• Title/Summary/Keyword: 무인항공시스템

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A Study on the Establishment of Minimum Safe Altitude and UAS Operating Limitations (최저비행고도와 UAS 운영제한고도 구축에 관한 연구)

  • Kim, Do Hyun;Lee, Dong Jin
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.29 no.2
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    • pp.94-99
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    • 2021
  • UTM is an air traffic management ecosystem under development for autonomously controlled operations of UAS by the FAA, NASA, other federal partner agencies, and industry. They are collaboratively exploring concepts of operation, data exchange requirements, and a supporting framework to enable multiple UAS operations beyond visual line-of-sight at altitudes under AGL 500ft in airspace where air traffic services are not provided. Minimum Safe Altitude is a generic expression, used in various cases to denote an altitude below which it is unsafe to fly owing to presence of terrain or obstacles. The European drone regulation mentions that the UAS is maintained within 120 metres from the closest point of the surface of the earth during flight, except when overflying an obstacle. This study attempted to develop a minimum flight altitude database system. Based on domestic and international rules and regulations on setting the minimum flight altitude it is expected that it can be applied to the operation of aircraft and unmanned aerial system in UTM environments for specific area in Korea.

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
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    • v.16 no.4
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    • pp.45-52
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    • 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.

Research on Dual Flight Control System for High Altitude Long Endurance UAV (고고도 장기체공 무인기의 비행제어시스템 이중화에 대한 연구)

  • An, Seok-Min;Kim, Seong-Uk;Yu, Hyeok
    • 한국항공운항학회:학술대회논문집
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    • 2015.11a
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    • pp.55-58
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    • 2015
  • 고고도 장기체공 무인기는 일반적인 무인기와 달리 고고도에서의 환경과 장시간의 체공에 따른 위험도가 높을 수밖에 없다. 따라서 신뢰도를 높이기 위한 다양한 방안을 강구해야 한다. 가장 중요한 요소 중 하나가 비행제어시스템이며, 본 논문에서는 비행제어시스템의 이중화에 따른 설계결과와 비행시험결과를 기술하였다.

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Challenges; Interoperability of UAV in the NAS (국가공역체계에서 무인항공기 통합운영에 대한 동향)

  • Kim, Joong-Wook;Kim, Do-Hyun
    • Current Industrial and Technological Trends in Aerospace
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    • v.8 no.2
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    • pp.136-144
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    • 2010
  • The utilization of UAV and the activities of diverse widening, now the challenge was how to operate and integrate UAV safely in the NAS. The purpose of this study is to look around the trend for interoperability of UAV in the NAS and to provide its implications and the future direction of integrated operating airspace focusing on U.S. where R&D and demand of UAV are the most in the world.

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Development of Video Transfer System using LTE/WiFi for Small UAV (LTE/WiFi 기반 소형 무인기용 영상 전송 시스템 개발)

  • Bae, Joong-Won;Lee, Sang-Jeong
    • Journal of Aerospace System Engineering
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    • v.13 no.2
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    • pp.10-18
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    • 2019
  • In this paper, we present the results of a developed LTE/Wi-Fi-based video transmission system which can be applied in small unmanned aerial vehicles of 25kg or less. The developed video transmission system comprised of airborne datalink terminal, ground datalink terminal, and used LTE and Wi-Fi wireless data communication technologies to transmit videos of resolution higher than HD (720p/30fps, 1080p/30fps) taken by small UAV. The airborne device is designed to efficiently transmit real-time streaming video through the incorporation of H.264 video processing board. Ground tests and evaluation indicated the possibility of the developed system to transmit real-time videos from close distance in regards to non-line-of-sight area.

Technology Trends and Performance Evaluation for Unmanned Aircraft System Datalink (무인 항공 시스템 데이터링크 기술 동향 및 성능 분석)

  • Hwang, Hyunsu;Jung, Yongcheol;Jung, Yunho
    • Journal of Advanced Navigation Technology
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    • v.20 no.4
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    • pp.329-335
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    • 2016
  • Unmanned aircraft systems (UAS) are defined as the system whose components include the necessary equipment, network, and personnel to control an unmanned aircraft. In the past, UAS were predominately operated for military operations. However, nowadays, the applications of UAS to commercial area are explosively augmented and UAS are being expected to be integrated in national airspace. Therefore, the need for the standardized datalink systems rapidly and the development of control and non-payload communication (CNPC) system are being processed for integration in national airspace in United States and Europe. In this paper, the technology trends for UAS CNPC datalink are explained and presented the performance evaluation results for CNPC system, which is the modified version of IEEE 802.15.4 ZigBee system.

Electric power Small fixed wing UAV Aerodynamic performance Analysis (전기 동력 소형 고정익 무인항공기 공력성능 연구)

  • Jeong, Seongrok
    • Journal of Aerospace System Engineering
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    • v.13 no.1
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    • pp.11-17
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    • 2019
  • In this paper, the performance of a small fixed wing unmanned aerial vehicle is predicted theoretically with the minimum specifications and a low Reynolds number. Based on the results, it was compared with the results of an actual flight test and simple electric motor wind tunnel test. As a result of the validity of the analysis, a 3.5 kilograms class fixed wing small UAV can predict aerodynamic performance by general theory analysis. However, the required thrust was analyzed as a possible design error. Based on the results of this study, this paper proposed a method to minimize the design error when developing small fixed wing UAV flying in a low Reynolds number.

An Improved CNN-LSTM Hybrid Model for Predicting UAV Flight State (무인항공기 비행 상태 예측을 위한 개선된 CNN-LSTM 혼합모델)

  • Hyun Woo Seo;Eun Ju Choi;Byoung Soo Kim;Yong Ho Moon
    • Journal of Aerospace System Engineering
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    • v.18 no.3
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    • pp.48-55
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    • 2024
  • In recent years, as the commercialization of unmanned aerial vehicles (UAVs) has been actively promoted, much attention has been focused on developing a technology to ensure the safety of UAVs. In general, the UAV has the potential to enter an uncontrollable state caused by sudden maneuvers, disturbances, and pilot error. To prevent entering an uncontrolled situation, it is essential to predict the flight state of the UAV. In this paper, we propose a flight state prediction technique based on an improved CNN-LSTM hybrid mode to enhance the flight state prediction performance. Simulation results show that the proposed prediction technique offers better state prediction performance than the existing prediction technique, and can be operated in real-time in an on-board environment.

A Study on the Development of Low-Altitude and Long-Endurance Solar-Powered UAV from Korea Aerospace University (3) - Flight Test Results and Analysis of Solar Powered UAV - (한국항공대학교 저고도 장기체공 태양광 무인기 개발에 관한 연구 (3) - 태양광 무인기 비행실험 결과 및 분석 -)

  • Kim, Doyoung;Kim, Taerim;Jeong, Jaebaek;Park, Sanghyuk;Bae, Jae-Sung;Moon, Seokmin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.50 no.7
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    • pp.489-496
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    • 2022
  • This paper introduces the system for KAU-SPUAV, which is designed and developed by Korea Aerospace University, and verifies its performance through flight test. Specification of two versions of KAU-SPUAV, avionics system, and Ground Control System (GCS) are introduced. Three missions are performed with suggested UAVs: LTE signal mapping, circumnavigation of Jeju island seashore, and long endurance flight. Each mission consists of long distance and long endurance flight which takes advantage of KAU-SPUAV. Research team of KAU-SPUAV confirmed its versatility through suggested flight data. Also based on flight results, the team found the potential of performance improvement of KAU-SPUAV.

A study of the status of UAS Certification System and Airworthiness Standards (민간 무인항공기시스템 인증체계 현황 및 관련규정 연구 동향 분석)

  • Ahn, Hyojung;Park, Jonghyuk;Yoo, Seungwoo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.10
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    • pp.893-901
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    • 2014
  • UAS and related technology have been mainly developed for military use but, in recent years, various types of civil UAS have been using in a variety of applications. For example, there are multicopters to shoot aerial photography, pesticide spraying unmanned helicopter, and in addition there are radio control (R/C) aircraft to be used for hobbyists. UAV has spread rapidly enough that permitted experts as well as the public can use it but the related safety regulations are not properly equipped. We investigated the status of domestic and international UAS certification system and airworthiness standards. And the trends in research for the development and modification of the certification system were studied in this paper. As a result, most countries have studied to develop the related regulations and especially ICAO has tried to develop RPAS manual, standards and recommended plans and modify the related ICAO annex through the research group, ICAO UASSG. Based on the manual and SARPs, authorities, related organizations and companies have prepared to develop and modify regulations in accordance with the actual situation of each country.