• 전기전자학회논문지
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• 제26권2호
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• pp.141-149
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• 2022

인공지능 및 무인 감시, 자율화 기술의 발전으로 인해 무인으로 운용되는 원격 감시/자율 주행 시스템의 개발이 활발히 연구되고 있다. 개발되는 원격운용 및 제어 시스템의 효과적인 성능분석을 위해서는 원격운용 시스템의 데이터를 실시간으로 기록하고 그 데이터를 분석하는 일이 중요하다. 또한, 통제 시스템과 원격 시스템 간의 성능분석을 위해서는 각 시스템의 기록데이터 간 시간동기화가 필수적으로 요구된다. 본 논문에서는 원격운용 시스템의 기록데이터 분석을 위한 GPS 기반 시간동기화 설계 방안을 제시한다. 제안 방법은 기록데이터에 GPS 신호를 활용한 정밀한 시간정보를 기록함으로써 원격 시스템이 기록데이터 시간 오차를 1ms 이내로 만족할 수 있도록 하였으며, OS 내 설정을 통해 이더넷 통신을 특정 CPU가 전담하도록 하는 CPU shielding 및 affinity 설정 기법을 통해 시간동기화 성능을 개선하였다. 제안 방법은 단계별 실험 및 네트워크 데이터 저장 실험을 통해서 그 성능을 입증하였으며, 무인수색차량의 무인차량과 통제차량 기록장치에 적용할 수 있음을 확인하였다. 제안 방법은 향후 무인수색차량의 네트워크 데이터 분석 방법으로 활용할 예정이며, 활용 중에 발생하는 다양한 분석을 통해 성능 개선을 해 나갈 예정이다.

• 한국항행학회논문지
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• 제8권2호
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• pp.105-111
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• 2004

최근의 무인항공기는 정찰임무를 비롯하여 무인기에 미사일을 장착하여 지대공 공격 임무를 수행하기까지 군용으로 뿐만 아니라 기상 관측, 해상 관측 등의 목적으로 폭넓게 활용하고 있으며, 점차 필요성이 높아지고 있다. 이러한 무인기는 정밀한 자세제어를 위하여 자세정보를 제공하는 AHRS와 같은 센서를 장착하는데 비용이 500만원 정도에서 고급 센서는 수 천 만원에 이르고 있다. 최근 한국항공우주연구원에서는 이러한 고가의 센서 출력정보인 자세각 정보를 사용하지 않고 각속도 정보를 기반으로 저가형 자동비행시스템을 개발하여 소형표적기와 무인표적기 비행시험을 통하여 성능을 입증하였다. 본 논문에서는 무인항공기의 항법시스템 설계를 위하여 목표로 하는 신뢰성을 충족시키면 동시에 저가형인 GPS 센서를 선택하기 위하여 Hardware in the Loop Simulation(HILS)을 통하여 GPS 출력주파수에 따른 성능을 확인하였다. 마지막으로 무인표적기에 자동비행시스템과 항법시스템을 장착하여 비행시험을 수행하였으며, 설계된 항법시스템 성능을 비행시험 결과를 통하여 확인하였다.

• 산업경영시스템학회지
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• 제45권1호
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• pp.10-19
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• 2022

Recently, the Defense Advanced Research Projects Agency(DARPA) in the United States is studying a new concept of war called Mosaic Warfare, and MUM-T(Manned-Unmanned Teaming) through the division of missions between expensive manned and inexpensive unmanned aircraft is at the center. This study began with the aim of deriving the priority of autonomous functions according to the role of unmanned aerial vehicles in the present and present collaboration that is emerging along with the concept of mosaic warfare. The autonomous function of unmanned aerial vehicles between the presence and absence collaboration may vary in priority depending on the tactical operation of unmanned aerial vehicles, such as air-to-air, air-to-ground, and surveillance and reconnaissance. In this paper, ACE (Air Combat Evaluation), Skyborg, and Longshot, which are recently studied by DARPA, derive the priority of autonomous functions according to air-to-air collaboration, and use AHP analysis. The results of this study are meaningful in that it is possible to recognize the priorities of autonomous functions necessary for unmanned aircraft in order to develop unmanned aerial vehicles according to the priority of autonomous functions and to construct a roadmap for technology implementation. Furthermore, it is believed that the mass production and utilization of unmanned air vehicles will increase if one unmanned air vehicle platform with only essential functions necessary for air-to-air, air-to-air, and surveillance is developed and autonomous functions are expanded in the form of modules according to the tactical operation concept.

• International Journal of Aeronautical and Space Sciences
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• 제18권4호
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• pp.623-640
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• 2017

The full nonlinear equations of an unmanned aerial vehicle ground taxiing mathematical dynamic model are built based on a type of unmanned aerial vehicle data in LMS Virtual.Lab Motion. The flexible landing gear model is considered to make the aircraft ground motion more accurate. The electric braking control system is established in MATLAB/Simulink and the experiment of it verifies that the electric braking model with the pressure sensor is fitted well with the actual braking mechanism and it ensures the braking response speediness. The direction rectification control law combining the differential brake and the rudder with 30% anti-skid brake is built to improve the directional stability. Two other rectifying control laws are demonstrated to compare with the designed control law to verify that the designed control is of high directional stability and high braking efficiency. The lateral displacement increases by 445.45% with poor rectification performance under the only rudder rectifying control relative to the designed control law. The braking distance rises by 36m and the braking frequency increases by 85.71% under the control law without anti-skid brake. Different landing conditions are simulated to verify the good robustness of the designed rectifying control.

• 한국군사과학기술학회지
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• 제13권2호
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• pp.171-179
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• 2010

A fundamental technology of UGV(Unmanned Ground Vehicle) to perform a given mission with success in various environment is a path planning method which generates a safe and optimal path to the goal. In this paper, we suggest a local path-planning method of UGV based on the binary map using world model data which is gathered from terrain perception sensors. In specially, we present three core algorithms such as shortest path computation algorithm, path optimization algorithm and path smoothing algorithm those are used in the each composition module of LPP component. A simulation is conducted with M&S(Modeling & Simulation) system in order to verify the performance of each core algorithm and the performance of LPP component with scenarios.

• 제어로봇시스템학회논문지
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• 제18권3호
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• pp.251-257
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• 2012

Unmanned ground vehicles have important military, reconnaissance, and materials handling application. Many of these applications require the UGVs to move at high speeds through uneven, natural terrain with various compositions and physical parameters. This paper presents a framework for high speed autonomous navigation based on the integrated real time traversability. Specifically, the proposed system performs real-time dynamic simulation and calculate maximum traversing velocity guaranteeing safe motion over rough terrain. The architecture of autonomous navigation is firstly presented for high-speed autonomous navigation. Then, the integrated real time traversability, which is composed of initial velocity profiling step, dynamic analysis step, road classification step and stable velocity profiling step, is introduced. Experimental results are presented that demonstrate the method for a $6{\times}6$ autonomous vehicle moving on flat terrain with bump.

• 제어로봇시스템학회논문지
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• 제14권6호
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• pp.608-614
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• 2008

This paper describes a location tracking system to guide landing process of an Unmanned Helicopter(UMH) exploiting MIT Cricket nodes. For automatic landing of a UMH, a precise positioning system is indispensable. However, GPS(Global Positioning System) is inadequate for tracking the three dimensional position of a UMH because of large positioning errors. The Cricket systems use Time-Difference-of-Arrival(TDoA) method with ultrasonic and RF(Radio Frequency) signals to measure distances. They operate in passive mode in that a listener attached to a moving device receives distance signals from several beacons located at fixed points on ground. Inevitably, this passive type of implementation causes large disturbances in measuring distances between beacons and the listener due to wind blow from propeller and turbulence of UMH body. To cope with this problem, we proposed active type of implementation for positioning a UMH. In this implementation, a beacon is set up at UMH body and four listeners are located at ground area at least where the UMH will land. A pair of Ultrasonic and RF signals from the beacon arrives at several listeners to calculate the position of the UMH. The distance signals among listeners are synchronized with a counter value appended to each distance signals from the beacon.

• 항공우주기술
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• 제3권1호
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• pp.9-15
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• 2004

본 논문에서는 무인비행선 비행제어시스템의 HILS(Hardware-In-the-Loop-Simulation) 시스템 개발 결과를 소개한다. HILS 시스템은 비행선 제어를 위해 설계된 비행제어컴퓨터의 지상시험을 위해 개발되었다. HILS 시스템을 구성하기 위해 각각 별도의 컴퓨터에서 작동하는 통신장비 모사 시스템, 탑재장치 모사 시스템, 비행선 운동 모사 시스템, 그리고 운동 가시화 시스템을 개발하였고, 이와 함께 3축 운동 시험대와 관성항법장치(Inertial Navigation Unit)도 포함하였다. 개발된 HILS 시스템을 이용한 단계적인 시험을 통해 비행 제어컴퓨터의 기능과 성능을 검증하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.579-582
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• 2008

PEM Fuel cell system was designed and constructed to use as a power source of unmanned aerial vehicles(UAV) in the present study. Sodium borohydride was selected as a hydrogen source and was decomposed by catalytic hydrolysis reaction. Fuel cell system consists of a fuel cell stack, a hydrogen generation system(HGS), and power management system(PMS). HGS was composed of a catalytic reactor, micropump, fuel cartridge, and separator. Hybrid power system between lithium-polymer battery and fuel cell was developed. The fuel cell system was integrated and packaged into a blended wing-body UAV. Energy density of the total system was 1,000 $W{\cdot}hr/kg$ and high endurance more than 5 hours was accomplished in the ground tests.

• 한국위성정보통신학회논문지
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• 제12권1호
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• pp.43-48
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• 2017

Recently, demands on civilian UAV (Unmanned Aerial Vehicle) has been increasing and appropriate communication system is required for the UAV. In this paper, the performance of the UAV communication system using commercial wireless mobile network is discussed. The main service area of the wireless mobile network is ground level however the flying range of the UAV is normally in high altitude. Because of this mismatch of service area the performance of the UAV communication system is degraded in high altitude. To compensate performance degradation of the UAV communications system in high altitude, adaptive array antenna is introduced which is able to overcome altitude limitation of the UAV communication system.