• 제목/요약/키워드: unmanned aviation vehicle

검색결과 78건 처리시간 0.02초

SHELL 모델과 HFACS를 활용한 영국 민간 무인 항공기 사고 요인 특징 분석 (Characteristics Analysis of Accident Factors of UK Civil Unmanned Aircraft Using SHELL Model and HFACS)

  • 김도윤;장조원
    • 한국항공운항학회지
    • /
    • 제32권1호
    • /
    • pp.1-9
    • /
    • 2024
  • The unmanned aerial vehicle industry has developed a lot, but the possibility of accidents is increasing due to potential risks. In this study, SHELL models and HFACS were used to analyze unmanned aerial vehicle accidents in the UK and to identify the main causes and characteristics of accidents. The main cause analyzed by the SHELL model was identified as an abnormality in the alarm system. The main cause of the accident analyzed by HFACS was identified as the technical environment. The common cause identified by the SHELL model and HFACS was identified as a mechanical problem of unmanned aerial vehicles. This is due to the lack of accurate information or functionality of the alarm system in the operator interface, which often prevents the operator from responding to sensitive information. Therefore, in order to prevent civil UAV accidents, the stability and reliability of the system must be secured through regular inspections of the UAV system and continuous software updates. In addition, an ergonomic approach considering human interfaces is needed when developing technologies.

국방 분야의 인간-차량 인터랙션 연구 (A Survey of Research on Human-Vehicle Interaction in Defense Area)

  • 양지현;이상헌
    • 한국CDE학회논문집
    • /
    • 제18권3호
    • /
    • pp.155-166
    • /
    • 2013
  • We present recent human-vehicle interaction (HVI) research conducted in the area of defense and military application. Research topics discussed in this paper include: training simulation for overland navigation tasks; expertise effects in overland navigation performance and scan patterns; pilot's perception and confidence on an overland navigation task; effects of UAV (Unmanned Aerial Vehicle) supervisory control on F-18 formation flight performance in a simulator environment; autonomy balancing in a manned-unmanned teaming (MUT) swarm attack, enabling visual detection of IED (Improvised Explosive Device) indicators through Perceptual Learning Assessment and Training; usability test on DaViTo (Data Visualization Tool); and modeling peripheral vision for moving target search and detection. Diverse and leading HVI study in the defense domain suggests future research direction in other HVI emerging areas such as automotive industry and aviation domain.

소형 무인기 구조 안전계수 (Structural safety factor for small unmanned aircraft)

  • 김성준;이승규;김태욱
    • 한국항공운항학회지
    • /
    • 제25권2호
    • /
    • pp.12-17
    • /
    • 2017
  • Manned aircraft structural design is based on structural safety factor of 1.5, and this safety factor is equivalent to a probability of failure of between 10-2 and 10-3. The target failure probability of FARs is between 10-6 and 10-9 per flight according to aircraft type. NATO released STANAG 4703 to established the airworthiness requirements for small UAV which is less than 150kg. STANAG 4703 requires the Target Level of Safety according to MTOW. The requirements of failure probability for small UAV is between 10-4 and 10-5. In this paper, requirements of airworthiness certification for small UAV were investigated and the relationship of safety factors to the probability of structural failure is analyzed to reduce measure of safety factor and structural weight of unmanned aircraft.

환경요인에 따른 복합형 수직이착륙 무인항공기의 통합 시스템 오차 상관도 분석 (Analysis of the Total System Error Correlation of Hybrid Fixed-Wing UAV (Unmanned Aerial Vehicle) according to Environmental Factor)

  • 엄송근;김정민;오정환;이동진;김도윤;한상혁
    • 한국항공운항학회지
    • /
    • 제31권1호
    • /
    • pp.11-17
    • /
    • 2023
  • In this study, the correlation analysis between total system error and environmental factor variables was performed to confirm the effect on the performance of the integrated navigation system by various environmental factors. To collect flight data of hybrid vertical take-off and landing UAVs, scenarios including various turning sections and straight sections such as left turn, right turn, turning rate, and path change angle were selected, and environmental data of wind direction, wind speed, temperature, air pressure, and humidity were collected in real time through weather station. As a result of the correlation analysis between the collected flight data and environmental data, it was concluded that the performance of the integrated navigation system by environmental factors within the collected data was not significant affected and was robust.

움직임 예측을 이용한 무인항공기 영상에서의 이동 객체 추적 (Moving Object Tracking in UAV Video using Motion Estimation)

  • 오훈걸;이형진;백중환
    • 한국항행학회논문지
    • /
    • 제10권4호
    • /
    • pp.400-405
    • /
    • 2006
  • 본 논문에서는 무인항공기 영상에서 움직임 예측을 이용한 이동 물체 추적 알고리즘을 제안하였다. 제안한 알고리즘은 초기모델 생성단계와 이동 물체 추적 단계로 구성되어있으며, 이전 프레임에 비해 이동 거리가 커진 경우에도 안정적으로 추적할 수 있었다. 그리고 무인항공기 카메라의 흔들림에도 효과적으로 추적을 할 수 있었고, 이동 물체의 위치를 정확히 검출하여 추적시간을 단축할 수 있었다. 블록 영상과 참조 영상 간 이동물체의 유사도 판정은 블록 매칭 알고리즘을 사용하였다. 제안한 알고리즘은 실험을 통해서 기존의 전역탐색 알고리즘보다 향상된 결과를 보여주었다.

  • PDF

국가공역체계 내에서 군용 무인항공기 비행규칙에 관한 제언 (A Proposal on the Aviation Rules of the Military UAV in the National Airspace System)

  • 박원태;이강석;임광현
    • 한국항공운항학회지
    • /
    • 제22권1호
    • /
    • pp.22-31
    • /
    • 2014
  • Military UAV(Unmanned Aerial Vehicle) operated as a RC(Remotely Control) model level within the limit of the military special use airspace until now. However, the high and medium altitude of URA(Unmanned Reconnaissance Aircraft) which the ROKAF have been trying to import recently is at the UAV level and needs the criteria for the classified airspace flights. The required flight criteria includes operator location, mission operation limit, equipment, etc., which are the principle and standard applied based on the airspace use for UAV. Also, the general flight rules, visual flight rules, instrument flight rules are required in order to have to be applied to the actual flight. Besides, an appliance regulation needs to be arranged regarding two-way communication, ATC and communication issue, airspace and area in-flight between UAS( Unmanned Aircraft System) users. An operation of the UAV in the air significantly requires the guarantee of the aircraft's capacity, and also the standardized flight criteria. A safe and smooth use is ensured only if this criteria is applied and understood by the entire airspace users. For the purpose, a standardized military UAV flight operations criteria that is to be applied for each airspace by UAV is to be prepared through analysis of the present state, a legend UAV system, and a special character analysis.

Use of unmanned aerial systems for communication and air mobility in Arctic region

  • Gennady V., Chechin;Valentin E., Kolesnichenko;Anton I., Selin
    • Advances in aircraft and spacecraft science
    • /
    • 제9권6호
    • /
    • pp.525-536
    • /
    • 2022
  • The current state of telecommunications infrastructure in the Arctic does not allow providing a wide range of required services for people, businesses and other categories, which necessitates the use of non-traditional approaches to its organization. The paper proposes an innovative approach to building a combined communication network based on tethered high-altitude platform station (HAPS) located at an altitude of 1-7 km and connected via radio channels with terrestrial and satellite communication networks. Network configuration and composition of telecommunication equipment placed on HAPS and located on the terrestrial and satellite segment of the network was justified. The availability of modern equipment and the distributed structure of such an integrated network will allow, unlike existing networks (Iridium, Gonets, etc.), to organize personal mobile communications, data transmission and broadband Internet up to 100 Mbps access for mobile and fixed subscribers, rapid transmission of information from Internet of Things (IoT) sensors and unmanned aerial vehicles (UAV). A substantiation of the possibility of achieving high network capacity in various paths is presented: inter-platform radio links, subscriber radio links, HAPS feeder lines - terrestrial network gateway, HAPS radio links - satellite retransmitter (SR), etc. The economic efficiency of the proposed solution is assessed.

Obstacle Awareness and Collision Avoidance Radar Sensor System for Smart UAV

  • Kwag, Young K.;Hwang, Kwang Y.;Kang, Jung W.
    • International Journal of Aeronautical and Space Sciences
    • /
    • 제6권2호
    • /
    • pp.97-109
    • /
    • 2005
  • In this paper, the critical requirement for obstacle awareness and avoidance is assessed with the compliance of the equivalent level of safety regulation, and then the collision avoidance sensor system is presented with the key design parameters for the requirement of the smart unmanned aerial vehicle in low-altitude flight. Based on the assessment of various sensors, small-sized radar sensor is selected for the suitable candidate due to the real-time range and range-rate acquisition capability of the stationary and moving aircraft even under all-weather environments. Through the performance analysis for the system requirement, the conceptual design result of radar sensor model is proposed with the range detection probability and collision avoidance mode is established based on the time-to-collision, which is analyzed by collision scenario.