• 제목/요약/키워드: Trajectory Analysis

검색결과 955건 처리시간 0.035초

도로 네트워크에서 이동 객체를 위한 시공간 유사 궤적 검색 알고리즘 (Trajectory Search Algorithm for Spatio-temporal Similarity of Moving Objects on Road Network)

  • 김영창;라빈드라 비스타;장재우
    • 한국공간정보시스템학회 논문지
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    • 제9권1호
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    • pp.59-77
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    • 2007
  • 모바일 환경의 대중화와 이를 위한 기반 기술의 발전으로 인하여 이동 객체들을 효과적으로 표현하고 분석하는 것이 중요한 문제로 대두되고 있다. 이러한 환경에서 이동 객체 궤적의 유사성 검색은 궤적에 대한 데이터 마이닝의 일부분으로 중요한 연구 분야중의 하나이다. 본 논문에서는 도로 네트워크상의 이동 객체 궤적을 위한 시공간 유사 궤적 검색 알고리즘을 제안한다. 이를 위하여 도로 네트워크상에서 두 이동 객체 궤적 사이의 시공간 거리를 정의하고, 이를 기반으로 궤적 사이의 시공간 유사도 측정 방법을 제안한다. 유사 궤적 알고리즘은 효율적인 검색을 위하여 시그니쳐 파일 기법을 이용하여 궤적을 검색한다. 마지막으로, 본 논문에서 제안하는 시공간 유사 궤적 검색 알고리즘을 구현하고, 성능 분석을 통해 제안하는 알고리즘의 효율성을 입증한다.

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3차원 레이다 궤적 생성 및 성능 분석 (Performance Analysis of Three-Dimensional Radar for Angle and Distance Errors)

  • 임형용;장연수;이태우;황재덕;윤동원
    • 한국정보통신학회:학술대회논문집
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    • 한국정보통신학회 2014년도 추계학술대회
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    • pp.837-839
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    • 2014
  • 레이다 시스템에서 3차원 궤적 정보는 목표물 추적을 위해 필수적이다. 이때 3차원 레이다는 수신 신호를 통해 방위각, 고각 및 거리를 추정하여 3차원 궤적 정보를 얻게 된다. 수신 신호에 따라 추정된 각도들과 거리는 오차를 가지게 되며 이 오차의 정도에 따라 3차원 레이다 시스템의 성능에 미치는 영향에 대한 분석이 요구되어진다. 본 논문에서는 3차원 레이다 시스템의 각도 및 거리 오차에 따라 추정된 3차원 궤적 정보와 실제 궤적 정보에 대해 RMSE (Root Mean Square Error)를 통해 성능을 분석한다.

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Numerical Analysis of the Piston Secondary Dynamics in Reciprocating Compressors

  • Kim, Tae-Jong
    • Journal of Mechanical Science and Technology
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    • 제17권3호
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    • pp.350-356
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    • 2003
  • In this study, a numerical analysis for the piston secondary dynamics of small refrigeration reciprocating compressors is performed. In general, the length of cylinder in this class of compressors is shortened to diminish the frictional losses of the piston-cylinder system. So, the contacting length between piston and cylinder wall is in variable with the rotating crank angle around the BDC of the reciprocating piston. In the problem formulation of the piston dynamics, the variation in bearing length of the piston and all corresponding forces and moments are considered in order to determine the piston trajectory, velocity and acceleration at each step. A Newton-Raphson procedure was employed in solving the secondary dynamic equations of the piston. The developed computer program can be used to calculate the entire piston trajectory and the lubrication characteristics as functions of crank angle under compressor running conditions. The results explored the effects of some design parameters and operating conditions on the stability of the piston, the oil leakage, and friction tosses.

왕복동형 압축기 피스톤-실린더계의 동적 거동 및 윤활특성 해석 (Analysis of the Dynamic Behavior and Lubrication Characteristics of the Piston-Cylinder System in Reciprocating Compressors)

  • 김태종
    • Tribology and Lubricants
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    • 제18권4호
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    • pp.291-298
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    • 2002
  • In this study, a numerical analysis f3r the piston secondary dynamics and lubrication characteristics of small refrigeration reciprocating compressors is presented. In general, the length of cylinder in this class of compressors is shortened to diminish the frictional losses of the piston-cylinder system. So, the contacting length between piston and cylinder wall is in variable with the rotating crank angle around the BDC of the reciprocating piston. In the problem formulation of the piston dynamics, the change in bearing length of the piston and all corresponding forces and moments are considered in order to determine the piston trajectory, velocity and acceleration at each step. A Newton-Raphson procedure was employed in solving the secondary dynamic equations of the piston. The developed computer program can be used to calculate the entire piston trajectory and the hydrodynamic forces and moments as functions of crank angle under compressor running conditions. The results explored the effects of the radial clearance, lubricant viscosity, and pin location on the stability of the piston, the oil leakage, and friction losses.

영상처리기법을 이용한 무인전투기 와류 궤적 계측에 관한 연구 (A Study on the measurement for Vortex trajectory over an UCAV using image processing methods)

  • 고지훈
    • 한국항공우주학회지
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    • 제36권6호
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    • pp.594-599
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    • 2008
  • 현재 국방과학연구소 수동 시험에서 생성된 영상데이터는 수작업에 의해 분석되어지고 있다. 이러한 방법은 관측자에 따라 정확성과 분석소요시간이 상이할 수 있다 . 본 논문에서는 개선된 영상데이터 처리와 분석을 위해 MATLAB을 기반으로 한 알고리즘을 제안하였다. 이 알고리즘은 왜곡 보정 , 그레이 레벨 변환, 노이즈 제거, 이진화를 하는 영상 전처리 과정, 와류 궤적을 계측하는 영상 분석 과정으로 구성되어 있다 . 수동 시험에서 획득된 영상데이터를 이용하여 테스트 한 결과 제안된 알고리즘은 기존 영상데이터 분석 방법에 비해 정확성과 실행속도가 향상되었다.

낙하산을 갖는 단거리 발사체의 오차분석 (A Study on the Circular Error Probability of Short-Range Rocket with Parachute)

  • 김찬수;조요한
    • 한국군사과학기술학회지
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    • 제2권2호
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    • pp.218-225
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    • 1999
  • This paper contains the computational simulation of a free rocket with a parachute and the development of a firing table for each range. To obtain the trajectory of the rocket, 6 DOF model of rocket with parachute was generated and the wind tunnel test was done for the input parameters. Good agreement was obtained between the analysis of trajectory and the flight test result. Also the trajectory error analysis was performed by the Monte Carlo simulation. As a result of simulation, the CEP(Circular Error Probability) of the firing table was calculated.

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Dominant Synoptic Patterns Controlling PM10 Spatial Variabilities over the Korean Peninsula

  • Park, Hyo-Jin;Wie, Jieun;Moon, Byung-Kwon
    • 한국지구과학회지
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    • 제40권5호
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    • pp.476-486
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    • 2019
  • This study examines the controlling role of synoptic disturbances on $PM_{10}$ spring variability in the Korean Peninsula by using empirical orthogonal function (EOF) and back trajectory analyses. Three leading EOF modes are identified, and a lead-lag analysis suggests that $PM_{10}$ variabilities be closely related to the synoptic weather systems. The first EOF shows the spatially homogeneous distribution of $PM_{10}$, which is influenced by travelling anticyclonic disturbance with negative precipitation and descending motion. The second and third modes exhibit the dipole structures of $PM_{10}$, being associated with propagating cyclones. Furthermore, the back-trajectory analysis suggests that the transport of pollutants by anomalous winds associated with synoptic disturbances also contribute to the altered $PM_{10}$ concentration. Hence, a substantial synoptic control should be considered in order to fully understand the $PM_{10}$ spatiotemporal variability.

Analysis of Market Trajectory Data using k-NN

  • Park, So-Hyun;Ihm, Sun-Young;Park, Young-Ho
    • Journal of Multimedia Information System
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    • 제5권3호
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    • pp.195-200
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    • 2018
  • Recently, as the sensor and big data analysis technology have been developed, there have been a lot of researches that analyze the purchase-related data such as the trajectory information and the stay time. Such purchase-related data is usefully used for the purchase pattern prediction and the purchase time prediction. Because it is difficult to find periodic patterns in large-scale human data, it is necessary to look at actual data sets, find various feature patterns, and then apply a machine learning algorithm appropriate to the pattern and purpose. Although existing papers have been used to analyze data using various machine learning methods, there is a lack of statistical analysis such as finding feature patterns before applying the machine learning algorithm. Therefore, we analyze the purchasing data of Songjeong Maeil Market, which is a data gathering place, and finds some characteristic patterns through statistical data analysis. Based on the results of 1, we derive meaningful conclusions by applying the machine learning algorithm and present future research directions. Through the data analysis, it was confirmed that the number of visits was different according to the regional characteristics around Songjeong Maeil Market, and the distribution of time spent by consumers could be grasped.

MSAP을 이용한 F/A-18C로 부터 JDAM 분리 해석 (Application of MSAP to JDAM Separation from an F/A-18C Aircraft)

  • 이승수
    • 한국전산유체공학회지
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    • 제9권1호
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    • pp.41-47
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    • 2004
  • A successful store separation analysis tool, MSAP(Multi-body Separation Analysis Program) has been applied to F/A-18C/JDAM CFD Challenge Ⅱ. The challenge was devised to challenge CFD community to use CFD methodologies to predict and match the trajectory of a JDAM MK-84 separating from F/A-l8C. Trajectory simulations for two flight conditions were performed. Comparison between computed and measured flight trajectories for both conditions shows a good agreement.

과학연구용 로케트의 성능해석 (Performance analysis of the sounding rockets)

  • 류장수;김재수;박점주;오범석
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1989년도 한국자동제어학술회의논문집; Seoul, Korea; 27-28 Oct. 1989
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    • pp.76-81
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    • 1989
  • This paper represents the preliminary design process and the performance of the sounding rockets. At the design phase of the development, we selected rocket configuration according to results of aerodynamic weight and thrust analysis. And the payload-apogee performance of the rockets are determined with the variation of the launch angle and payload weight. Also the performance trajectory was calculated by a particle trajectory simulation. And the parameters which affect the system performance was analyzed.

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