• Title/Summary/Keyword: 비행환경변화

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auto-pilot flight for UAVs using public Data (공공 데이터를 이용한 UAV 자동경로비행)

  • Park, KyungSeok;Kim, MinJun;Oyindamola, Owolabi Ganiyat;LIU, HUIYU;Kim, SungHo
    • Proceedings of the Korea Information Processing Society Conference
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    • 2019.05a
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    • pp.242-245
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    • 2019
  • 움직이는 UAV는 많은 위치에너지와 운동에너지를 가지므로 지상으로 추락하는 경우 많은 충격량을 가질 수 있다. 이는 인명피해로 연결될 수 있기 때문에 본 논문에서는 UAV 비행경로 상의 인구밀집지역을 위험구역으로 정의하였다. 기존의 UAV 경로비행은 사용자에 의해 미리 설정된 경로만을 운행하는 수동적인 형태였다. 일부 UAV는 경로비행 중 장애물을 회피하는 시스템 등 안전기능을 포함하고 있지만, 비행환경변화에 대응하기에는 부족하다. UAV 경로비행에 공공 데이터를 활용할 경우, 위험구역을 검출하고 회피비행을 수행할 수 있어서 비행환경변화에 대한 대응이 향상될 수 있다. 따라서 본 논문에서는 수집된 데이터를 활용하여 위험구역을 회피하는 최적경로 비행 방안을 제안한다. 실험결과, 제안하는 자동경로비행에서 목적지와 목적지에 따른 경로를 지정할 경우, 위험지역을 스스로 판단하여 최적 우회경로로 비행하는 것을 확인하였다. 추후 회피방안에 따라 비행하여 획득하는 영상의 질적 만족도를 높일 수 있는 방안을 연구할 예정이다.

A Study on the Changing Factors of Flight Operational Environment (운항 환경 변화 요인에 관한 연구)

  • Youn, Seung-Joong;Han, Kyoung-Keun
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.1
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    • pp.37-66
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    • 1993
  • 항공기 운항과 관련한 환경의 변화는 다른 분야의 환경 변화보다 그속도가 빠르고 변화의 폭이 크다고 할 수 있다. 약 1세기 동안에 항공기 개발기술은 실로 놀라운변화를 거듭해 왔으며 전자시스템의 도입으로 수 십년 전에는 상상조차 할 수 없었던 일들이 현실로 나타나게 되었다. 본 논문은 이러한 환경변화 가운데 비행안전이라는 목표를 실현하기 위해 우선적으로 항공기 운항과 관련한 환경변화 요인들에 내포되어 있는 문제점들을 분석하고자 하였으며 장비개발 및 Human Factor, 항공교통 관제 및 항공기 운항 그리고 조종사 관리 및 조종 환경으로 분야를 나누어 요인 분석을 함으로써 현재와 미래를 통해 예상되는 문제점들을 도출하였다. 또한 항공기 사고사례를 분석하여 공통되는 요인을 도출, 이를 문제점으로 제시하였다. 이러한 문제점들에 대한 대책에 관한 연구는 항공기 운항 분야의 발전과 비행안전을 위해 계속해서 이루어질 것으로 기대한다.

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Detecting and Avoiding Dangerous Area for UAVs Using Public Big Data (공공 빅데이터를 이용한 UAV 위험구역검출 및 회피방법)

  • Park, Kyung Seok;Kim, Min Jun;Kim, Sung Ho
    • KIPS Transactions on Software and Data Engineering
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    • v.8 no.6
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    • pp.243-250
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    • 2019
  • Because of a moving UAV has a lot of potential/kinetic energy, if the UAV falls to the ground, it may have a lot of impact. Because this can lead to human casualities, in this paper, the population density area on the UAV flight path is defined as a dangerous area. The conventional UAV path flight was a passive form in which a UAV moved in accordance with a path preset by a user before the flight. Some UAVs include safety features such as a obstacle avoidance system during flight. Still, it is difficult to respond to changes in the real-time flight environment. Using public Big Data for UAV path flight can improve response to real-time flight environment changes by enabling detection of dangerous areas and avoidance of the areas. Therefore, in this paper, we propose a method to detect and avoid dangerous areas for UAVs by utilizing the Big Data collected in real-time. If the routh is designated according to the destination by the proposed method, the dangerous area is determined in real-time and the flight is made to the optimal bypass path. In further research, we will study ways to increase the quality satisfaction of the images acquired by flying under the avoidance flight plan.

A Study on Thermal Characteristics of Stratospheric Airship Considering Radiation Heat Transfer (복사 열전달에 의한 성층권 무인 비행선의 열 특성 연구)

  • Kim Seung-Min;Lee Sang-Myeong;Roh Tae-Seong;Choi Dong-Hwan
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2005.11a
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    • pp.285-288
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    • 2005
  • A Stratospheric airship should stay long to achieve its original mission. Meanwhile, to obtain what the solar radiation and heat transfer have an effect on Stratospheric condition, heat analysis has been done. For this work, Stratospheric heat condition's been examined and for the numerical analysis, by using Gridgen, grids of airship have been generated. And by using STAR-CD, the study about heat characteristic of airship model was carried out. Especially, with changing the position of the Sun, the temperature change of the airship body was focused on. With this background, the possibility of realizing the simulation of the effects solar radiation have on the Stratospheric airship.

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A Study on Thermal Characteristics of Stratospheric Airship Considering Radiation Heat Transfer (복사 열전달에 의한 성층권 무인 비행선의 열 특성 연구)

  • Kim Seung-Min;Lee Sang-Myeong;Park Hwi-Seob;Roh Tae-Seong;Choi Dong-Hwan
    • Journal of the Korean Society of Propulsion Engineers
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    • v.10 no.2
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    • pp.31-38
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    • 2006
  • A study of thermal characteristics of the airship considering radiation heat transfer has been conducted by building a numerical model for the airship in order to identify the possibility to obtain the reliable flight performance in severe stratospheric heat conditions. The variations of distributed temperature of the skin and the inner flow by free convection have been calculated according to the change of the solar position. As the results of the analyses, the stratospheric heat conditions slightly have an influence on the flight performance of the airship.

Flight Trajectory Simulation via Reinforcement Learning in Virtual Environment (가상 환경에서의 강화학습을 이용한 비행궤적 시뮬레이션)

  • Lee, Jae-Hoon;Kim, Tae-Rim;Song, Jong-Gyu;Im, Hyun-Jae
    • Journal of the Korea Society for Simulation
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    • v.27 no.4
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    • pp.1-8
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    • 2018
  • The most common way to control a target point using artificial intelligence is through reinforcement learning. However, it had to process complicated calculations that were difficult to implement in order to process reinforcement learning. In this paper, the enhanced Proximal Policy Optimization (PPO) algorithm was used to simulate finding the planned flight trajectory to reach the target point in the virtual environment. In this paper, we simulated how this problem was used to find the planned flight trajectory to reach the target point in the virtual environment using the enhanced Proximal Policy Optimization(PPO) algorithm. In addition, variables such as changes in trajectory, effects of rewards, and external winds are added to determine the zero conditions of external environmental factors on flight trajectory learning, and the effects on trajectory learning performance and learning speed are compared. From this result, the simulation results have shown that the agent can find the optimal trajectory in spite of changes in the various external environments, which will be applicable to the actual vehicle.

A study on the efficient design of pilot education according to the advances in aviation technology (항공기술 발전에 따른 효과적인 비행교육 방안에 관한 연구)

  • Eun, Hee-Bong
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.3 no.1
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    • pp.7-19
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    • 1995
  • 현대 항공기의 특징인 자동화나 컴퓨터화는 조종석(Glass cockpit)에서의 조종사 임무를 변화시켜, 과거에는 항공기를 조종하기 위하여 속도, 고도, 항로를 유지하는 것이 주된 임무였으나, 현대 항공기의 경우에는 이러한 일은 거의 모두 자동화 되어 조종사는 일명 'Glass cockpit' 내에서 화면을 통하여 비행 진행 상태를 모니터하고 필요한 사항을 컴퓨터에 입력하여 지시하는 형태로 바뀌었다. 따라서 조종사 교육제도도 과거의 기술(Skill)이나 절차(Procedure)를 위주로 하던 형태에서, 이제는 조종사에게 관리자(Manager)로서의 능력을 부여할 수 있는 교육내용이 요구되고 있다. 본 연구에서는 항공기술 발전과 특히 미래 항행시스템의 개발에 관하여 살펴보고, 운항환경 변화에 따른 변화된 조종사의 역할과 이를 기준으로 우리나라의 대표적 민간 조종사 교육기관이라 할 수 있는 한국 항공대학교 항공운항학과와 대한항공의 기초비행 훈련원, 아시아나 항공의 초기조종사 훈련과정(Ab-initio)의 교육내용을 비교 분석하여 앞으로 조종사 교육에 있어서 추가되어야 하거나 개선되어야 할 내용에 관하여 연구하였다.

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Risk Assessment of a Drone Under the Gust and its Precise Flight Simulation (드론의 외풍 환경 비행 안전성 평가 및 정밀 시뮬레이션)

  • Lee, DongYeol;Park, SunHoo;Shin, SangJoon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.50 no.3
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    • pp.173-180
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    • 2022
  • The operation and transportation environment for an unmanned aerial vehicle will be completely different from those for the conventional air and ground transportation. The requirement for a traffic management system for its safe operation has been emerging. Accordingly, investigation is being conducted to analyze the danger that unmanned aerial vehicle may encounter during the flight and to provide the countermeasure by the simulation. When the drones operate in an urban environment, they may be affected by the wind around the building. Thus it is essential to predict the influence of the gust and analyze the resulting risk. In this paper, a method for evaluating the safety for a flight mission under the gust is suggested. By using the precise 6-degree-of-freedom flight simulation that is capable of simulating the gust condition, possible deviation from the pre-planned flight path in terms of the attitude orientation will be predicted. A method of quantifying the probability of the flight mission failure will also be presented.

Prediction of the Flight Times of Hydrochara affinis and Sternolophus rufipes in Paddy Fields Based on RCP 8.5 Scenario (RCP 8.5 기후변화 시나리오를 적용한 논 서식 애물땡땡이 (Sternolophus rufipes)와 잔물땡땡이(Hydrochara affinis)의 비행시기 예측)

  • Choi, Soon-Kun;Kim, Myung-Hyun;Choe, Lak-Jung;Eo, Jinu;Bang, Hea-Son
    • Korean Journal of Agricultural and Forest Meteorology
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    • v.18 no.1
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    • pp.16-29
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    • 2016
  • The total area of paddy field was estimated to be 55 % of the cultivated lands in South Korea, which is approximately 1 million hectares. Organisms inhabiting paddy fields if they are sensitive to environmental changes can be environmental indicator of paddy fields. Biological indicators such as phenology and distributional range are evaluated as intuitive and quantitative method to analyze the impact of climate change. This study aims to estimate flight time change of Hydrophilidae species' based on the RCP 8.5 climate change scenario. Unmanned monitoring systems were installed in Haenam, Buan, Dangjin and Cheorwon relative to the latitudinal gradient. In the three regions excepting Cheorwon, it was able to measure the abundance of flying Hydrochara affinis and Sternolophus rufipes. Degree-day for the flight time was determined based either on field measurement values and estimates of 2020s, 2050s and 2080s from KMA climate change scenario data. As a result, it is found that date of both species of initial flight becomes 15 days earlier, that of peak flight becomes 22 days earlier and that of final flight does 27 days earlier in 2080s compared to 2020s. The climate change impact on flight time is greater in coastal area, rural area and valley than inland area, urban area and plan. H. affinis and S. rufipes can be used as climate change indicator species.

Instrument Flight Certification Process and Flight Test Results of Korean Utility Helicopter (한국형 기동헬기 계기비행 인증절차 및 비행시험 결과)

  • Kwon, Hyuk-Jun;Park, Jong-Hoo;Park, Jae-Young
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.2
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    • pp.173-180
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    • 2014
  • In this paper, the instrument flight certification process and flight test results of Korean Utility Helicopter (KUH) are presented. For the instrument flight certification, the suitability of installed equipments and instruments have been reviewed and verified by ground and flight tests. Next, static and dynamic stability test are conducted in accordance with FAR-29 Appendix B. The static stability is determined by the change of speed and attitude according to control inputs. The dynamic stability is evaluated by how quickly the response of the helicopter due to long and short period control inputs are decreased. The pilot workload evaluation are also carried out by simulated IMC flight tests. This paper presents the workload assessment results when some failures are occurred at cockpit instruments, engine or flight control systems as well as the normal situation. After the simulated IMC flight test is completed, actual instrument flight test are conducted in a real IMC environment according to the air traffic controls.