• 한국ITS학회 논문지
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• 제18권2호
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• pp.29-43
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• 2019

미시적 교통류 모형의 정산은 시뮬레이션 분석에 있어 매우 중요한 요소이다. 유전자 알고리즘은 교통류 모형의 정산에 널리 활용되어 왔으며, 일반적으로 이러한 최적화 문제에 있어 높은 효율성을 보이는 것으로 알려져 있다. 하지만 제한된 시간내에 신속한 의사결정을 위한 시뮬레이션 분석에 있어 유전자알고리즘의 모형 정산속도는 여전히 느리다. 이에 본 연구에서는 정산 효율 향상을 위해 중심합성계획법 기반의 이중유전자알고리즘을 활용한 차량추종모형 정산방법론을 개발하였다. 개발된 정산 방법론에서는 실험계획법 중 하나인 중심합성계획법과 유전자알고리즘을 결합하여 준최적해를 찾고, 이를 다시 유전자알고리즘의 초기 값으로 하여 모형 파라미터의 최적해를 찾는다. 개발된 방법을 활용하여 Gipps의 차량추종모형을 정산하였다. 선행연구에서 사용된 단일 유전자알고리즘을 활용한 방법과 비교한 결과, 본 연구에서 개발한 방법이 더 짧은 시간내에 최적해를 찾는 것으로 확인되었다. 개발된 방법론은 유전자알고리즘을 사용하는 다양한 교통분석에 활용될 수 있을 것으로 기대된다.

• ETRI Journal
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• 제42권4호
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• pp.619-632
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• 2020

Highly dispersive S-boxes are desirable in cryptosystems as nonlinear confusion sublayers for resisting modern attacks. For a near optimal cryptosystem resistant to modern cryptanalysis, a highly nonlinear and low differential probability (DP) value is required. We propose a method based on a piecewise linear chaotic map (PWLCM) with optimization conditions. Thus, the linear propagation of information in a cryptosystem appearing as a high DP during differential cryptanalysis of an S-box is minimized. While mapping from the chaotic trajectory to integer domain, a randomness test is performed that justifies the nonlinear behavior of the highly dispersive and nonlinear chaotic S-box. The proposed scheme is vetted using well-established cryptographic performance criteria. The proposed S-box meets the cryptographic performance criteria and further minimizes the differential propagation justified by the low DP value. The suitability of the proposed S-box is also tested using an image encryption algorithm. Results show that the proposed S-box as a confusion component entails a high level of security and improves resistance against all known attacks.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1991년도 한국자동제어학술회의논문집(국제학술편); KOEX, Seoul; 22-24 Oct. 1991
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• pp.1664-1670
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• 1991

For kinematically redundant manipulators, conventional dynamic control methods of local torque optimization showed the instability which resulted in physically unachievable torque requirements. In order to guarantee stability of the null space vector method which resolves redundancy at the acceleration level, Maciejewski[1] analyzed the kinetic behavior of homogeneous solution component and proposed the condition to identify regions of stability and instability for this method. 'In this paper, a modified null space vector method is first presented based on the Maciejewski's condition which is a function of a manipulator's configuration. Secondly, a new control method which is based on the concept of aspects is proposed. It was shown by computer simulations that the modified null space vector method and the proposed method have a common property that a preferred aspect is preserved during the execution of a task. It was also illustrated that both methods demonstrate a drastic reduction of torque loadings at the joints in the tracking motion of a long trajectory when compared with the null space vector method, and thus guarantee the stability of joint torque.

• 한국전산구조공학회논문집
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• 제22권3호
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• pp.251-258
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• 2009

개념설계단계에서 전투차량은 크게 화력성능, 기동성능과 체계의 물리적 특성으로 나누어진다. 본 연구에서는 전투차량체계를 구성하는 3가지 특성 중 화력성능의 최적화로 제한한다. 체계의 개념설계 단계에서 화력성능에 영향을 미치는 주요 인자로 파괴효과에 직접적인 영향을 주는 탄의 중량과 원거리 사격을 고려한 최대사거리를 분석대상으로 선정하였다. 최대 사거리 분석을 위하여 강내탄도와 강외탄도해석은 질량 집중 모델, Le Duc모델과 질점탄도모델을 사용하여 분석하였다. 실험계획법과 회귀분석으로 반응표면식을 구성하고 선정된 인자를 반응표면법으로 최적화하였다.

• Nuclear Engineering and Technology
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• 제52권8호
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• pp.1817-1825
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• 2020

Background: Cosmic ray-induced particles can lead to failure of semiconductors packaged for export during air transport. This work performed MCNP 6.2 simulations to optimize shielding against neutrons and protons induced by cosmic radiation Methods and materials: The energy spectra of protons and neutrons by incident angle at the flight altitude were determined using atmospheric cuboid model. Various candidates for the shielding materials and the geometry of the Unit Load Device Container were evaluated to determine the conditions that allow optimal shielding at all sides of the container. Results: It was found that neutrons and protons, at the flight altitude, generally travel with a downward trajectory especially for the particles with high energy. This indicated that the largest number of particles struck the top of the container. Furthermore, the simulation results showed that, among the materials tested, borated polyethylene and stainless steel were the most optimal shielding materials. The optimal shielding structure was also determined with the weight limit of the container in consideration. Conclusions: Under the determined optimal shielding conditions, a significantly reduced number of neutrons and protons reach the contents inside the container, which ultimately reduces the possibility of semiconductor failure during air transport.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2001년도 합동 추계학술대회 논문집 정보 및 제어부문
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• pp.311-314
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• 2001

The objectives of this paper include the development of an agile prototype of SFFS, the $CAFL^{VM}$(Computer Aided fabrication of Lamination for Various Material), which is suitable for the multi-item and small-quantity production and various material fabrication. This paper includes remodeling of the layer slices for the 2D cutting, supplementing information of the layer slices and developing process conditions to fabricate products of various shape. And also includes developing control hardware as well as software by enhancing BOF of the manipulator to 3 degree for the precise 2D cutting. It will generate optimal layer trajectory considering the dynamic characteristics of the laser beam. The system can be used as a competitive agile protype system in terms of various materials, fabrication speed, and accuracy by CAD modeling precise layer slicing, material development, robot path control, and optimization of the support structure.

• 제어로봇시스템학회논문지
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• 제20권1호
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• pp.6-11
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• 2014

Repetitive control is a specialized control scheme to track and/or attenuate a periodic reference trajectory and/or disturbance. Most researches about repetitive control have been performed in the frequency domain. Recently, several approaches to deal with repetitive control systems in the state space are developed by representing a q filter as a state-space equation. This paper presents a design method of a repetitive control system in the state space to satisfy $H_{\infty}$ performance. The overall system is composed of a plant, a repetitive controller, and a state-feedback controller, which can be converted to a standard form used in $H_{\infty}$ control. A LMI (Linear Matrix Inequality)-based stability condition is derived for fixed state-feedback gains. Under a given q filter, another LMI condition is derived to improve $H_{\infty}$ performance and is employed to find state-feedback gains by solving an optimization problem. Finally, to verify the feasibility of the proposed method, a numerical example is demonstrated.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 추계학술대회논문집A
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• pp.659-664
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• 2000

Fuel-consumption and catalyst-out emissions of a parallel hybrid electric vehicle are affected by operating region of an engine. In many researches, It is generally known that it is profitable in fuel- consumption to operate engine in OOL(Optimal Operating Line). We established the mathematical model of a parallel hybrid electric vehicle, which is linear time-invariant. To operate an engine in OOL, we applied RHC(Receding Horizon Control) to the driving control of a parallel hybrid electric vehicle. And it is known that the RHC has advantages such as good tracking performance under state and control constraints. This RHC is obtained by using linear matrix inequality (LMI) optimization. In this paper, there are three main topics. First, without state and control constraints, the optimal tracking of OOL was simulated. Second, with state and control constraints by engine and motor performances, the optimal tracking of OOL was simulated. In the last, we studied on the optimal gear ratio. That is to say, we combined the RHC and the iterative simulation to extract the optimal gear ratio. In this simulation, the vehicle is commanded to track the reference vehicle trajectory and the engine is operated in the optimal operating region which is made by the state constraints.

• 한국항공우주학회지
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• 제44권7호
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• pp.620-628
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• 2016

호모토피 알고리즘은 비선형성이 강하거나 다수의 최적해가 존재하는 비선형 최적제어 문제에서 점진적으로 비선형 항으로 고려하게 해줌으로써 강건하게 전역의 최적해를 구할 수 있는 방법이다. 본 논문에서는 초기 추정치에 둔감한 SBS 알고리즘과 호모토피 알고리즘을 결합한 비선형 최적제어 알고리즘을 제시하였다. 이러한 접근방식은 저추력 궤적최적화 문제와 같이 비선형성이 강한 문제의 최적해를 구하는데 효과적이다. 또한, 비선형성이 강한 문제들은 종종 다수 국소 해가 존재하게 되는데, 이러한 경우에 SBS-호모토피 방법은 점진적으로 전역해를 찾는 것을 가능하게 한다.

• 한국항공우주학회지
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• 제48권8호
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• pp.573-580
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• 2020

다중개체를 제어하기 위해서 해결해야 되는 문제들 중 하나는 위치제어다. 위치와 속도를 제어하기 위한 모델로 augmented Cucker-Smale 모델이 존재했다. 하지만 기존 모델은 모든 개체에 동일한 시스템을 적용함에 따라서 개별개체의 특성을 살리지 못했다는 특징이 있다. 본 논문에서는 그 점을 보안하고 적절한 형태로 변형하기 위해서 초기 위치와 분포를 이용한 마할라노비스 거리를 계수와 통계학적 자유도를 적용해서, 모델의 수렴시간과 소모에너지를 동시에 줄이고자 한다. 모델의 성능 검증을 위해서 몬테카를로 시뮬레이션을 통해서 전체적인 경향성을 판단했고, 추가적으로 개별 개체의 움직임을 분석하여서 마할라노비스 거리 계수가 적절한 역할을 수행하고 있는지 확인했다.