• 제목/요약/키워드: Unmanned aerial vehicle system

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무인항공기의 시스템 식별을 위한 비행시험기법 (A Plight Test Method for the System Identification of an Unmanned Aerial Vehicle)

  • 이윤생;석진영;김태식
    • 한국항공우주학회지
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    • 제30권7호
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    • pp.130-136
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    • 2002
  • 본 논문에서는 자동조종장치를 장착한 무인항공기의 시스템 식별을 위한 비행시험기법에 대해 기술하였다. 종운동 및 횡/방향운동 구동입력으로는 멀티스텝 입력을 이용하였다. 각 운동모드에 대해 주파수역 해석을 통해 최적의 입력시간을 설정하였다. 무인항공기의 자동조종장치를 탑재한 비행조종컴퓨터를 이용하여 프로그래밍 모드에서의 비행시험방법으로 종운동과 횡/방향운동의 분리를 통해 시스템 식별을 위한 최적의 자료를 제공하고 있다. 또한 설계치에 근사한 정확한 구동입력을 인가하여 보다 높은 입력주파수를 확보할 수 있었다. 비행시험에서는 안정된 대기상태에서 반복적인 시행을 수행하였으며, 향상된 비행체 탑재 자료저장장치를 이용하여 고품질의 비행자료를 확보하였다. 본 비행시험 기법을 적용하여 획득한 비행자료는 무인항공기의 시스템 식별을 위한 비행자료로 이용되었다.

동적인 위협이 존재하는 전장에서의 무인 항공기 지역경로계획 (A Local Path Planning for Unmanned Aerial Vehicle on the Battlefield of Dynamic Threats)

  • 김기태;남용근;조성진
    • 산업경영시스템학회지
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    • 제35권1호
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    • pp.39-46
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    • 2012
  • An unmanned aerial vehicle (UAV) is a powered aerial vehicle that does not carry a human operator, uses aerodynamic forces to provide vehicle lift, can fly autonomously or be piloted remotely, can be expendable or recoverable, and can carry a lethal or non-lethal payload. An UAV is very important weapon system and is currently being employed in many military missions (surveillance, reconnaissance, communication relay, targeting, strike, etc.) in the war. To accomplish UAV's missions, guarantee of survivability should be preceded. The main objective of this study is a local path planning to maximize survivability for UAV on the battlefield of dynamic threats (obstacles, surface-to-air missiles, radar etc.). A local path planning is capable of producing a new path in response to environmental changes. This study suggests a $Smart$ $A^*$ (Smart A-star) algorithm for local path planning. The local path planned by $Smart$ $A^*$ algorithm is compared with the results of existing algorithms ($A^*$ $Replanner$, $D^*$) and evaluated performance of $Smart$ $A^*$ algorithm. The result of suggested algorithm gives the better solutions when compared with existing algorithms.

Ironbird Ground Test for Tilt Rotor Unmanned Aerial Vehicle

  • Hwang, Soo-Jung;Choi, Seong-Wook
    • International Journal of Aeronautical and Space Sciences
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    • 제11권4호
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    • pp.313-318
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    • 2010
  • The power plant system of a tilt rotor unmanned aerial vehicle (UAV) was verified by the Ironbird ground test, which considerably reduces cost and risk during the developmental stages. The function and performance of the engine, drive line, nacelle conversion, and rotor systems were evaluated using a building block test approach. The Ironbird test concept facilitates the discovery of potential faults in earlier stages of the testing period. As a result, the developmental testing period could effectively be shortened. The measured test data acquired through a ground control and data acquisition system exhibited satisfactory results which meet the developmental specifications of a tilt rotor UAV.

Mapping Herbage Biomass on a Hill Pasture using a Digital Camera with an Unmanned Aerial Vehicle System

  • Lee, Hyowon;Lee, Hyo-Jin;Jung, Jong-Sung;Ko, Han-Jong
    • 한국초지조사료학회지
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    • 제35권3호
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    • pp.225-231
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    • 2015
  • Improving current pasture productivity by precision management requires practical tools to collect site specific pasture biomass data. Recent developments in unmanned aerial vehicle (UAV) technology provide cost effective and real time applications for site specific data collection. For the mapping of herbage biomass (BM) on a hill pasture, we tested a UAV system with digital cameras (visible and near-infrared (NIR) camera). The field measurements were conducted on the grazing hill pasture at Hanwoo Improvement Office, Seosan City, Chungcheongnam-do Province, Korea on May 17 and June 27, 2014. Plant samples were obtained from 28 sites. A UAV system was used to obtain aerial photos from a height of approximately 50 m (approximately 30 cm spatial resolution). Normalized digital number (DN) values of Red and NIR channels were extracted from the aerial photos and a normalized differential vegetation index using DN ($NDVI_{dn}$) was calculated. The results show that the correlation coefficient between BM and $NDVI_{dn}$ was 0.88. For the precision management of hilly grazing pastures, UAV monitoring systems can be a quick and cost effective tool to obtain site-specific herbage BM data.

System Identification and Stability Evaluation of an Unmanned Aerial Vehicle From Automated Flight Tests

  • Jinyoung Suk;Lee, Younsaeng;Kim, Seungjoo;Hueonjoon Koo;Kim, Jongseong
    • Journal of Mechanical Science and Technology
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    • 제17권5호
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    • pp.654-667
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    • 2003
  • This paper presents a consequence of the systematic approach to identify the aerodynamic parameters of an unmanned aerial vehicle (UAV) equipped with the automatic flight control system. A 3-2-1-1 excitation is applied for the longitudinal mode while a multi-step input is applied for lateral/directional excitation. Optimal time step for excitation is sought to provide the broad input bandwidth. A fully automated programmed flight test method provides high-quality flight data for system identification using the flight control computer with longitudinal and lateral/directional autopilots, which enable the separation of each motion during the flight test. The accuracy of the longitudinal system identification is improved by an additional use of the closed-loop flight test data. A constrained optimization scheme is applied to estimate the aerodynamic coefficients that best describe the time response of the vehicle. An appropriate weighting function is introduced to balance the flight modes. As a result, concurrent system models are obtained for a wide envelope of both longitudinal and lateral/directional flight maneuvers while maintaining the physical meanings of each parameter.

Embedded Real-Time Software Architecture for Unmanned Autonomous Helicopters

  • Hong, Won-Eui;Lee, Jae-Shin;Rai, Laxmisha;Kang, Soon-Ju
    • JSTS:Journal of Semiconductor Technology and Science
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    • 제5권4호
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    • pp.243-248
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    • 2005
  • The UAV (Unmanned Aerial Vehicle) systems like unmanned autonomous helicopters are used in various missions of flight navigation and used to collect the environmental information of the surroundings. To realize the full functionalities of the UAV, the software part becomes a challenging problem. In this paper embedded real-time software architecture for unmanned autonomous helicopter is proposed that guarantee real-time performance of hard-real time tasks and re-configurability of soft-real time and non-real time tasks. The proposed software architecture has four layers: hardware, execution, service agent and remote user interface layer according to the reactiveness level for external events. In addition, the layered separation of concurrent tasks makes different kinds of mission reconfiguration possible in the system. An Unmanned autonomous helicopter system was implemented (Kyosho RC Helicopter) in our lab to test and evaluate the performance of the proposed system.

Navigation Performance Analysis Method for Integrated Navigation System of Small Unmanned Aerial Vehicles

  • Oh, Jeonghwan;Won, Daehan;Lee, Dongjin;Kim, Doyoon
    • International journal of advanced smart convergence
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    • 제9권3호
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    • pp.207-214
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    • 2020
  • Currently, the operation of unmanned aerial vehicle (UAV) is regulated to be able to fly only within the visible range, but in recent years, the needs for operation in the invisible area, in the urban area and at night have increased. In order to operate UAVs in the invisible area, at night, and in the urban area, a flight path for UAVs must be prepared like those operated by manned aircraft, and for this, it is necessary to establish an unmanned aircraft system traffic management (UTM). In order to establish the UTM, information on the minimum separation distance to prevent collisions with UAVs and buildings is required, and accordingly, information on the navigation performance of UAVs is required. In order to analyze the navigation performance of an UAV, total system error (TSE), which is the difference between the planned flight path and the actual location of the UAV, is required. If the collected data are insufficient and classification according to integrity, independence, and direction is not performed, accurate navigation performance is not derived. In this paper, propose a navigation performance analysis method of UAV that is derived TSE using flight data and modeled with normal distribution, analyze performance.

A Feasibility Study of Highway Traffic Monitoring using Small Unmanned Aerial Vehicle

  • Ro, Kap-Seong;Oh, Jun-Seok
    • International Journal of Aeronautical and Space Sciences
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    • 제8권2호
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    • pp.54-66
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    • 2007
  • Traffic and emergency monitoring systems are essential constituents of Intelligent Transportation System (ITS) technologies, but the lack of traffic monitoring has become a primary weakness in providing prompt emergency services. Demonstrated in numerous military applications, unmanned aerial vehicles (UAVs) have great potentials as a part of ITS infrastructure for providing quick and real-time aerial video images of large surface area to the ground. Despite of obvious advantages of UAVs for traffic monitoring and many other civil applications, it is rare to encounter success stories of UAVs in civil application including transportation. The objective of this paper is to report the outcomes of research supported by the state agency in US to investigate the feasibility of integrating UAVs into urban highway traffic monitoring as a part of ITS infrastructure. These include current technical and regulatory issues, and possible suggestions for a future UAV system in civil applications.

시퀀스 유사도 기반 무인 비행체 이상 탐지 시스템 (Sequence Based Anomaly Detection System for Unmanned Aerial Vehicle)

  • 서강욱;김휘강
    • 정보보호학회논문지
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    • 제32권1호
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    • pp.39-48
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    • 2022
  • 본 논문에서는 무인 비행체 내부 네트워크의 이상 징후를 탐지하는 시퀀스 기반 이상 탐지 시스템을 제안한다. 제안하는 이상 탐지 시스템은 무인 비행체가 지상 통제 시스템에 주기적으로 전송하는 상태 메시지 시퀀스들 간의 유사도를 측정하여 이상 징후를 탐지한다. 본 연구에서는 무인 비행체 내부 네트워크에서 수행 가능한 악의적인 메시지 주입 공격 세 가지를 정의하고, 해당 공격 기법들을 Pixhawk4 쿼드콥터에서 시뮬레이션하였다. 결과적으로, 제안하는 이상 탐지 시스템은 96% 이상의 정확도로 비정상 시퀀스를 탐지할 수 있었다.

복합재 주익 무인항공기의 낙뢰보호 설계와 피격영역 해석 (Protection Design and Lightning Zone Analysis for Unmanned Aerial Vehicle with Composite Wings)

  • 우희채;김용태
    • 한국군사과학기술학회지
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    • 제26권3호
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    • pp.302-312
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    • 2023
  • This paper describes the analysis of lightning strike zoning, the indirect lightning data simulation and the protection design for lightning indirect effects of equipment by lightning strike for unmanned aircraft consisting of composite wings. Through the analysis of lightning strike zoning according to the external shape of unmanned aerial vehicles, the structure areas that should be protected during lightning strike is derived, and the protection requirements of lightning indirect effects for flight critical equipments and equipment that must be operated upon lightning strike was derived. Lightning protection levels according to the location of mounting equipment and surrounding structure materials for each equipment was derived, and the protection design of the unmanned aerial vehicle with composite structures was also proposed from direct effect of lightning. Later, the lightning protection technology will be verified by the ground test of lightning direct and indirect effects.