• 대기
• /
• 제23권1호
• /
• pp.93-102
• /
• 2013

Atmospheric transport pathway of an air mass is an important constraint controlling the chemical properties of the air mass observed at a designated location. Such information could be utilized for understanding observed temporal variabilities in atmospheric concentrations of long-lived chemical compounds, of which sinks and/or sources are related particularly with natural and/or anthropogenic processes in the surface, and as well as for performing inversions to constrain the fluxes of such compounds. The Lagrangian particle dispersion model FLEXPART provides a useful tool for estimating detailed particle dispersion during atmospheric transport, a significant improvement over traditional "single-line" trajectory models that have been widely used. However, those without a modeling background seeking to create simple back-trajectory maps may find it challenging to optimize FLEXPART for their needs. In this study, we explain how to set up, operate, and optimize FLEXPART for back-trajectory analysis, and also provide automatization programs based on the open-source R language. Discussions include setting up an "AVAILABLE" file (directory of input meteorological fields stored on the computer), creating C-shell scripts for initiating FLEXPART runs and storing the output in directories designated by date, as wells as processing the FLEXPART output to create figures for a back-trajectory "footprint" (potential emission sensitivity within the boundary layer). Step by step instructions are explained for an example case of calculating back trajectories derived for Anmyeon-do, Korea for January 2011. One application is also demonstrated in interpreting observed variabilities in atmospheric $CO_2$ concentration at Anmyeon-do during this period. Back-trajectory modeling information introduced in this study should facilitate the creation and automation of most common back-trajectory calculation needs in atmospheric research.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 1996년도 Proceedings of the Korea Automatic Control Conference, 11th (KACC); Pohang, Korea; 24-26 Oct. 1996
• /
• pp.307-310
• /
• 1996

In this paper, we deal with some numerical analyses of a re-entry vehicle in a 2-dimensional plane as an optimal control problem. To reduce the dynamic load, the heat load and the oscillation in the trajectory, we researched the trajectories in which the load factor or the rate of flight path angle was minimized during re-entry. In addition to that, taking advantage of the monotonous subarc method and the folded time-axis method, we tried to find the heat-less and load-less trajectory with combinations of some sectional functionals so that we can achieve more comfortability.

• 한국정밀공학회지
• /
• 제14권3호
• /
• pp.137-146
• /
• 1997

External linkage type spine motion analysis was developed for relative trunk motion respect to the pelvis. A special programs for calculation of the relative angular motion and for graphical display were also developed. The developed device assured its accuracy and conveniency after application to 15 normal vol- unteers. Compare to the normal subjects, 18 patients treated with fixations and decompression surgery showed relatively large coupling motion. Optimal trajectory of the trunk motion derived from mathematical model in flexion and extension matched well with measurement for normal subjects.

• 한국산업융합학회 논문집
• /
• 제21권3호
• /
• pp.125-131
• /
• 2018

In this paper, we propose a homogeneous multisensor-based navigation algorithm for a mobile robot, which is intelligently searching the goal location in unknown dynamic environments with moving obstacles using multi-ultrasonic sensor. Instead of using "sensor fusion" method which generates the trajectory of a robot based upon the environment model and sensory data, "command fusion" method by fuzzy inference is used to govern the robot motions. The major factors for robot navigation are represented as a cost function. Using the data of the robot states and the environment, the weight value of each factor using fuzzy inference is determined for an optimal trajectory in dynamic environments. For the evaluation of the proposed algorithm, we performed simulations in PC as well as real experiments with mobile robot, AmigoBot. The results show that the proposed algorithm is apt to identify obstacles in unknown environments to guide the robot to the goal location safely.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 2001년도 ICCAS
• /
• pp.125.2-125
• /
• 2001

Inertial navigation error is the major source of miss distance when only the inertial navigation system is used for guidance, and tend to monotonically increase if the flight time is small compared to the Schuler period. Miss distance due to these inertial navigation errors, therefore, can be minimized when a missile has the minimum time trajectory. Moreover, vertical component of navigation error becomes null if he impact angle to a surface target approaches to 90 degrees. In this paper, the minimum time trajectories with the steep terminal impact angle constraint are obtained by using CFSQP 2.5, and their properties are analyzed to give a guideline for he construction of an effective guidance algorithm for short range tactical surface-to-surface missiles.

• KSII Transactions on Internet and Information Systems (TIIS)
• /
• 제6권12호
• /
• pp.3197-3218
• /
• 2012

Compared with traditional itinerary planning, intention-oriented itinerary recommendations can provide more flexible activity planning without requiring the user's predetermined destinations and is especially helpful for those in unfamiliar environments. The rank and classification of points of interest (POI) from location-based social networks (LBSN) are used to indicate different user intentions. The mining of vehicles' physical trajectories can provide exact civil traffic information for path planning. This paper proposes a POI category-based itinerary recommendation framework combining physical trajectories with LBSN. Specifically, a Voronoi graph-based GPS trajectory analysis method is utilized to build traffic information networks, and an ant colony algorithm for multi-object optimization is implemented to locate the most appropriate itineraries. We conduct experiments on datasets from the Foursquare and GeoLife projects. A test of users' satisfaction with the recommended items is also performed. Our results show that the satisfaction level reaches an average of 80%.

• Earthquakes and Structures
• /
• 제22권4호
• /
• pp.421-430
• /
• 2022

This paper addresses the stochastic control problem of robots within the framework of parameter uncertainty and uncertain noise covariance. First of all, an open circle deterministic trajectory optimization issue is explained without knowing the unequivocal type of the dynamical framework. Then, a Linear Quadratic Gaussian (LQG) controller is intended for the ostensible trajectory-dependent linearized framework, to such an extent that robust hereditary NN robotic controller made out of the Kalman filter and the fuzzy controller is blended to ensure the asymptotic stability of the non-continuous controlled frameworks. Applicability and performance of the proposed algorithm shown through simulation results in the complex systems which are demonstrate the feasible to improve the performance by the proposed approach.

• International journal of advanced smart convergence
• /
• 제12권2호
• /
• pp.117-126
• /
• 2023

To improve the overall performance and realism of your game, it is important to calculate the trajectory of a projectile accurately and quickly. One way to increase realism is to use a ballistic model that takes into account factors such as air resistance, density, and wind when calculating a projectile's trajectory. However, the more these factors are taken into account, the more computationally time-consuming and expensive it becomes, creating a trade-off between overall performance and efficiency. Therefore, we present an optimal solution to find a balance between ballistic model accuracy and computation time. We perform ballistic calculations using numerical methods such as Euler, Velocity Verlet, RK2, RK4, and Akima interpolation, and measure and compare the computation time, memory usage (RSS, Resident Set Size), and accuracy of each method. We show developers how to implement more accurate and efficient ballistic models and help them choose the right computational method for their numerical applications.

• Journal of Astronomy and Space Sciences
• /
• 제22권4호
• /
• pp.451-462
• /
• 2005

향후 우리나라의 화성 탐사선 개발을 대비하여 B-평면 조준법(B-plane targeting method)을 이용한 최적 궤적 보정 기동(Optimal Trajectory Correction Maneuver, TCM)의 설계에 대한 연구를 수행하였다. 궤적 보정 기동을 설계하기 위하여 요구되는 화성 탐사 임무의 각 단계별 비행 궤적 및 궤도 정보 역시 이 연구를 통해 개발된 알고리즘을 이용하여 산출 할 수 있으며, 관련 정보는 임무 설계시 필요로 하는 최소의 섭동력들을 고려한 상황에서 산출되었다. 항행 단계에서의 탐사선은 다양한 섭동력에 의한 영향 또는 순간 기동의 오차로 기인된 비행 궤적의 오차로 인하여 목표한 위치에 도달하지 못할 수 있다. 따라서 탐사선의 적절한 비행 궤적을 유지하고 목표하고자 한 지점에 정확하게 도달시키기 위하여 도착 행성의 위치에 대하여 설정된 B-평면 좌표계를 이용하여 탐사선의 방향을 조준하여 줄 필요가 있다. NPSOL 소프트웨어를 사용하여 관련 최적해를 도출하였으며 임무동안 수행되는 기동의 총 크기를 최소화 시키도록 목적함수를 설정하였다. 수행되는 기동의 횟수는 설계자가 임의로 설정($1\~5$회)할 수 있도록 하였으며 그 시기 역시 조정 변수로 설정 할 수 있다. 마지막으로 화성 도착시 설정된 B-평면 좌표의 위치가 최종 구속조건으로 적용되어 최적화 문제를 완성하게 된다. 이 연구를 통하여 지구 출발에서부터 화성 도착, 그리고 임무 수행을 위한 포획궤도에 이르기까지 전반적인 임무 설계 및 해석이 가능하게 되었으며, 항행 단계에서 이루어지는 궤적 보정 기동의 최적 시기 및 크기 또한 분석이 가능하게 되었다. 이 연구를 통하여 개발된 알고리즘을 이용하여 향후 우리나라의 화성 탐사 임무의 설계, 분석이 가능하다.

• 한국항공우주학회지
• /
• 제37권4호
• /
• pp.350-358
• /
• 2009

본 논문은 재진입 비행체의 TAEM 구간 유도와 제어에 관하여 기술 하였다. TAEM 구간은 공기의 밀도와 비행체의 속도의 범위가 큰 특징을 가지고 있으며, 이들 조건하에 TAEM 구간의 유도를 위한 궤적과 비행체의 상태값을 최적화하였다. 최적화된 상태값은 7가지의 상태이며, 상태값은 Down-range, Cross-range, 비행체의 고도, 속도, 경로각, 방위각, 그리고 비행 거리이다. 최적화 연산을 수행하기 위하여 DIDO 프로그램을 사용하였다. 재진입 비행체의 제어를 위하여 인공 신경망을 이용한 되먹임 선형화 제어법을 사용하였다. 비행체의 동역학 모델은 역전파 모델을 통하여 근사화 되고, 근사화된 동역학 모델과 지연된 제어 입력, 플랜트 출력으로부터 새로운 제어 입력을 생성하게 된다. 이를 이용하여 본 논문에서는 앞서 최적화된 7가지의 상태값을 추종하는 결과를 보였다.