• Journal of Electrical Engineering and information Science
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• 제1권2호
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• pp.77-86
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• 1996

In this paper we deal with the problem of recovering 3-D motion and structure from a time-varying 2-D velocity vector field. A great deal has been done on this topic, most of which has concentrated on finding necessary and sufficient conditions for there to be a unique 3-D solution corresponding to a given 2-D motion. While previous work provides useful theoretical insight, in most situations the known algorithms have turned out to be too sensitive to be of much practical use. It appears that any robust algorithm must improve the 3-D solutions over time. As a step toward such algorithm, we present a method for recovering 3-D motion and structure from a given time-varying 2-D velocity vector field. The surface of the object in the scene is assumed to be locally planar. It is also assumed that 3-D velocity vectors are piecewise constant over three consecutive frames (or two snapshots of flow field). Our formulation relates 3-D motion and object geometry with the optical flow vector as well as its spatial and temporal derivatives. The linearization parameters, or equivalently, the first-order flow approximation (in space and time) is sufficient to recover rigid body motion and local surface structure from the local instantaneous flow field. We also demonstrate, through a sensitivity analysis carried out for synthetic and natural motions in space, that 3-D motion can be recovered reliably.

• Wind and Structures
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• 제38권3호
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• pp.161-170
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• 2024

In recent years, there have been an increasing number of experimental studies showing the need to include robustness criteria in the design process to develop complex active control designs for practical implementation. The paper investigates the crosswind aerodynamic parameters after the blocking phase of a two-dimensional square cross-section structure by measuring the response in wind tunnel tests under light wind flow conditions. To improve the accuracy of the results, the interpolation of the experimental curves in the time domain and the analytical responses were numerically optimized to finalize the results. Due to this combined effect, the three aerodynamic parameters decrease with increasing wind speed and asymptotically affect the upper branch constants. This means that the aerodynamic parameters along the density distribution are minimal. Taylor series are utilized to describe the fuzzy nonlinear plant and derive the stability analysis using polynomial function for analyzing the aerodynamic parameters and numerical simulations. Due to it will yield intricate terms to ensure stability criterion, therefore we aim to avoid kinds issues by proposing a polynomial homogeneous framework and utilizing Euler's functions for homogeneous systems. Finally, we solve the problem of stabilization under the consideration by SOS (sum of squares) and assign its fuzzy controller based on the feasibility of demonstration of a nonlinear system as an example.

• International Journal of Aeronautical and Space Sciences
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• 제15권4호
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• pp.356-365
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• 2014

This paper is the second in a series and aims to build a high-fidelity mathematical model for a propeller-driven airplane using the propeller's aerodynamics and inertial models, as developed in the first paper. It focuses on aerodynamic models for the fuselage, the main wing, and the stabilizers under the influence of the wake trailed from the propeller. For this, application of the vortex lattice method is proposed to reflect the propeller's wake effect on those aerodynamic surfaces. By considering the maneuvering flight states and the flow field generated by the propeller wake, the induced velocity at any point on the aerodynamic surfaces can be computed for general flight conditions. Thus, strip theory is well suited to predict the distribution of air loads over wing components and the viscous flow effect can be duly considered using the 2D aerodynamic coefficients for the airfoils used in each wing. These approaches are implemented in building a high-fidelity mathematical model for a propeller-driven airplane. Flight dynamic analysis modules for the trim, linearization, and simulation analyses were developed using the proposed techniques. The flight test results for a series of maneuvering flights with a scaled model were used for comparison with those obtained using the flight dynamics analysis modules to validate the usefulness of the present approaches. The resulting good correlations between the two data sets demonstrate that the flight characteristics of the propeller-driven airplane can be analyzed effectively through the integrated framework with the propeller and airframe aerodynamic models proposed in this study.

• 한국정보통신학회논문지
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• 제16권1호
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• pp.48-58
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• 2012

본 논문에서는 다중 대역 전송 시스템에서 광대역 전력 증폭기의 선형화를 위한 새로운 전치왜곡 기법을 제안한다. 특히, 한 시스템에서 동시에 다중대역/다중모드 신호를 전송함에 있어 다중대역 신호가 하나의 전력 증폭기에 의해 증폭되어 전송되는 시스템을 고려한다. 상호 대역 간 비선형 왜곡을 포함한 비선형 특성을 보상하기 위하여, 본 논문에서는 다중 전치왜곡기 블록을 갖는 새로운 전치왜곡 구조를 제안하며, 다중 전치왜곡기의 계수를 동시에 갱신하는 적응 알고리즘을 제안한다. 제안하는 다중 대역 모델을 검증하기 위하여 상용 증폭기를 사용하여 증폭기 모델을 추출하였으며, 추출된 모델을 기반으로 제안한 알고리즘을 모의실험을 통해 검증하였다. 모의실험 결과는 제안 알고리즘이 효과적으로 다중 전치왜곡기의 계수를 구할 수 있으며, 다중 대역을 효과적으로 선형화 할 수 있음을 보여준다.

• Earthquakes and Structures
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• 제3권6호
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• pp.821-838
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• 2012

This paper proposes a new three-layer pillar-type hysteretic damper system for residential houses. The proposed vibration control system has braces, upper and lower frames and a damper unit including hysteretic dampers. The proposed vibration control system supplements the weaknesses of the previously proposed post-tensioning vibration control system in the damping efficiency and cumbersomeness of introducing a post-tension. The structural variables employed in the damper design are the stiffness ratio ${\kappa}$, the ductility ratio ${\mu}_a$, and the ratio ${\beta}$ of the damper's shear force to the maximum resistance. The hysteretic dampers are designed so that they exhibit the targeted damping capacity at a specified response amplitude. Element tests of hysteretic dampers are carried out to examine the mechanical property and to compare its restoring-force characteristic with that of the analytical model. Analytical studies using an equivalent linearization method and time-history response analysis are performed to investigate the damping performance of the proposed vibration control system. Free vibration tests using a full-scale model are conducted in order to verify the damping capacity and reliability of the proposed vibration control system. In this paper, the damping capacity of the proposed system is estimated by the logarithmic decrement method for the response amplitudes. The accuracy of the analytical models is evaluated through the comparison of the test results with those of analytical studies.

• 한국전자통신학회논문지
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• 제15권2호
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• pp.237-244
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• 2020

본 논문은 2차원 공간에서 SLAM(: Simultaneous Localization and Mapping)의 구현을 설명한다. 본 논문에서 사용한 방법은 불변량이라고 하는 변수가 일정하게 유지 될 때 변환된 변수가 선형 공간을 구성하도록 상태 변수와 측정 변수를 변환하는 IEKF(: Invariant extended Kalman filter)를 사용한다. 따라서, IEKF는 불변량이 일정하게 유지되는 경우 수렴을 보장한다. 제안된 IEKF 접근법 중 변환을 하는 과정에서는 리군(Lie group) 행렬을 사용한다. 이 방법은 시뮬레이션을 통해 테스트 되었으며 결과는 선형 칼만 필터의 경우와 마찬가지로 칼만 이득이 일정하다는 것을 보여준다. 즉, 시뮬레이션 결과 이동체의 추정된 위치와 검출된 물체들 사이의 일관성을 보였다.

• 한국추진공학회지
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• 제19권3호
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• pp.54-64
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• 2015

본 논문에서는 DACS(Divert and Attitude Control System)를 장착한 KV(kill vehicle)의 비선형 가속도 조종루프 설계에 대해서 다룬다. ACS(Attitude Control System)는 받음각을 0으로 유지시키는 추력을 유발시키며, 받음각 제어를 위해 ACS를 제어명령으로 사용하는 궤환선형화 기반 비선형 받음각 조종루프를 제안한다. 받음각이 0인 조건에서는 비행경로각과 자세각이 일치하기 때문에 DCS(Divert Control System)는 유도루프에서 요구하는 측방향 가속도를 직접 생성하도록 제어한다. 이러한 방식에서는 추력에 의한 공력간섭 효과를 최소화 시킬 수 있으며, DCS와 ACS의 운용로직을 단순화 시킬 수 있다. 수치 시뮬레이션을 통해 제안한 기법의 성능을 검증한다.

• Earthquakes and Structures
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• 제4권4호
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• pp.397-428
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• 2013

This paper examines whether the "effective period" of bilinear isolation systems, as defined invariably in most current design codes, expresses in reality the period of vibration that appears in the horizontal axis of the design response spectrum. Starting with the free vibration response, the study proceeds with a comprehensive parametric analysis of the forced vibration response of a wide collection of bilinear isolation systems subjected to pulse and seismic excitations. The study employs Fourier and Wavelet analysis together with a powerful time domain identification method for linear systems known as the Prediction Error Method. When the response history of the bilinear system exhibits a coherent oscillatory trace with a narrow frequency band as in the case of free vibration or forced vibration response from most pulselike excitations, the paper shows that the "effective period" = $T_{eff}$ of the bilinear isolation system is a dependable estimate of its vibration period; nevertheless, the period associated with the second slope of the bilinear system = $T_2$ is an even better approximation regardless the value of the dimensionless strength,$Q/(K_2u_y)=1/{\alpha}-1$, of the system. As the frequency content of the excitation widens and the intensity of the acceleration response history fluctuates more randomly, the paper reveals that the computed vibration period of the systems exhibits appreciably scattering from the computed mean value. This suggests that for several earthquake excitations the mild nonlinearities of the bilinear isolation system dominate the response and the expectation of the design codes to identify a "linear" vibration period has a marginal engineering merit.

• 한국ITS학회 논문지
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• 제8권2호
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• pp.75-82
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• 2009

본 논문에서는 Doherty 전력 증폭기의 선형성을 증가시키는 mechanism을 이용하여 선형성을 증가시키고, 선형성 개선으로 인한 효율 감소를 보상할 수 있는 방법을 제안하였다. 또한 이를 검증하기 위하여 제안된 방법으로 20W급 전력 증폭기를 설계 및 제작하였다. 제작된 class-F를 이용한 3-way 증폭기는 2-way 증폭기보다 선형성이 약 10dBc개선되었으며, 효율은 1.5% 가량 개선되었다. 또한 3-way 증폭기와 비교하였을 때, 선형 특성은 비슷하였으나, 효율 특성은 약 3.5% 개선되었다. 본 논문에서 제안한 F급 바이어스를 이용한 3-way Doherty 전력 증폭기는 선형성 및 효율 향상에 적합함을 확인할 수 있으며, 향후 다양한 무선 통신 시스템의 전력 증폭기에 적용되리라 기대한다.

• 대한토목학회논문집
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• 제6권2호
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• pp.85-91
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• 1986

심해나 해상조건이 나쁜 지점에서 운영될 해양구조물의 설계시에는 파랑하중에 대한 구조물의 피로수명예측이 매우 중요하다. 본 논문에서는 랜덤파랑하중에 의해 해양구조물에 발생되는 응력의 bandwidth가 구조물의 피로수명예측 결과에 주는 영향에 대하여 연구하였다. 구조물의 동적거동해석은 비선형 점성저항력의 선형화를 통한 주파수영역해법을 사용하여 수행되었으며, 랜덤응력스펙트럼을 구하고 이를 바탕으로 피로해석을 수행하였다. 피로손상의 예측을 위한 랜덤응력 cycle의 산정은 narrow band cycle 산정법과 함께 wide band process 에 대하여 더 적정한 rainflow cycle 산정법을 사용하였다. 수심이 다른 지점에 위치한 2개의 구조물을 택하여 예제해석을 수행하였으며, 두 응력 cycle 산정법에 의해 얻은 피로해석 결과들을 비교하고 응력의 bandwidth의 영향을 분석하였다.