• 디지털정책학회지
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• 제1권2호
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• pp.47-52
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• 2022

드론 비행의 위치 인식에 있어 GPS 신호의 절대적 의존성, 비행 안정성, 배터리 한계로 인한 비행시간 문제는 드론 산업 발전의 큰 제약이 되고 있다. 특히 20분 내외의 짧은 임무 비행시간은 드론 활용에 있어 큰 걸림돌이 되고 있으며, 이를 극복하기 위해 액체수소를 에너지원으로 이용한 드론개발이 활발히 진행되고 있다. 하지만 액체수소 드론개발의 속도보다 현재의 규제 및 인증 제도 개정의 속도가 더뎌 개발 드론의 시험, 인증, 상용화에 어려움을 겪고 있으며, 이는 결국 드론 시장 선점의 문제점이 되고 있다. 본 논문에서는 수소 에너지 기반 드론개발 동향을 분석하며 규제와 인증 제도의 한계점을 소개하고 해결방안을 간략히 제시한다.

• 한국수소및신에너지학회논문집
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• 제32권6호
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• pp.542-550
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• 2021

As the application of multirotor grows, the demands for multirotor that can fly longer and load more are increasing. Hydrogen has a high energy density, so it can satisfy these demands when used in multirotor. In order to design hydrogen fueled multirotor that satisfies the desired flight time and payload, it is important to calculate the specifications of a fuel cell, battery, and hydrogen storage system. This paper contains detailed information on various energy systems used in multirotor and fuel cell powered multirotor research trends. This study proposed a sizing calculation method that meets the target flight time and payload using thrust and power equations. It has been explained how the two equations derive the particular specifications. The specifications of the multirotor were derived by assuming a payload of 50 kg and a flight time of 1 hour. In addition, the effects of the values of the fuel cell, hydrogen storage system, and motor propeller were analyzed.

• 한국수소및신에너지학회논문집
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• 제34권6호
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• pp.758-766
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• 2023

Multi-copter of unmanned aerial vehicle (UAV) was initially developed as strategic technology in the only military field, but it is developing into an industrial field with a wide range of applications in the civil sector based on the development and convergence of aviation technology and information and communication technology. Currently, the degree of utilization of multi-copter is increasing in various industries for the purpose of performing classic tactical missions, logistics transportation, farm management, internet supply, video filming, weather management, life-saving, etc, and active technology development responding to market demand. Existing commercial multi-copter mainly use an electric energy propulsion system consisting of an electric battery and a brushless direct current (BLDC) motor. It is the limitations for usage in the flying time (up to 20 minutes) and payload (less than 20 kg). this study aims to overcome these limitations and expand the commercialization of engine-powered multi-copter of UAV in various industries in the futures.