• 제목/요약/키워드: Unmanned station

검색결과 109건 처리시간 0.029초

무인 비행체용 저가의 ADGPS/INS 통합 항법 시스템 (Design of a Low-Cost Attitude Determination GPS/INS Integrated Navigation System for a UAV (Unmanned Aerial Vehicle))

  • 오상헌;이상정;박찬식;황동환
    • 제어로봇시스템학회논문지
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    • 제11권7호
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    • pp.633-643
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    • 2005
  • An unmanned aerial vehicle (UAV) is an aircraft controlled by .emote commands from ground station and/o. pre-programmed onboard autopilot system. A navigation system in the UAV provides a navigation data for a flight control computer(FCC). The FCC requires accurate and reliable position, velocity and attitude information for guidance and control. This paper proposes an ADGPS/INS integrated navigation system for a UAV. The proposed navigation system comprises an attitude determination GPS (ADGPS) receive., a navigation computer unit, and a low-cost commercial MEMS inertial measurement unit(IMU). The navigation algorithm contains a fault detection and isolation (FDI) function fur integrity. In order to evaluate the performance of the proposed navigation system, two flight tests were preformed using a small aircraft. The first flight test was carried out to confirm fundamental operation of the proposed navigation system and to check the effectiveness of the FDI algorithm. In the second flight test, the navigation performance and the benefit of the GPS attitude information were checked in a high dynamic environment. The flight test results show that the proposed ADGPS/INS integrated navigation system gives a reliable performance even when anomalous GPS data is provided and better navigation performance than a conventional GPS/INS integration unit.

Ground Test and Evaluation of a Flight Control Systemfor Unmanned Aerial Vehicles

  • Suk, Jin-Young
    • International Journal of Aeronautical and Space Sciences
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    • 제5권1호
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    • pp.57-63
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    • 2004
  • UAV(Unmanned Aerial Vehicle) has become one of the most popularmilitary/commercial aerial robots in the new millennium. In spite of all theadvantages that UAVs inherently have, it is not an easv job to develop a UAVbecause it requires very systematic and complete approaches in full developmentenvelop. The ground test and evaluation phase has the utmost importance in thesense that a well-developed system can be best verified on the ground. In addition,many of the aircraft crashes in the flight tests were resulted from the incompletedevelopment procedure. In this research, a verification procedure of the wholeairbome integrated system was conducted including the flight management system.An airbome flight control computer(FCC) senses the extemal environment from thepehpheral devices and sends the control signal to the actuating system using theassigned control logic and flight test strategy. A ground test station controls themission during the test while the downlink data are transferred from the flightmanagement computer using the serial communication interface. The pilot controlbox also applies additional manual actuating commands. The whole system wastested/verified on the wind-tunnel system, which gave a good pitch controlperformance with a preUspecified flight test procedure. The ground test systemguarantees the performance of fundamental functions of airbome electronic systemfor the future flight tests.

신분당선 전철의 경쟁력 제고 방안 (Competitiveness Increasing Methods of Metropolitan Railway Shinbundang-line)

  • 한우진;박정수
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2009년도 춘계학술대회 논문집
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    • pp.1936-1942
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    • 2009
  • Shinbundang-line is new Metropolitan Railway which was invested by private capital and is under construction for opening in 2010. Now Shinbundang-line pursues various innovation, for example, an express train which uses long distance of each station, and an unmanned operation. And it may be independent of existing metropolitan railway system from a viewpoint of line and fare system. So according to the present plan, Shinbundang-line will be not able to get sufficient demand because of weak connection with existing lines and monotonous function of the line. And it may be difficult to deliver various innovation which Shinbundang-line prepares to passengers. Hereupon, in this paper, I propose 3 methods for increasing competitive power of Shinbundang-line railway. First, making Shinbundang-line a trunk railway line of southern metropolitan area was proposed in relation to northern and southern extension of it. In addition connection with bus and light rail was discussed. Second, multipurpose usage of Shinbundang-line was proposed as express train and conventional passenger train in that line in addition to simple metropolitan railway. Finally, an effective operation method which Shinbundang-line must have was proposed from unmanned driving and fare system side. These methods can improve Shinbundang-line and then it will solve traffic congestion of southern metropolitan area effectively.

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무인 항공 시스템에서 촬영 영상의 GCP 기하보정을 통한 정밀한 지상 표적 좌표 획득 방법 (Acquiring Precise Coordinates of Ground Targets through GCP Geometric Correction of Captured Images in UAS)

  • 안남원;임경미;정소영
    • 한국군사과학기술학회지
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    • 제26권2호
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    • pp.129-138
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    • 2023
  • Acquiring precise coordinates of ground targets can be regarded as the key mission of the tactical-level military UAS(Unmanned Aerial System) operations. The coordinates deviations for the ground targets estimated from UAV (Unmanned Aerial Vehicle) images may depend on the sensor specifications and slant ranges between UAV and ground targets. It has an order of several tens to hundreds of meters for typical tactical UAV mission scenarios. In this paper, we propose a scheme that precisely acquires target coordinates from UAS by mapping image pixels to geographical coordinates based on GCP(Ground Control Points). This scheme was implemented and tested from ground control station for UAS. We took images of targets of which exact location is known and acquired the target coordinates using our proposed scheme. The experimental results showed that errors of the acquired coordinates remained within an order of several meters and the coordinates accuracy was significantly improved.

무인항공기 체계의 통합검증을 위한 무인항공기 체계통합실험실(UAV SIL) 개발 (Development of Unmanned Aerial Vehicle System Integration Laboratory(UAV SIL) for the Integrated Verification)

  • 심재익;우희채;김상진;정상준
    • 한국군사과학기술학회지
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    • 제27권1호
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    • pp.70-79
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    • 2024
  • This paper describes the results of the development of the the unmanned aerial vehicle system integration laboratory(UAV SIL) for the integrated verification. This UAV SIL is designed to test the robustness of the UAV system including the operational logics and the flight control system behaviors under many abnormal and emergency conditions such as data-link losses, airborne subsystem failures, engine shut down conditions, and ground control station faults. This paper presents how to build the UAV SIL and how to verify the in-development UAV system through the UAV SIL.

무인 스피드 스프레이어의 개발(I) -원격제어 및 유도케이블 시스템- (Development of Unmanned Speed Sprayer(I) -Remote Control and Induction Cable System-)

  • 장익주;김태한;조명동
    • Journal of Biosystems Engineering
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    • 제20권3호
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    • pp.226-235
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    • 1995
  • 과수원 방제 작업 시 인체에 해로운 농약으로부터 운전자를 보호하고 노동력 및 농약의 절감, 환경오염의 방지 등의 효과를 꾀하기 위하여 무선 전파 리모콘을 이용한 무인 스피드 스프레이어의 원격제어 시스템을 개발함과 동시에 유도케이블식 주행유도 장치에 의한 자율주행 무인스피드 스프레이어를 개발하였다. 무인 스피드 스프레이어는 원격조종 시스템, 유도케이블 시스템, 장해물 검출장치, 제어 액튜에이터 등으로 구성되어 있고 원격조종 및 자율주행이 가능한 시스템이다. 무인화 한 스피드 스프레이어의 특징은 다음과 같다. 1) 무선 전파 리모콘과 유도 케이블에 의한 주행 유도장치를 개발하여 스피드 스프레이어에 장착한 결과 리모콘 조작방식과 주행 유도방식 모두 가능하였다. 2) 원격 조종은 주행 (전진, 후진), 조향, 3방향의 노즐 및 팬, 분무기, 주행정지 등 16종류의 조작이 가능하다. 3) 농업용 리모콘으로는 FSK방식보다 전송에러가 적은 DTMF방식이 우수하였으며, 농업용 특정 소전력 무선국이 필요하다고 생각된다. 4) 5개의 저임피던스 검출코일과 윈도우 컴퍼레이터 회로로 구성된 디지털식 케이블 유도 시스템은 2개의 검출코일에 유기 된 상대적 전압치로서 궤도를 수정하는 아날로그 검출방식보다 주행 성능이 우수하였다.

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Enhancement of UAV-based Spatial Positioning Using the Triangular Center Method with Multiple GPS

  • Joo, Yongjin;Ahn, Yushin
    • 한국측량학회지
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    • 제37권5호
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    • pp.379-388
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    • 2019
  • Recently, a technique for acquiring spatial information data using UAV (Unmanned Aerial Vehicle) has been greatly developed. It is a very crucial issue of the GIS (Geographic Information System) mapping system that passes way point in the unmanned airframe and finally measures the accurate image and stable localization to the desired destination. Though positioning using DGPS (Differential Global Navigation System) or RTK-GPS (Real Time Kinematic-GPS) guarantee highly accurate, they are more expensive than the construction of a single positioning system using a single GPS. In the case of a low-priced single GPS system, the stability of the positioning data deteriorates. Therefore, it is necessary to supplement the uncertainty of the absolute position data of the UAV and to improve the accuracy of the current position data economically in the operating state of the UAV. The aim of this study was to present an algorithm enhancing the stability of position data in a single GPS mode of UAV with multiple GPS. First, the arrangement of multiple GPS receivers through the center of gravity of the UAV were examined. Next, MD (Mahalanobis Distance) is applied to detect instantaneous errors of GPS data in advance and eliminate outliers to increase the accuracy of previously collected multiple GPS data. Processing procedure for multiple GPS reception data by applying the center of the triangular method were presented to improve the position accuracy. Second, UAV navigation systems integrated multiple GPS through configuration of the UAV specifications were implemented. Using the unmanned airframe equipped with multiple GPS receivers, GPS data is measured with the TCM (Triangular Center Method). In addition, UAV equipped with multiple GPS were operated in study area and locational accuracy of multiple GPS of UAV with VRS (Virtual Reference Station) GNSS surveying were compared. The result showed that the error factors are compensated, and the error range are reduced, resulting in the reliability of the corrected value. In conclusion, the result in this paper is expected to realize high-precision position estimation at low cost in UAV using multiple low-cost GPS receivers.

Multi-constellation Local-area Differential GNSS for Unmanned Explorations in the Polar Regions

  • Kim, Dongwoo;Kim, Minchan;Lee, Jinsil;Lee, Jiyun
    • Journal of Positioning, Navigation, and Timing
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    • 제8권2호
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    • pp.79-85
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    • 2019
  • The mission tasks of polar exploration utilizing unmanned systems such as glacier monitoring, ecosystem research, and inland exploration have been expanded. To facilitate unmanned exploration mission tasks, precise and robust navigation systems are required. However, limitations on the utilization of satellite navigation system are present due to satellite orbital characteristics at the polar region located in a high latitude. The orbital inclination of global positioning system (GPS), which was developed to be utilized in mid-latitude sites, was designed at $55^{\circ}$. This means that as the user is located in higher latitudes, the satellite visibility and vertical precision become worse. In addition, the use of satellite-based wide-area augmentation system (SBAS) is also limited in higher latitude regions than the maximum latitude of signal reception by stationary satellites, which is $70^{\circ}$. This study proposes a local-area augmentation system that additionally utilizes Global Navigation Satellite System (GLONASS) considering satellite navigation system environment in Polar Regions. The orbital inclination of GLONASS is $64.8^{\circ}$, which is suitable in order to ensure satellite visibility in high-latitude regions. In contrast, GLONASS has different system operation elements such as configuration elements of navigation message and update cycle and has a statistically different signal error level around 4 m, which is larger than that of GPS. Thus, such system characteristics must be taken into consideration to ensure data integrity and monitor GLONASS signal fault. This study took GLONASS system characteristics and performance into consideration to improve previously developed fault detection algorithm in the local-area augmentation system based on GPS. In addition, real GNSS observation data were acquired from the receivers installed at the Antarctic King Sejong Station to analyze positioning accuracy and calculate test statistics of the fault monitors. Finally, this study analyzed the satellite visibility of GPS/GLONASS-based local-area augmentation system in Polar Regions and conducted performance evaluations through simulations.

HITL 시뮬레이션 기반 무인비행체 패킷 데이터를 활용한 실시간 이상 탐지 시스템 (Real-time Anomaly Detection System Using HITL Simulation-Based UAV Packet Data)

  • 박대경;김병진
    • 융합보안논문지
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    • 제23권2호
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    • pp.103-113
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    • 2023
  • 최근 몇 년 동안 무인비행체는 다양한 산업 분야에서 널리 사용되고 있다. 그러나, 무인비행체에 대한 의존도가 급격하게 높아짐에 따라 무인비행체의 보안과 안전에 대한 우려가 커지고 있다. 현재 무인비행체의 제어권을 탈취하거나 웹 애플리케이션에서 무인비행체와 통신할 수 있는 권한을 탈취하는 등 다양한 취약점들이 공개되고 있다. 하지만, 무인비행체의 보안과 관련된 연구가 많이 부족한 실정이다. 따라서 본 논문에서는 실제 환경과 유사한 HITL 시뮬레이션 환경에서 무인비행체의 패킷 데이터를 수집하여 패킷 데이터가 정상 데이터인지 비정상 데이터인지 판단하는 연구를 진행하였다. 또한, 본 논문에서는 모델링 과정에서 Computation Cost를 줄이고 데이터 해석의 용이성을 높이는 방법과 정상 데이터만을 학습하여 비정상 데이터를 탐지하는 기계 학습 기반 이상 탐지 모델 및 최적화된 하이퍼 파라미터값을 제안한다.

차등 위성항법 보정을 이용한 정밀 드론 위치추적 시스템 구현 (Implementation of Precise Drone Positioning System using Differential Global Positioning System)

  • 정재영
    • 한국산학기술학회논문지
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    • 제21권1호
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    • pp.14-19
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    • 2020
  • 본 논문은 차등 위성항법 보정 시스템을 이용한 측위 오차 보정을 통해 소형 드론의 위치를 정밀하게 계측할 수 있는 시스템 구현에 대해 서술하고 있다. 본 시스템은 고정된 위치에 자리하는 기준국과 실시간으로 움직이는 이동국(드론)으로 이루어져 있다. 자체 기준국 위치 정보와 국가에서 제공하는 관측 정보를 함께 후처리하여 기준국의 정밀 좌표를 획득하는 과정에 대해 서술하고, 이동국을 정밀 추적하기 위한 차등 위성 항법 시스템의 하드웨어 및 소프트웨어 구성에 대해 설명한다. 기준국 및 이동국 구현에 있어 저가의 경량 위성 항법 수신기 및 오픈소스 소프트웨어 코드와 라이브러리를 활용하여 범용성과 경제성을 극대화 하였으며, 오차 보정 정보 송수신에는 비 면허 주파수 대역 무선통신인 지그비(Zigbee)를 사용하였다. 본 시스템을 이용하여 소형 드론 위치 추적 시험 결과, 평균 측위 오차가 0.8m 및 최대 측위 오차가 1.2m로, 단일 위성 항법 수신기를 사용했을 경우 대비 오차가 86% 개선됨을 확인할 수 있었다.