• 방송공학회논문지
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• 제25권3호
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• pp.362-373
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• 2020

최근 자율 주행 자동차와 지능형 CCTV에 대한 관심이 높아지면서 효율적인 객체 검출의 중요성은 필수적인 요소이다. 본 논문의 기반이 되는 DPM(Deformable Part Models)은 객체에 대한 변형 가능한 부분의 혼합을 사용하여 가변적인 객체를 나타낼 수 있는 대표적인 검출기로 다양한 분야에서 많이 연구 되고 있다. 객체 모델의 파트 모양과 구성을 잡아내는 기법으로 높은 검출 성능을 보여주지만 복잡한 알고리즘으로 인해 실제 어플리케이션에서 사용하기에는 한계가 있다. 이를 개선하기 위해 본 논문에서는 DPM에서 많은 연산을 필요로 하는 이미지 특징 피라미드(feature pyramid)를 구성하는 과정 대신, 특정 스케일에서 구해진 소수의 특징(feature) 맵에 적응적인 쌍선형(bilinear) 보간법을 이용하여 이미지 특징 피라미드를 재구성해 연산 속도를 줄이는 방법을 제안한다. 모의실험 결과, 제안된 방식의 DPM은 기존 DPM 방식 대비 검출 성능은 2.82%가 낮아졌지만 평균 연산 시간 10%를 향상시킴을 알 수 있었다.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2002년도 가을 학술발표회 논문집
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• pp.70-77
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• 2002

Since our physical world cannot be modeled as rigid body, deformable object models are important. For real-time simulation of elastic object, it must be guaranteed by its exact solution and low-latency computational cost. In this paper, we describe the boundary integral equation formulation of linear elastic body and related boundary element method(BEM). The deformation of elastic body can be effectively solved with 1ow run-time computational costs, using precomputed Green Function and fast low-rank updates based on Capacitance Matrix Algorithm.

• Geomechanics and Engineering
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• 제21권1호
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• pp.53-62
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• 2020

Rheological processes in the rock mass for the stress-strain analysis are quite important when considering the construction of underground structures in soft rock masses, particularly in case of construction in several stages. In the analysis, it can be assumed that the reinforced concrete structure is slightly deformable in relation to the rock mass, and the rheological stress redistribution happens at the expense of the elements of rock mass. The basic elements of rheological models for certain types of rock mass and analysis of these models are presented in the first part of this paper. The second part is dedicated to the analysis of rheological processes in marl rock mass and the influence of these processes on the reinforced-concrete tunnel structure.

• Nuclear Engineering and Technology
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• 제52권2호
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• pp.381-396
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• 2020

Investigations of the commercial aircraft impact effect on nuclear island infrastructures have been drawing extensive attention, and this paper aims to perform the safety assessment of Generation III nuclear power plant (NPP) buildings subjected to typical commercial aircrafts crash. At present Part I, finite element (FE) models establishment and validations for both the aircrafts and NPP buildings are performed. (i) Airbus A320 and A380 aircrafts are selected as the representative medium and large commercial aircrafts, and the corresponding fine FE models including the skin, beam, fuel and etc. are established. By comparing the numerically derived impact force time-histories with the existing published literatures, the rationality of aircrafts models is verified. (ii) Fine FE model of the Chinese Zhejiang Sanao NPP buildings is established, including the detailed structures and reinforcing arrangement of both the containment and auxiliary buildings. (iii) By numerically reproducing the existing 1/7.5 scaled aircraft model impact tests on steel plate reinforced concrete (SC) panels and assessing the impact process and velocity time-history of aircraft model, as well as the damage and the maximum deflection of SC panels, the applicability of the existing three concrete constitutive models (i.e., K&C, Winfrith and CSC) are evaluated and the superiority of Winfrith model for SC panels under deformable missile impact is verified. The present work can provide beneficial reference for the integral aircraft crash analyses and structural damage assessment in the following two parts of this paper.

• Nuclear Engineering and Technology
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• 제53권9호
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• pp.3085-3099
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• 2021

Investigations of large commercial aircraft impact effect on nuclear power plant (NPP) buildings have been drawing extensive attentions, particularly after the 9/11 event, and this paper aims to numerically assess the damage and vibrations of NPP buildings subjected to aircrafts crash. In Part I of present paper, two shots of reduce-scaled model test of aircraft impact on NPP were conducted based on the large rocket sled loading test platform. In the present part, the numerical simulations of both scaled and prototype aircraft impact on NPP buildings are further performed by adopting the commercial program LS-DYNA. Firstly, the refined finite element (FE) models of both scaled aircraft and NPP models in Part I are established, and the model impact test is numerically simulated. The validities of the adopted numerical algorithm, constitutive model and the corresponding parameters are verified based on the experimental NPP model damages and accelerations. Then, the refined simulations of prototype A380 aircraft impact on a hypothetical NPP building are further carried out. It indicates that the NPP building can totally withstand the impact of A380 at a velocity of 150 m/s, while the accompanied intensive vibrations may still lead to different levels of damage on the nuclear related equipment. Referring to the guideline NEI07-13, a maximum acceleration contour is plotted and the shock damage propagation distances under aircraft impact are assessed, which indicates that the nuclear equipment located within 11.5 m from the impact point may endure malfunction. Finally, by respectively considering the rigid and deformable impacts mainly induced by aircraft engine and fuselage, an improved Riera function is proposed to predict the impact force of aircraft A380.

• Journal of Astronomy and Space Sciences
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• 제38권4호
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• pp.237-250
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• 2021

A rover is a planetary surface exploration device designed to move across the ground on a planet or a planetary-like body. Exploration rovers are increasingly becoming a vital part of the search for scientific evidence and discoveries on a planetary satellite of the Sun, such as the Moon or Mars. Reliable behavior and predictable locomotion of a rover is important. Understanding soil behavior and its interaction with rover wheels-the terramechanics-is of great importance in rover exploration performance. Up to now, many researchers have adopted Bekker's semiempirical model to predict rover wheelsoil interaction, which is based on the assumption that soil is deformable when a pressure is applied to it. Despite this basic assumption of the model, the pressure-sinkage relation is not fully understood, and it continues to present challenges for rover designers. This article presents a new pressure-sinkage model based on dimensional analysis (DA) and results of bevameter tests. DA was applied to the test results in order to propose a new pressure-sinkage model by reducing physical quantitative parameters. As part of the work, a new bevameter was designed and built so that it could be successfully used to obtain a proper pressure-sinkage relation of Korean Lunar Soil Simulant (KLS-1). The new pressure-sinkage model was constructed by using three different sizes of flat plate diameters of the bevameter. The newly proposed model was compared successfully with other models for validation purposes.

• 한국광학회지
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• 제33권4호
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• pp.167-176
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• 2022

적응 광학(adaptive optics, AO)은 대기 외란을 실시간으로 보정하는 기술을 말하고, 이러한 적응광학의 효율적 개발을 위하여, 다양한 성능 예측 기법을 도입하여 적응광학이 적용된 시스템 성능 예측을 실시한다. 적응광학의 성능 예측 기법으로 자주 사용되는 기법으로는 통계분석, 전산모사 및 광학 벤치 테스트가 있다. 통계분석에서는 적응광학 시스템을 통계 분석 모델로 가정하여 오차값(분산)의 제곱을 전부 합쳐 스트렐비를 간단하게 추정한다. 다만, 하위 변수 간의 상관 관계는 무시되어 이에 따른 추정의 오류는 존재한다. 다음으로, 전산모사는 대기 난류, 파면센서, 변형거울, 폐쇄 루프 등 모든 구성요소를 가능한 한 실제와 가깝게 모델링하고, 시간 흐름에 따른 적응광학 시스템의 변화를 모두 구현하여 성능 예측을 수행한다. 다만, 전산모사 모델과 현실 사이에는 여전히 일부 차이가 있어, 광학 벤치 테스트를 통하여 시스템 성능을 확인한다. 최근 국내에서 개발된 변형 거울을 적용한 1.6 m 지상 망원경용 적응광학 시스템을 개발 중에 있어, 이에 적용 가능한 적응광학 시스템을 통하여 성능 예측 기법이 요구되며 동시에 성능 예측 기법의 비교를 진행하고자 한다. 앞서 언급된 통계분석 및 전산모사를 이용하여 시스템 성능 예측을 수행하였으며, 성능 예측의 분석을 위해 각각의 성능 예측 기법의 망원경 및 적응광학 시스템 모델링 과정 및 결과를 제시하였다. 이때 성능 예측을 위한 대기 조건으로는 보현산 관측 중앙값(median)을 적용하였다. 그 결과 통계 분석 방법의 경우 평균 스트렐 비가 0.31이 도출됨을 확인하였고, 전산모사 방법의 경우 평균 스트렐 비가 0.32를 가짐을 확인함으로써 두 방법에 의한 예측이 거의 유사함을 확인할 수 있었다. 추가적으로, 전산모사의 경우 해석 결과의 신뢰성을 확보하기 위하여, 모사 시간이 대기 임계 시간 상수의 약 240배인 0.9초 이상 수행되어야 함을 알 수 있었다.