• 시스템엔지니어링학술지
• /
• 제16권2호
• /
• pp.131-140
• /
• 2020

The characteristics of ballistic missiles are changing rapidly but studies have mostly focused on fragmentary flight trajectory analysis estimating the changing characteristics of some types, while there is a lack of research on comprehensive and efficient ballistic search, detection and prediction for missiles including the new types that have been gaining attention lately. This paper analyzes the flight trajectory characteristics of ballistic missiles at various ranges considering flight path angle adjustment, specific impulse and drag force with altitude based on the optimized equations of motion reflecting the parameters of North Korea's general and new types of ballistic missiles. The flight trajectory characteristics of representative ranges for each ballistic missile were analyzed by adjusting the flight path angle in the minimum energy method, lofted method, and depressed method. In addition, High value target can attacked by ballistic missiles considering flight path angle adjustment at various points. It's expected to be used to Threat Evaluation and Weapon Allocation, and deployment of defense systems by interpreting the analysis of the latest Iskander-class ballistic missiles and the new multiple rocket launcher.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 1992년도 한국자동제어학술회의논문집(국내학술편); KOEX, Seoul; 19-21 Oct. 1992
• /
• pp.686-691
• /
• 1992

Implicit guidance algorithm can deal with the trajectory error rapidly, but it has to save much data. If, however, the control variable is represented by a specific function form, a few parameters will suffice to define the control variable. In this paper, we study the method of updating the parameters of the control function for the reduction of trajectory errors. The method proposed here does not require much memory for guidance.

• Advances in aircraft and spacecraft science
• /
• 제9권5호
• /
• pp.401-414
• /
• 2022

In the present paper, the optimal selection of batteries for an electric pump-fed hybrid rocket engine is analyzed. A two-stage Mars Ascent Vehicle, suitable for the Mars Sample Return Mission, is considered as test case. A single engine is employed in the second stage, whereas the first stage uses a cluster of two engines. The initial mass of the launcher is equal to 500 kg and the same hybrid rocket engine is considered for both stages. Ragone plot-based correlations are embedded in the optimization process in order to chose the optimal values of specific energy and specific power, which minimize the battery mass ad hoc for the optimized engine design and ascent trajectory. Results show that a payload close to 100 kg is achievable considering the current commercial battery technology.

• 한국사회복지학
• /
• 제62권3호
• /
• pp.83-108
• /
• 2010

본 연구는 고령사회 준비를 위한 현황이해 차원에서 앤더슨 모형을 이용하여 노년기 외래의료 서비스 이용궤적 및 예측요인을 살펴보고, 초기노년기와 후기노년기 간에 궤적이나 예측요인이 차이가 있는지를 살펴보는 것을 목적으로 한다. 한국복지패널의 1, 2, 3차년도 자료를 사용하여, 궤적 및 예측 요인은 잠재성장모형을 이용해서 분석하였고 연령 차이는 다중집단분석을 이용하여 분석하였다. 60세 이상 노인들은 해가 지남에 따라서 외래이용 횟수를 증가시키는 경향을 보였는데, 75세 미만의 초기 노년기의 노인들이 75세 이상의 후기노년기의 노인들 보다가 이용 횟수를 상대적으로 빨리 증가시켰다. 예측요인에 있어서는 선행요인, 자원요인, 욕구요인들의 상당수가 궤적과 유의미한 관계가 있었는데, 자원요인 보다는 욕구요인들이 의료서비스 이용궤적에 크게 영향을 주는 것으로 나타났다. 하지만 예측요인에 있어서 초기 및 후기 노년기 사이에 큰 차이는 없었다. 결과를 토대로 연구의 의의 및 함의를 논의하였다.

• IEIE Transactions on Smart Processing and Computing
• /
• 제5권4호
• /
• pp.256-266
• /
• 2016

Concurrently detected and annotated abnormal events can have a significant impact on surveillance systems. By considering the specific domain of pedestrian trajectories, this paper presents two main contributions. First, as introduced in much of the work on trajectory-based anomaly detection in the literature, only information about pedestrian paths, such as direction and speed, is considered. Differing from previous work, this paper proposes a framework that deals with additional types of trajectory-based anomalies. These abnormal events take places when a person enters prohibited areas. Those restricted regions are constructed by an online learning algorithm that uses surrounding information, including detected pedestrians and background scenes. Second, a simple data-boosting technique is introduced to overcome a lack of training data; such a problem particularly challenges all previous work, owing to the significantly low frequency of abnormal events. This technique only requires normal trajectories and fundamental information about scenes to increase the amount of training data for both normal and abnormal trajectories. With the increased amount of training data, the conventional abnormal trajectory classifier is able to achieve better prediction accuracy without falling into the over-fitting problem caused by complex learning models. Finally, the proposed framework (which annotates tracks that enter prohibited areas) and a conventional abnormal trajectory detector (using the data-boosting technique) are integrated to form a united detector. Such a detector deals with different types of anomalous trajectories in a hierarchical order. The experimental results show that all proposed detectors can effectively detect anomalous trajectories in the test phase.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 1997년도 추계학술대회 논문집
• /
• pp.406-409
• /
• 1997

An economical 4-axis CNC controller employing step motors is designed and implemented in this paper. By using the inherent ability of holding position of the motor, the CNC controller uses open-loop control for removing trajectory error and for a simple hardware. Each drive of axis has an 8-bit microprocessor 89C52 and a PC controls the axes and pendant by means of RS232C serial communication. Backlash is also compensated at the axis controller. While compensating the backlash, the feed rate becomes zero in order to minimize trajectory error. The trajectories of 16ms interval are computed on PC and are sent to motor drives. In the drives, the trajectories are linearly interpolated for 2ms interval. The developed CNC does not require add-on specific motion card on PC. From the experimental results, the validity of the CNC controller based on step motor is proved.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 1990년도 한국자동제어학술회의논문집(국제학술편); KOEX, Seoul; 26-27 Oct. 1990
• /
• pp.990-995
• /
• 1990

A minimum-time trajectory planning for two robot arms with designated paths and coordination is proposed. The problem considered in this paper is a subproblem of hierarchically decomposed trajectory planning approach for multiple robots : i) path planning, ii) coordination planning, iii) velocity planning. In coordination planning stage, coordination space, a specific form of configuration space, is constructed to determine collision region and collision-free region, and a collision-free coordination curve (CFCC) passing collision-free region is selected. In velocity planning stage, normal dynamic equations of the robots, described by joint angles, velocities and accelerations, are converted into simpler forms which are described by traveling distance along collision-free coordination curve. By utilizing maximum allowable torques and joint velocity limits, admissible range of velocity and acceleration along CFCC is derived, and a minimum-time velocity planning is calculated in phase plane. Also the planning algorithm itself is converted to simple numerical iterative calculation form based on the concept of neural optimization network, which gives a feasible approximate solution to this planning problem. To show the usefulness of proposed method, an example of trajectory planning for 2 SCARA type robots in common workspace is illustrated.

• 대기
• /
• 제24권2호
• /
• pp.245-251
• /
• 2014

Statistical trajectory analysis has been widely used to identify potential source regions for chemically and radiatively important chemical species in the atmosphere. The most widely used method is a statistical source-receptor model developed by Stohl (1996), of which the underlying principle is that elevated concentrations at an observation site are proportionally related to both the average concentrations on a specific grid cell where the observed air mass has been passing over and the residence time staying over that grid cell. Thus, the method can compute a residence-time-weighted mean concentration for each grid cell by superimposing the back trajectory domain on the grid matrix. The concentration on a grid cell could be used as a proxy for potential source strength of corresponding species. This technical note describes the statistical trajectory approach and introduces its application to estimate potential source regions of $CO_2$ enhancements observed at Korean Global Atmosphere Watch Observatory in Anmyeon-do. Back trajectories are calculated using HYSPLIT 4 model based on wind fields provided by NCEP GDAS. The identified $CO_2$ potential source regions responsible for the pollution events observed at Anmyeon-do in 2010 were mainly Beijing area and the Northern China where Haerbin, Shenyang and Changchun mega cities are located. This is consistent with bottom-up emission information. In spite of inherent uncertainties of this method in estimating sharp spatial gradients within the vicinity of the emission hot spots, this study suggests that the statistical trajectory analysis can be a useful tool for identifying anthropogenic potential source regions for major GHGs.

• 전자공학회논문지B
• /
• 제30B권8호
• /
• pp.41-53
• /
• 1993

The tasks which detect and track moving objects, by analyzing dynamic images taken at a constant time interval, are essential in various applications. This paper suggests how to utilize domain-specific knowledge and motional knowledge for detecting and tracking moving objects. That is, The trajectory information of a moving object is to be used for generating hypotheses on expected motion and expected position of moving objects, and the domain-specific knowledge is to be used for verifying the generated hypotheses.

• 한국항공우주학회지
• /
• 제46권1호
• /
• pp.41-51
• /
• 2018

무장 헬리콥터에서 발사되는 무유도 로켓은 로터 블레이드에 의한 내리흐름과 전후좌우 기동으로 인한 외풍에 의해 전체 궤적 및 사거리가 변화하므로, 내리흐름 효과를 고려하여 무유도 로켓의 궤적을 예측하는 것이 중요하다. 내리흐름 효과를 고려한 무유도 로켓의 궤적 및 사거리를 예측하기 위해, 본 연구에서 여러 외풍 조건에 따른 후류 영역을 Actuator Disk Model(ADM)로 계산하고 6 자유도 (6 DOF) 운동 해석으로 무유도 로켓의 자세 및 전체 비행 궤적을 예측할 수 있는 알고리즘을 개발하였다. 개발된 알고리즘은 ADM 해석 결과를 6 자유도에 반영하여 다양한 초기 발사조건에서 무유도 로켓의 전체 궤적을 예측할 수 있고, 기존 Inflow model을 이용한 내리흐름 해석과는 다르게 동체와의 간섭효과를 고려하여 비교적 정확한 내리흐름 및 다양한 외풍 환경 조건으로 궤적을 예측 할 수 있다. 개발된 알고리즘을 이용하여, 내리흐름 효과에 의한 무유도 로켓의 자세 및 궤적 변화 메커니즘을 유효 받음각 변화와 기수 자세 안정성으로 규명하였다. 그리고 외풍으로 인해 변화하는 내리흐름 효과를 고려하여 무유도 로켓의 궤적변화와 사거리를 계산한 결과, 후방 외풍 시 최대 13% 사거리 증가를 보였다. 사거리 증가의 주요 요인으로 내리흐름 영역과 강도, 부차적 요인으로 외풍과 동체와의 간섭효과, 동압의 크기인 것을 밝혔다. 또한 사거리 변화량이 가장 큰 후방 외풍에서, 후방 외풍의 풍속이 증가함에 따라 로켓의 사거리가 증가하였다. 하지만 특정 후방 외풍 크기 이상에서 더 이상 로켓 사거리가 증가하지 않는 한계를 보였다.