• Title/Summary/Keyword: 궤적기반항행

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Development of Scheduling System for Trajectory Based Air Traffic Management (궤적 기반의 항공 교통 관리를 위한 스케줄링 시스템 개발)

  • Oh, Eun-Mi;Eun, Yeonju;Kim, Hyounkyoung;Jeon, Daekeun
    • Journal of Advanced Navigation Technology
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    • v.22 no.5
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    • pp.367-374
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    • 2018
  • A trajectory-based scheduling system is proposed for air traffic management using next generation aviation data communication link. Based on the service concept of 4-dimensional trajectory data link (4DTRAD) using air traffic serveices (ATS) datalink Baseline 2, a procedure for trajectory-based operation of an en-route flight is established and described in detail. To mitigate air traffic controllers' workload which might be caused by various and complicated data utilization, a prototype of the scheduling system, which predicts the aircraft trajectory based on the flight intents received by air traffic service system and provides advisory information for air traffic control, was developed. The simulation environment for trajectory based operation was built to validate the scheduling functionality of the prototype.

Optimal Surveillance Trajectory Planning for Illegal UAV Detection for Group UAV using Particle Swarm Optimization (불법드론 탐지를 위한 PSO 기반 군집드론 최적화 정찰궤적계획)

  • Lim, WonHo;Jeong, HyoungChan;Hu, Teng;Alamgir, Alamgir;Chang, KyungHi
    • Journal of Advanced Navigation Technology
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    • v.24 no.5
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    • pp.382-392
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    • 2020
  • The use of unmanned aerial vehicle (UAV) have been regarded as a promising technique in both military and civilian applications. Nevertheless, due to the lack of relevant and regulations and laws, the misuse of illegal drones poses a serious threat to social security. In this paper, aiming at deriving the three-dimension optimal surveillance trajectories for group monitoring drones, we develop a group trajectory planner based on the particle swarm optimization and updating mechanism. Together, to evaluate the trajectories generated by proposed trajectory planner, we propose a group-objectives fitness function in accordance with energy consumption, flight risk. The simulation results validate that the group trajectories generated by proposed trajectory planner can preferentially visit important areas while obtaining low energy consumption and minimum flying risk value in various practical situations.

Aircraft 4D Trajectory Model for Air Traffic Control Simulator (항공교통관제 시뮬레이션을 위한 항공기 4D 궤적모델 개발)

  • Jung, Hyuntae;Lee, Keumjin
    • Journal of Advanced Navigation Technology
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    • v.21 no.3
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    • pp.264-271
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    • 2017
  • This paper presents air traffic control simulation model for generating 4D trajectory, and aircraft dynamic model based on 4D trajectory information. With aircraft parameters from BADA and Total Energy Model, the trajectory is defined through modified Bezier curve and the simulation supports two aircraft control methods based on controlled time of arrival (CTA) or airspeed. The simulation results shown that flight time and path were almost identical to the defined trajectory, and derived the differences of each control methods according to wind conditions. Based on the simulation model developed in this study, it is expected to be applied to various air traffic management researches. Future studies will focus on applying optimization techniques in order to minimize the difference between generated trajectories and actual flight routes. This work will increase utilization of developed simulation futhermore.

Vision-Based Robust Control of Robot Manipulators with Jacobian Uncertainty (자코비안 불확실성을 포함하는 로봇 매니퓰레이터의 영상기반 강인제어)

  • Kim, Chin-Su;Jie, Min-Seok;Lee, Kang-Woong
    • Journal of Advanced Navigation Technology
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    • v.10 no.2
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    • pp.113-120
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    • 2006
  • In this paper, a vision-based robust controller for tracking the desired trajectory a robot manipulator is proposed. The trajectory is generated to move the feature point into the desired position which the robot follows to reach to the desired position. To compensate the parametric uncertainties of the robot manipulator which contain in the control input, the robust controller is proposed. In addition, if there are uncertainties in the Jacobian, to compensate it, a vision-based robust controller which has control input is proposed as well in this paper. The stability of the closed-loop system is shown by Lyapunov method. The performance of the proposed method is demonstrated by simulations and experiments on a two degree of freedom 5-link robot manipulators.

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A Study on Effect Analysis of Trajectory-Based Arrival Management using Continuous Descent Operations (연속강하운용을 이용한 궤적 기반의 항공기 도착 관리 효과 분석 연구)

  • Eun-Mi Oh;Daekeun Jeon
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.30 no.4
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    • pp.1-8
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    • 2022
  • In this study, we propose trajectory-based arrival management using CDO (Continuos Descent Operations). The operational procedures with TBO (Trajectory-Based Operations) concept were established to allow aircraft and ground system to share the trajectories with each other in real time. The proposed operational concept was validated in the air traffic control simulation environment, which consists of controller working position, pseudo pilot system, air traffic generation system, and controllers' decision support system for arrival management using CDO. Simulation results compared with actual flight data indicate that proposed concept could improve the efficiency of traffic flow management in terms of total descending time and fuel consumption. And it was confirmed that if there is a system that can share and utilize the synchronized trajectory, it can be helpful to control arrival aircraft and apply CDO concept.

A Algorithm-Based Practical Path Planning Considering the Actual Dynamic Behavioural Constraint in Unmanned Underwater Vehicles (무인잠수정의 실제 동역학적 제한을 고려한 A* 알고리즘 기반 현실적 경로계획)

  • Lee, Jaejun;Moon, Ji Hyun;Lee, Ho Jae;Kim, Moon Hwan;Park, Ho Gyu;Kim, Tae Yeong
    • Journal of the Korean Institute of Intelligent Systems
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    • v.27 no.2
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    • pp.170-178
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    • 2017
  • This paper proposes an improved path-planning technique based on the $A^*$ algorithm. The conventional $A^*$ algorithm only considers the optimality of the planned path and sometimes produces a path that an unmanned underwater vehicle (UUV) cannot navigate due to its dynamic constraint such as the limit of the radius of gyration. It is because that the previous method evaluate the moving cost based on the straight distance between nodes. We enhance the conventional method by evaluating the moving cost on the basis of the practically navigable trajectory, which is generated by the waypoint-tracking control of the UUV dynamics. The simulation examples indeed show the effectiveness of the proposed technique.

An Integration Approach of Trajectory-Based Aviation Weather and Air Traffic Information for NARAE-Weather (나래웨더를 위한 궤적기반 항공기상 정보와 항공교통 정보의 통합 방안)

  • Sang-il Kim;Do-Seob Ahn;Jiyeon Kim;Seungchul Kim;Kyung-Soo Han
    • Korean Journal of Remote Sensing
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    • v.39 no.6_1
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    • pp.1331-1339
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    • 2023
  • In support of the National ATM Reformation and Enhancement Plan (NARAE), a trajectory-based aviation weather service is under development through the NARAE-Weather project. Specifically, weather data presented in a standardized digital format facilitates the seamless integration of digital weather data with air traffic information. Thus, this paper introduces an approach that entails structuring numerical model data to integrate aviation weather information and flight trajectory data. The extraction results using structurally transformed data showed superior performance compared to the results extracted from the original data in terms of performance, and this research is poised to enhance the safety and efficiency of airline operations.

Analysis of Satellite Orbit Elements and Study of Constellation Methods for Micro-satellite System Operation (초소형위성체계 운용을 위한 위성궤도요소 분석 및 위성군 배치기법에 대한 고찰)

  • Soung Sub Lee;Jihae Son;Youngbum Song
    • Journal of Advanced Navigation Technology
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    • v.27 no.4
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    • pp.337-345
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    • 2023
  • This study analyzes considerations for satellite orbit elements for the national micro-satellite system to effectively perform its mission in accordance with the operational concept, and compares the conventionally used Walker method to improve the performance of the satellite constellation method of the repeating ground track orbit. In satellite orbit element analysis, altitude candidate values of micro-satellite system, use of eccentricity and argument of perigee through frozen orbit, necessity of selection of appropriate orbit inclination, and satellite phasing rules for flying the same repeating ground track orbit are proposed. Based on these analysis results, the superiority of the constellation method of the repeating ground track orbit compared to the Walker method is verified in terms of revisit performance analysis, global coverage characteristics, and orbit consistency.

Survey on Visual Navigation Technology for Unmanned Systems (무인 시스템의 자율 주행을 위한 영상기반 항법기술 동향)

  • Kim, Hyoun-Jin;Seo, Hoseong;Kim, Pyojin;Lee, Chung-Keun
    • Journal of Advanced Navigation Technology
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    • v.19 no.2
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    • pp.133-139
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    • 2015
  • This paper surveys vision based autonomous navigation technologies for unmanned systems. Main branches of visual navigation technologies are visual servoing, visual odometry, and visual simultaneous localization and mapping (SLAM). Visual servoing provides velocity input which guides mobile system to desired pose. This input velocity is calculated from feature difference between desired image and acquired image. Visual odometry is the technology that estimates the relative pose between frames of consecutive image. This can improve the accuracy when compared with the exisiting dead-reckoning methods. Visual SLAM aims for constructing map of unknown environment and determining mobile system's location simultaneously, which is essential for operation of unmanned systems in unknown environments. The trend of visual navigation is grasped by examining foreign research cases related to visual navigation technology.

UAS Automatic Control Parameter Tuning System using Machine Learning Module (기계학습 알고리즘을 이용한 UAS 제어계수 실시간 자동 조정 시스템)

  • Moon, Mi-Sun;Song, Kang;Song, Dong-Ho
    • Journal of Advanced Navigation Technology
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    • v.14 no.6
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    • pp.874-881
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    • 2010
  • A automatic flight control system(AFCS) of UAS needs to control its flight path along target path exactly as adjusts flight coefficient itself depending on static or dynamic changes of airplane's features such as type, size or weight. In this paper, we propose system which tunes control gain autonomously depending on change of airplane's feature in flight as adding MLM(Machine Learning Module) on AFCS. MLM is designed with Linear Regression algorithm and Reinforcement Learning and it includes EvM(Evaluation Module) which evaluates learned control gain from MLM and verified system. This system is tested on beaver FDC simulator and we present its analysed result.