velocity kinematic modeling of mobile robots. In order to show the validity for application of the differential motion transformation, we obtained velocity kinematic models for a type of exemplar mobile robot including spherical ballbots.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1990년도 추계학술대회 논문집 학회본부
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• pp.446-449
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• 1990

A Multi-Robot Control language (MRCL) is proposed to effectively control the multi-robot. MRCL has not only single-robot, command, but multi-robot command with multi-task OS, XINU. Concurrent motion, coordinate motion, and simple collision avoidance motion are implemented. This language is expected to act as a intelligent supporting tool for multi-robot system. To verify the effectiveness of the MRCL, a simple puzzle matching example is illustrated.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1999년도 하계학술대회 논문집 F
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• pp.2481-2483
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• 1999

This paper proposed the p-q-r coordinate system where the instantaneous active power p, and the two instantaneous reactive powers $q_{q}$, $q_{r}$ were defined. The three power components are linearly independent, so the compensation for the two instantaneous reactive powers leads to control the two components of the current space vector. With the theory, the neutral current of a three-phase four-wire system can be eliminated by only compensating the instantaneous reactive power using no energy storage element.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2003년도 신호처리소사이어티 추계학술대회 논문집
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• pp.195-198
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• 2003

Camera calibration is the method of finding the relationship between world coordinates and image coordinates with respect to camera coordinate. It is represented by PPM(Perspective Projection Mateix) compactly. And the PPM is effected by positions, intervals and distribution of control points. This paper presents to the relationship between PPMs and control points by experiment.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1996년도 춘계학술대회 논문집
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• pp.466-471
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• 1996

This work is concerned with the development of digital contouring controller formulti-axial servosystems. Digital optimal contouring controller is proposed to coordinate each of the controllers of multiple feed drives and specifically improve the controuring performance. The optimal control formulation includes the contour error explicity in the performance index to be minimized. The contouring control is exercised for straight line and circular contours. Substantial improvement in contouring perfomance is obtained for a range of contouring conditions. Both steady state and transient error measures have been considered. The simulation study presented has estiblished the potential of the proposed controller to improve contourning perfomance.

• 대한전기학회논문지
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• 제36권4호
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• pp.301-304
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• 1987

The Optimal Control Problems for the singular system with the Generalized state space model are considered. It is shown that when the system is singular, the dimension can be reduced by coordinate transformation and the equivalent nonsingular system is got. After we have nonsingular system, the solution for the optimal control problem can be got by Riccati equation.