• 한국항공운항학회지
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• 제16권4호
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• pp.1-11
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• 2008

This research presents a study for the knowledge-based configuration design development of a RC (remote control) helicopter. Parametric design and knowledge based design concepts are introduced for rapid design changes and analyses using commercial CAD software, CATIA(R) Knowledgeware module. It is crucial for RC helicopter design because it enables rapid conceptual design through instant configuration changes. Positions and dimensions of RC helicopter parts were used as design parameters. As an example, positions of CG(center of gravity) points were traced and plotted as the configuration changes. Further research should be performed in areas of user interfaces and web-based multi-user environments instead of using Excel data sheets.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2005년도 ICCAS
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• pp.1863-1866
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• 2005

In this paper we propose a platform that is applicable to low altitude remote sensing. Basic idea of the platform is based on the model helicopter. On big difference from the conventional model helicopter is that our platform has four main rotors. Furthermore, vision control strategy is introduced so that operator can use the platform without any specialized intensive knowledge

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 1998년도 추계종합학술대회 논문집
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• pp.743-746
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• 1998

In this paper, we developed an outdoor augmented reality system which has remote real scences acquisition ability. The real scenes acquisition system consists of image acquisition system, tracking system, wireless data transceiver and power supply. Tracking system that consists of Tans Vector and RT-20 measures a position and attitude of the CCD camera that attached at the remote control helicopter. Wireless data transceiver system is utilized for data transmission of remote system that of attitude, position information, andreal scenes data that acquired by the CCD camera. Maximum propelling power of remote control helicopter is 15Kg, so we used 7.2V li-ion cell as a power supply for system minimize. As the results of experiment, the developing system presented application possibility of remote information acquisition system such as construction simulation & estimation, broadcasting, tour guide.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2000년도 하계종합학술대회 논문집(3)
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• pp.153-156
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• 2000

In this paper, we developed an outdoor augmented reality system which has remote real scenes acquisition ability. The real scenes acquisition system consists of Image acquisition system, tracking system, wireless data transceiver and power supply. The tracking system consists of Tans Vector and RT-20 which measures a position and attitude of the CCD camera that attached to the remote control helicopter. Wireless data transceiver system is utilized for data transmission of remote system that of attitude, position information, and real scenes data that acquired by the CCD camera. Maximum propelling power of remote control helicopter is 15Kg, so we used 7.2V li-ion cell as a power supply for system minimize. As the results of experiment, the developing system presented application possibility of remote information acquisition system such as construction simulation & estimation, broadcasting, tour guide.

• 한국항공운항학회지
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• 제14권1호
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• pp.63-69
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• 2006

The operational environment of helicopters extends from the civil air traffic control system to remote and hazardous areas and from day operations under visual flight conditions to night operations in adverse weather. Helicopters can move in any direction, remain stationary while airborne, climb and descend vertically, and take off and land almost anywhere. Thus their range of maneuvers and control requirements vary more widely than do those of fixed-wing aircraft. In this study, I analyzed the job of helicopter pilot through methods of observation, and classified the required ability of them into the domain of cognitive, perceptual/spatial, psychomotor. I expect that the result of this study will be used to aid training and selection of helicopter pilot.

• 한국항공우주학회지
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• 제49권4호
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• pp.329-334
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• 2021

대한항공은 유인 헬리콥터를 무인화 후 원격 조종으로 제자리 비행을 수행하는 것을 무인 헬리콥터 개발의 1단계 목표로 수립하였다. 개발 목표를 달성하기 위해 대한항공은 유인기의 창급정비와 기체 개조 수행 후 체계통합, 지상시험, 안전줄 시험을 순차적으로 수행하며 단계별로 무인 헬리콥터 체계의 조종성과 비행안전성을 검증하였다. 특히 검증의 마지막 단계에서 사용한 안전줄시험 기법은 완전무인화된 무인 헬리콥터 체계에 대해 비행안전성과 조종성을 검증할 수 있는 유효한 방법임을 확인하였다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2002년도 Proceedings of International Symposium on Remote Sensing
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• pp.746-749
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• 2002

This paper is introducing a radio control helicopter as a new platform of ground truth measurement. This helicopter is normally used for spraying an agricultural chemical. It can do pinpoint hovering and programing flight using DGPS etc., A spectrometer with dual port can measure ground surface and white reference plate at the same time. And it can also take digital images by digital camera. It is needed to collect ground reflectance information as satellite sensor footprint size for satellite data validation. Generally it is possible to get such ground reflectance by an airplane measurement. But it is high cost and not so easy to make a measurement by airplane. Developed validation system can provide such ground reflectance in low cost and easy.

• 한국지능시스템학회논문지
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• 제25권4호
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• pp.398-404
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• 2015

본 논문에서는 관성측정장치를 기반으로 블루투스 환경에서의 자율비행을 위한 멀티 로터형 헬리콥터에 대한 설계 및 성능을 제시하였다. 멀티 로터관련 다양한 연구가 진행되어오고 있긴 하지만 최근에는 다양한 서비스를 목적으로 짐벌이 장착된 헥사로터형의 헬리콥터에 대한 관심이 모아지고 있다. 따라서, 본 논문에서는 지상의 원격조정 PC나 고성능의 원격제어장치나 영상시스템과 같은 외부보조 시스템 없이 연구와 구조활동, 모니터링 활동을 수행할 수 있는 컴팩트하고 자율비행을 위한 헥사로터(hexa rotor)형 헬리콥터에 대한 하드웨어 및 소프트웨어를 소개하고자 한다. 제안한 시스템은 헥사로터 헬리콥터의 구조와 관성측정장치 관련 하드웨어 구성과 수학적 모델링 및 시뮬레이션 결과를 각각 제시하였다. 또한, IMU 구현을 위하여 MCU(ARM-cortex) 보드를 장착하여 각 로터의 회전과 관성 측정장치의 입력신호에 대한 상태를 제어할 수 있도록 하였다. 그리고 시스템 시뮬레이션과 실험을 통한 시스템의 성능을 각각 검증하였다.

• 한국지리정보학회지
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• 제10권2호
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• pp.82-90
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• 2007

최근 무분별한 개발로 인한 산림지역의 훼손으로 토양의 침식이 발생하고 이는 강우와 결부되어 하천 오염 및 하천의 바닥고를 상승시켜 통수능을 저하시키는 원인이 되기도 한다. 이를 위해 국내에서는 환경영향평가 및 재해영향평가를 통하여 토사유출의 정량적 분석을 실시하여 적절한 대책을 수립하도록 하고 있다. 토사유출량 산정 시 고려되는 매개변수 중 본 연구에서는 무선조종 헬기 통하여 취득한 영상 정보를 이용하여 절취사면의 사면경사계수(LS) 및 토양피복계수(C)를 영상분석을 이용하여 보다 정확한 값을 산정하였다.

• 제어로봇시스템학회논문지
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• 제13권1호
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• pp.58-64
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• 2007

In this paper, the stabilization problem of the image stabilization system(ISS) that captures the image of an object on the ground by remote sensing is considered. The ISS should be stable under outer disturbance such as helicopter vibration for tracking line of sight. Although PID controllers are optimized for the system, disturbances cause the instability of the system. To minimize the effect of the disturbance, the time-delayed control method is used to compensate for uncertainties. Simulation studies are performed and experiments are conducted to confirm the simulation results. Performances of PID control and time-delayed control methods are compared.