• International Journal of Aeronautical and Space Sciences
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• 제10권1호
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• pp.112-121
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• 2009

This paper deals with supersonic air-breathing missile system. A supersonic air-breathing missile system has very complicated and incoherent thrust characteristics with respect to outer and inner environment during operation. For this reason, the missile system has many maneuver constraints and is allowed to operate within narrow flight envelope. In this paper, trajectory optimization of the missile is accomplished. The trajectory optimization problem is formulated as a discrete parameter optimization problem. For this formulation, Legendre Pseudo-Spectral method is introduced. This method is based on calculating the state and control variables on Legendre-Gauss-Lobatto (LGL) points. This approach helps to find approximated derivative and integration quantities simply. It is shown that, for this trajectory optimization, trend analysis is performed from thrust characteristics on various conditions so that the trajectory optimization is accomplished with fine initial guess with these results.

• Journal of Electrical Engineering and Technology
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• 제13권2호
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• pp.961-968
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• 2018

Recently, researches on automatic recognition of human activities have been actively carried out with the emergence of various intelligent systems. Since a large amount of visual data can be secured through Closed Circuit Television, it is required to recognize human behavior in a dynamic situation rather than a static situation. In this paper, we propose new intelligent human activity recognition model using the trajectory information extracted from the video sequence. The proposed model consists of three steps: segmentation and partitioning of trajectory step, feature extraction step, and behavioral learning step. First, the entire trajectory is fuzzy partitioned according to the motion characteristics, and then temporal features and spatial features are extracted. Using the extracted features, four pedestrian behaviors were modeled by decision tree learning algorithm and performance evaluation was performed. The experiments in this paper were conducted using Caviar data sets. Experimental results show that trajectory provides good activity recognition accuracy by extracting instantaneous property and distinctive regional property.

• 한국정보과학회논문지:컴퓨팅의 실제 및 레터
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• 제15권3호
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• pp.145-153
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• 2009

궤적(trajectory) 데이타는 실세계 어디에서든지 쉽게 찾아볼 수 있다. 최근 들어, 위성, 센서, RFID, 비디오 및 무선 통신 기술의 발전으로 말미암아 이동 객체를 체계적으로 추적하고, 많은 양의 궤적데이타를 수집할 수 있게 되었다. 이에 따라, 궤적 데이타의 분석에 대한 필요성이 점차 증대되고 있다. 본 논문에서는 대규모 궤적 데이타를 위한 마이닝 툴을 개발한다. 본 마이닝 툴에서는 가장 널리 사용되는 마이닝 연산인 집단화(clustering), 분류(classification), 이상치 발견(outlier detection)을 제공한다. 궤적 집단화는 공통적인 이동 패턴을 발견하며, 궤적 분류는 궤적에 기반하여 이동 객체의 범주를 예측하며, 궤적 이상치 발견은 나머지 궤적들과 크게 다르거나 일관적이지 않은 궤적을 발견한다. 본 마이닝 툴의 가장 큰 장점은 데이타 마이닝 도중에 부분 궤적 정보를 활용한다는 점이다. 본 마이닝 툴의 우수성은 다양한 실제 궤적 데이타 셋을 사용하여 입증되었다. 본 논문의 결과로 궤적 데이타 마이닝을 위한 실용적인 소프트웨어를 개발하였고 많은 실제 응용에 적용될 수 있을 것이라 사료된다.

• 한국군사과학기술학회지
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• 제21권5호
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• pp.572-582
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• 2018

In this paper, we have calculated a formular for sabot-trajectory of shipboard projectile including ship motion and generated trajectory-range function for analysing interference with structure of naval ship. We make formula to approximate the ship motion data of naval ship using optimization technique. Through this formula, we calculate the velocities and accelerations of sabot caused by ship motion(surge, sway, heave, roll, pitch, yaw) and then, we produce the formula about the trajectory of sabot including effects of ship motion in addition to previous study which had considered the effects of the pressure of flume, friction force, etc. To investigate interference with ship structures, we make the trajectory-range functions and then extract the nearest or farthest trajectory to ship structure. Through these data, we can conform whether the interference is happened or not.

• KSII Transactions on Internet and Information Systems (TIIS)
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• 제12권12호
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• pp.5782-5799
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• 2018

With the development of GPS and the popularity of mobile devices with positioning capability, collecting massive amounts of trajectory data is feasible and easy. The daily trajectories of moving objects convey a concise overview of their behaviors. Different social roles have different trajectory patterns. Therefore, we can identify users or groups based on similar trajectory patterns by mining implicit life patterns. However, most existing daily trajectories mining studies mainly focus on the spatial and temporal analysis of raw trajectory data but missing the essential semantic information or behaviors. In this paper, we propose a novel trajectory semantics calculation method to identify groups that have similar behaviors. In our model, we first propose a fast and efficient approach for stay regions extraction from daily trajectories, then generate semantic trajectories by enriching the stay regions with semantic labels. To measure the similarity between semantic trajectories, we design a semantic similarity measure model based on spatial and temporal similarity factor. Furthermore, a pruning strategy is proposed to lighten tedious calculations and comparisons. We have conducted extensive experiments on real trajectory dataset of Geolife project, and the experimental results show our proposed method is both effective and efficient.

• Journal of Astronomy and Space Sciences
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• 제27권3호
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• pp.195-204
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• 2010

The optimal Earth-Moon transfer trajectory considering spacecraft's visibility from the Daejeon ground station visibility at both the trans lunar injection (TLI) and lunar orbit insertion (LOI) maneuvers is designed. Both the TLI and LOI maneuvers are assumed to be impulsive thrust. As the successful execution of the TLI and LOI maneuvers are crucial factors among the various lunar mission parameters, it is necessary to design an optimal lunar transfer trajectory which guarantees the visibility from a specified ground station while executing these maneuvers. The optimal Earth-Moon transfer trajectory is simulated by modifying the Korean Lunar Mission Design Software using Impulsive high Thrust Engine (KLMDS-ITE) which is developed in previous studies. Four different mission scenarios are established and simulated to analyze the effects of the spacecraft's visibility considerations at the TLI and LOI maneuvers. As a result, it is found that the optimal Earth-Moon transfer trajectory, guaranteeing the spacecraft's visibility from Daejeon ground station at both the TLI and LOI maneuvers, can be designed with slight changes in total amount of delta-Vs. About 1% difference is observed with the optimal trajectory when none of the visibility condition is guaranteed, and about 0.04% with the visibility condition is only guaranteed at the time of TLI maneuver. The spacecraft's mass which can delivered to the Moon, when both visibility conditions are secured is shown to be about 534 kg with assumptions of KSLV-2's on-orbit mass about 2.6 tons. To minimize total mission delta-Vs, it is strongly recommended that visibility conditions at both the TLI and LOI maneuvers should be simultaneously implemented to the trajectory optimization algorithm.

• Journal of Astronomy and Space Sciences
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• 제34권4호
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• pp.331-342
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• 2017

To ensure the successful launch of the Korea pathfinder lunar orbiter (KPLO) mission, the Korea Aerospace Research Institute (KARI) is now performing extensive trajectory design and analysis studies. From the trajectory design perspective, it is crucial to prepare contingency trajectory options for the failure of the first lunar brake or the failure of the first lunar orbit insertion (LOI) maneuver. As part of the early phase trajectory design and analysis activities, the required time of flight (TOF) and associated delta-V magnitudes for each recovery maneuver (RM) to recover the KPLO mission trajectory are analyzed. There are two typical trajectory recovery options, direct recovery and low energy recovery. The current work is focused on the direct recovery option. Results indicate that a quicker execution of the first RM after the failure of the first LOI plays a significant role in saving the magnitudes of the RMs. Under the conditions of the extremely tight delta-V budget that is currently allocated for the KPLO mission, it is found that the recovery of the KPLO without altering the originally planned mission orbit (a 100 km circular orbit) cannot be achieved via direct recovery options. However, feasible recovery options are suggested within the boundaries of the currently planned delta-V budget. By changing the shape and orientation of the recovered final mission orbit, it is expected that the KPLO mission may partially pursue its scientific mission after successful recovery, though it will be limited.

• 스마트미디어저널
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• 제5권4호
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• pp.26-40
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• 2016

최근 모바일 기기가 발전함에 따라 사용자의 위치 수집 및 분석 방법에 대한 연구가 활발히 이루어지고 있다. 사용자의 위치분석 방법 중 궤적 데이터 마이닝은 사용자의 궤적을 바탕으로 의미 있는 정보를 추출하기 위해 사용된다. 궤적 데이터 마이닝을 수행하기 위해서는 사용자의 GPS 궤적을 분석하여 Stay Point를 추출하는 과정이 선행되어야 한다. 기존의 Stay Point 추출 알고리즘은 두 가지의 임계값이 필요하며 해당 임계값들은 사용자가 임의로 설정함으로써 알고리즘의 신뢰도가 떨어지고, 실내에서 머문 지점과 실외에서 머문지점에 대한 구분이 없기 때문에 Stay Point 위치의 모호성이 높아지는 문제점이 있다. 본 논문에서는 통계적 분석방법을 이용하여 SP를 추출하는 방법을 제안한다. 제안 알고리즘은 가우시안 확률분포를 사용하여 실내와 실외 SP를 각각 추출함으로써 SP 위치의 모호성을 개선하였다. 또한, 사용자가 임의로 설정하는 임계값이 없기 때문에 알고리즘의 신뢰도를 향상시켰다.

• 한국자동차공학회논문집
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• 제4권2호
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• pp.115-126
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• 1996

In order to obtain the principal design data for developing the Autonomous Robot Vehicle(ARV), Sensitivity analysis on the trajectory error and friction force with respect to the dynamic parameters is performed. In the straight motion, the trajectory error has been proved to be much affected by the mass variance of the ARV while the lateral friction force is much affected by the location of the mass center. In the curved motion, the effect of mass and moment of inertia is considered importantly. In addition, the lateral offset gives more effect than the geometric dimension of the ARV on the trajectory errors and friction force.

• 한국국방경영분석학회지
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• 제32권1호
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• pp.176-187
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• 2006

탄도미사일은 비행속도가 매우 빠르고 불안정한 하강운동에 기인하는 나선형과 같은 고유의 특이한 비행운동으로 인해 정확한 비행궤적의 추정이 어렵다. 이 논문은 탄도미사일의 비행궤적 특성에 대한 종합적인 해석을 기술한다. 최대사거리를 포함 다양한 미사일 비행사거리에 따른 비행궤적특성이 해석적 방법에 의해 도출되었다. 최대사거리를 줄여 발사했을 때 비행특성에 따른 위협이 급격히 증가됨을 해석적으로 나타냈다. 이 연구는 하층미사일방어체계 구축의 운용개념 설정에 대한 기반연구이다.