• Title/Summary/Keyword: 항공 사고

Search Result 419, Processing Time 0.021 seconds

Smart Electric Wheelchair using Eye-Tracking (아이트래킹을 이용한 스마트 전동휠체어)

  • Kim, Tae-Sun;Yoon, Seung-Mok;Kim, Tae-Seong;Park, Hyeon-Kyeong;Park, Seong-Hwan;Kim, Woo-Jong;Jeong, Sang-Su;Jang, Young-Sang;Jung, Hyo-Jin;Park, Su-Bin
    • Proceedings of the Korean Society of Computer Information Conference
    • /
    • 2020.07a
    • /
    • pp.259-260
    • /
    • 2020
  • 기존의 전동휠체어를 사용하는 약자 또는 중증 장애인 등 지체(肢體)가 불편한 사람들이 휠체어 사용 시 생기는 문제점을 해소할 목적으로 시작되었다. 이는 전동휠체어가 보행 기구임에도 자동차에 준하는 교통사고에 대해 무방비하게 노출되고, 중증 장애인에 대한 이동권 보장이 아직 미흡하여 생기는 문제이다. 따라서 본 연구에서는 이러한 문제로 인한 불편함을 해소하고자 아이트래킹을 이용한 스마트 전동휠체어 기술을 적용하고자 한다. 루게릭병 등으로 인해 지체(肢體)의 움직임에 제한이 있는 사람들에게 보호자가 밀어주는 휠체어에 의존하는 것이 아닌 Eye-Tracker를 이용한 시선 추적(Eye-Tracking) 기술로 휠체어 동작이 가능하다. Web-Cam과 라즈베리 파이를 통해 얻은 전·후·좌·우의 영상정보를 디스플레이 화면에 송출한다. 그 후 Eye-Tracking 기술을 이용해 디스플레이 화면에 표시된 전·후·좌·우 이동에 관한 UI(User Interface)룰 사용자가 송출된 영상을 보면서 눈의 움직임만으로 선택해 휠체어의 방향을 제어한다. 또한 전동휠체어의 조작 실수로 다른 행인 또는 장애물과 충돌하는 문제점을 초음파 센서를 이용하여 일정 거리 내에 사물이나 사람이 있을 경우 디스플레이 화면에 경고표시 및 경고음, 각 초음파 센서 위치에 맞는 LED작동으로 사용자들에게 추돌 위험경고와 함께 장애물의 위치파악이 가능하도록 한다. 따라서 스마트 전동휠체어를 통하여 수동적인 움직임이 아닌 능동적이고, 초음파 센서로 인해 안전한 이동이 가능하게 한다.

  • PDF

Review on U.S. Army Helicopter Mishap Analysis for Revision of Crashworthiness Requirements (내추락성 요구도 개정을 위한 미 육군 헬기 사고사례 분석 고찰)

  • Hwang, Jungsun;Lee, Sangmok
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.41 no.9
    • /
    • pp.734-739
    • /
    • 2013
  • Representative crashworthiness requirement documents for military helicopter are MIL-STD-1290 and the Aircraft Crash Survival Design Guide(ACSDG) which were lastly revised in the 1980's. Taking analysis results of diverse U.S. Army helicopter mishaps into account, we can say that adequate guidelines do not exist to ensure crashworthiness of new generation aircraft. In this paper, U.S. Army helicopter mishap analysis conducted by U.S. Army Research, Development and Engineering Command(RDECOM) is readjusted to review the basis of new crashworthiness design criteria for military helicopter, in other words, Full Spectrum Crashworthiness Criteria(FSCC). This analysis effort is a part of FSC development. This effort was to research and quantify the dynamics of military aircraft crashes to be used as the quantitative basis for new design criteria.

Unstable Approach Mitigation Based on Flight Data Analysis (비행 데이터 분석 기반의 불안정 접근 경감방안)

  • Kim, Hyeon Deok
    • Journal of Advanced Navigation Technology
    • /
    • v.25 no.1
    • /
    • pp.52-59
    • /
    • 2021
  • According to the International Air Transport Association (IATA), 61% of the accidents occurred during the approach and landing phase of the flight, with 16% of the accidents caused by unstable access of the commercial aircraft. It was identified that the pilot's unstable approach and poor manipulation of correction led to accidents by continuing the excessive approach without go-around manuever. The causes of unstable access may vary, including airport approach procedures, pilot error, misplanning, workload, ATC (Air Traffic Contol) congestion, etc. In this study, we use the flight data analysis system to select domestic case airports and aircraft type where unstable approach events occur repeatedly. Through flight data analysis, including main events, airport approach procedures, pilot operations, as well as various environmental factors such as weather and geographical conditions at the airport. It aims to identify and eliminate the tendency of unstable approach events and the causes and risks of them to derive implications for mitigating unstable approach events and for developing navigation safety measures.

A Study on the Calculation of Minimum Safety Distance during Storage and Combustion Test of Solid Propellants for Launch Vehicles (발사체 고체추진제의 저장 및 시험 시 안전거리 산정에 관한 연구)

  • Shin, Ahn-Tae;Park, Byung-Mun;Byun, Hun-Soo
    • Korean Chemical Engineering Research
    • /
    • v.59 no.2
    • /
    • pp.180-185
    • /
    • 2021
  • In accordance with the revision of the US-Korea missile guidelines, restrictions on the use of solid propellants for space launch vehicles have been completely lifted. The solid propellant can be used as a solid propellant rocket like the KSR-1 (Korea Sounding Rocket-1), and can also be used as a thrust augmentation booster for liquid fuel launch vehicles. It is known that solid propellants have a lower risk of explosion than liquid propellants. but if an accident such as an explosion at the Alcantara Launch Center in Brazil occurs, it can lead to a large-scale personal accident. In order to prevent such large-scale accidents, it is necessary to review and reflect the minimum safety distance during use, storage and combustion test of solid propellants from the planning phase of the project. In this paper, the minimum safety distance for safe use of the solid propellant is presented by dividing it into storage facilities and combustion tests.

Review of Crash Landing Load Factor (추락착륙 하중배수에 대한 고찰)

  • Bae, Hyo-gil;Kim, Do-Hyung;Park, Jea Sung
    • Journal of Aerospace System Engineering
    • /
    • v.15 no.1
    • /
    • pp.47-55
    • /
    • 2021
  • When an abnormal landing occurs, aircraft structures should be designed to guarantee occupants survivability without preventing egress. To find out fire root causes at crash, lots of fixed aircraft crash tests were conducted. Appropriate crash load factors were established with the comprehension of structural behavior based on dynamic analysis and investigation of human tolerance. Cargo restraint criteria were set up considering passengers safety and operational cost while analyzing past cargo aircraft accident data using a probabilistic approach. Reviewing results of past crash tests, current crash landing load factor was appreciated physically, medically, and economically.

Possibility of Establishing an International Court of Air and Space Law (국제항공우주재판소의 설립 가능성)

  • Kim, Doo-Hwan
    • The Korean Journal of Air & Space Law and Policy
    • /
    • v.24 no.2
    • /
    • pp.139-161
    • /
    • 2009
  • The idea of establishing an International Court of Air and Space Law (hereinafter referred to ICASL) is only my academic and practical opinion as first proposal in the global community. The establishment of the International Court of Air and Space Law can promote the speed and promote fairness of the trial in air and space law cases. The creation of an ICASL would lead to strengthening of the international cooperation deemed essential by the global community towards joint settlement in the transnational air and space cases, claims and would act as a catalyst for the efforts and solution on aircraft, satellite and space shuttle's accidents and cases and all manpower, information, trial and lawsuit to be centrally managed in an independent fashion to the benefit of global community. The aircraft, satellite and spacecraft's accidents attributes to the particular and different features between the road, railway and maritime's accidents. These aircraft, satellite and spacecraft's accidents have incurred many disputes between the victims and the air and space carriers in deciding on the limited or unlimited liability for compensation and the appraisal of damages caused by the aircraft's accidents, terror attack, satellite, space shuttle's accidents and space debris. This International Court of Air and Space Law could hear any claim growing out of both international air and space crash accidents and transnational accidents in which plaintiffs and defendants are from different nations. This alternative would eliminate the lack of uniformity of decisions under the air and space conventions, protocols and agreements. In addition, national courts would no longer have to apply their own choice of law analysis in choosing the applicable liability limits or un-limit for cases that do not fall under the air and space system. Thus, creation of an International Court of Air and Space Law would eliminate any disparity of damage awards among similarly situated passengers and shippers in nonmembers of air and space conventions, protocols, agreements and cases. Furthermore, I would like to explain the main items of the abovementioned Draft for the Convention or Statute of the International Court of Air and Space Law framed in comparison with the Statute of the International Court of Justice, the Statue of the International Tribunal for the Law of the Sea and the Statute of the International Criminal Court. First of all, in order to create the International Court of Air and Space Law, it is necessary for us to legislate a Draft for the Convention on the Establishment of the International Court of Air and Space Law. This Draft for the Convention must include the elected method of judges, term, duty and competence of judge, chambers, jurisdiction, hearing and judgment of the ICASL. The members of the Court shall be elected by the General Assembly and Council of the ICAO and by the General Assembly and Legal Committee of the UNCOPUOS from a list of persons nominated by the national groups in the six continent (the North American, South American, African, Oceania and Asian Continent) and two international organization such as ICAO and UNCOPUOS. The members of the Court shall be elected for nine years and may be re-elected as one time. However, I would like to propose a creation an International Court of Air and Space Law in extending jurisdiction to the International Court of Justice at the Hague to in order to decide the air and space convention‘s cases. My personal opinion is that if an International Court on Air and Space Law will be created in future, it will be settled quickly and reasonably the difficulty and complicated disputes, cases or lawsuit between the wrongdoer and victims and the injured person caused by aircraft, satellite, spacecraft's accidents or hijacker and terrorists etc. on account of deciding the standard of judgment by judges of that’s court. It is indeed a great necessary and desirable for us to make a new Draft for the Convention on a creation of the International Court of Air and Space Law to handle international air and space crash litigation. I shall propose to make a new brief Draft for the Convention on the Creation of an International Court of Air and Space Law in the near future.

  • PDF

A study on the exemption of liability of air carriers (항공운송인의 손해배상책임 면제에 관한 법적 고찰)

  • So, Jae-Seon;Lee, Chang-Kyu
    • The Korean Journal of Air & Space Law and Policy
    • /
    • v.30 no.1
    • /
    • pp.95-116
    • /
    • 2015
  • Air transport agreement can be divided into air passenger contract of carriage and aviation also of the contract of carriage. And air carriers for damages greater (1) cause reason, of (2) limit reason, (3) exemption reason. Exemption reason for the extinction of the liability for damages in our Commercial Code, the Convention and domestic law are mixed. Convention on the Commercial Code and air transport, air transport people, if it is proved and that it has taken all the measures that are needed for the prevention of damage to overdue damage of passengers, liability is waived. So what was to achieve the requirements of all the actions that are reasonably necessary in any case is a problem. Amendment has the feature that the treaty for the International Air Transport reflect in accordance with the domestic situation, while being struck by international standards encompassing land, sea and air transport, even on the system. However, Commercial Code while mainly reflect the Montreal Convention governing air carrier's liability issues on the contract of carriage, a problem which the Convention had also began to occur together. So the problem due to accept the treaty to fit the domestic situation occurs. There is a need for analysis of all of the actions that are "reasonably necessary, which is defined in the Commercial Code. If there is no claim within Value Date rotor two years to air carriers on the court for the damage caused by air transport, the responsibility of air carriers disappear, sued the period of such two years, what kind of meaning on domestic law extension and stop to be whether it is interpreted, it should be determined to do their aggressive measures for the reasonable care and accident prevention.

Comment on the ICAO Draft Convention of the Compensation Liability for the Third Parties on the Surface Caused by Aircraft Accidents and Direction of the Domestic Legislation (항공기사고로 인한 지상 제3자의 배상책임에 관한 ICAO 조약초안에 대한 논평과 국내입법의 방향)

  • Kim, Doo-Hwan
    • The Korean Journal of Air & Space Law and Policy
    • /
    • v.21 no.2
    • /
    • pp.9-53
    • /
    • 2006
  • 오늘날 항공기사고는 우리나라뿐만 아니라 세계도처에서 때때로 발생되고 있다. 특히 외국항공기의 돌연한 추락 또는 물건의 낙하로 인해 지상에 있는 제3자에게 손해를 입히는 경우가 간혹 발생되고 있다. 이와 같은 사건에 있어 가해자(항공기운항자)는 피해자(지상 제3자)에 대하여 불법행위책임을 부담하게 되는데 이 사건해결을 위하여 1952년 및 1978년의 개정로마조약 등이 있음으로 본 논문에서는 이들 조약의 성립경위 및 주요내용과 개정이유 등을 설명하였다. 현재 국제민간항공기관(ICAO)에서는 2001년도 미국의 9,11테러사건 이후 이와 같은 사건의 법적조치와 대응을 위하여 1952년 개정로마조약의 현대화에 관한 새로운 조약초안이 발표되었다. 본 논문에서는 이 새로운 조약초안의 현대화를 위한 ICAO의 활동과 이 조약 초안에 대한 주된 내용과 필자의 논평(견해)을 밝히었다. 한편 본 논문에서는 항공운송인의 책임에 관계된 국제조약과 세계 각국(미국, 영국, 독일, 프랑스, 러시아, 오스트레일리아, 중국 등)의 입법례 등을 참작한 후 우리나라의 현실에 적합한 항공운송법 시안에 관한 국내입법의 추진방향과 항공운송약관의 효력문제, 동법시안을 제정하여야만 되는 이유, 입법경위, 입법방안, "항공운송법 시안"의 주요항목 등 작성하여 제시하였다.

  • PDF

Flight State Prediction Techniques Using a Hybrid CNN-LSTM Model (CNN-LSTM 혼합모델을 이용한 비행상태 예측 기법)

  • Park, Jinsang;Song, Min jae;Choi, Eun ju;Kim, Byoung soo;Moon, Young ho
    • Journal of Aerospace System Engineering
    • /
    • v.16 no.4
    • /
    • pp.45-52
    • /
    • 2022
  • In the field of UAM, which is attracting attention as a next-generation transportation system, technology developments for using UAVs have been actively conducted in recent years. Since UAVs adopted with these technologies are mainly operated in urban areas, it is imperative that accidents are prevented. However, it is not easy to predict the abnormal flight state of an UAV causing a crash, because of its strong non-linearity. In this paper, we propose a method for predicting a flight state of an UAV, based on a CNN-LSTM hybrid model. To predict flight state variables at a specific point in the future, the proposed model combines the CNN model extracting temporal and spatial features between flight data, with the LSTM model extracting a short and long-term temporal dependence of the extracted features. Simulation results show that the proposed method has better performance than the prediction methods, which are based on the existing artificial neural network model.

Implementation of LED panels for Rear Safety of Vehicle (차량의 후방 안전을 위한 LED 패널의 구현)

  • Kim, Tae-Sun;Kim, Sang-Hyeok;Kim, Ki-Hun;Oh, Yong-Teak;Lee, Jae-Hong;Jo, Woo-Bin;Jang, Won-Young;Moon, Jea-Woong;Kim, Kyung-Ho
    • Proceedings of the Korean Society of Computer Information Conference
    • /
    • 2021.01a
    • /
    • pp.177-178
    • /
    • 2021
  • 우리나라 차량의 수는 매년 증가한다. 한 가구당 2대 이상의 차량을 가지고 있는 경우는 드물지 않다. 이는 도로의 포화를 발생시키고 교통사고의 원인이 된다. 본 연구에서는 안전성을 더욱 증가시키는 것을 전제로 아두이노를 이용한 초음파 센서와 라즈베리를 통한 블루투스 기술을 통해 LED 패널에 적용하고자 한다. 현재 많은 차량에는 후방 감지 센서와 차량 후방에서 다가오는 차량을 감지하는 센서 등을 사용하고 있다. 이 기술들은 운전자를 보호하는 장치이지만 모두 개인적으로 사용되는 장치이므로 다른 운전자를 보호하기 위한 장치가 필요하다. 또한, 이러한 시스템이 설치되어 있지 않은 차량이 많다. 추가로 설치하기 위해서 보다 큰 비용을 내야 하므로 적은 비용에 비해 큰 효율을 발생할 수 있는 가성비 좋은 장치가 필요하다. 본 논문은 이러한 문제점들을 개선하기 위해 버스에 장착된 LED 패널과 도로정비 차량 후방에 장착된 LED 패널에서 아이디어에 착안하여 '차량용 후방 안전 LED 패널' 기술을 제안한다. 기존에 글자를 이용해 단순히 의사소통이 가능한 LED 패널을 아두이노와 라즈베리 파이를 통해 사용자가 출력하고 싶은 문구를 실시간으로 출력하여 다른 운전자에게 정보를 전달할 수 있다.

  • PDF