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성층권 드론에 적용할 멀티레벨 인버터 회로 분석 및 경량화 분석
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | 황광복 | - |
| dc.contributor.author | 박희문 | - |
| dc.contributor.author | 전향식 | - |
| dc.contributor.author | 이정환 | - |
| dc.contributor.author | 박진현 | - |
| dc.date.accessioned | 2023-11-13T07:42:01Z | - |
| dc.date.available | 2023-11-13T07:42:01Z | - |
| dc.date.issued | 2023-10 | - |
| dc.identifier.issn | 1226-833x | - |
| dc.identifier.issn | 2765-5415 | - |
| dc.identifier.uri | https://scholarworks.gnu.ac.kr/handle/sw.gnu/68450 | - |
| dc.description.abstract | The stratospheric drones are developed to perform missions such as weather observation, communication relay, surveillance, and reconnaissance at 18km to 20km, where climate change is minimal and there is no worry about a collision with aircraft. It uses solar panels for daytime flights and energy stored in batteries for night flights, providing many advantages over existing satellites. The electrical and power systems essential for stratospheric drone flight must ensure reliability, efficiency, and lightness by selecting the optimal circuit topology. Therefore, it is necessary to analyze the circuit topology of various types of multi-level inverters with high redundancy that can ensure the reliability and efficiency of the motor driving power required for stable long-term flight of stratospheric drones. By quantifying the switch element voltage drop and the number and weight of inverter components for each topology, we evaluate efficiency and lightness and propose the most suitable circuit topology for stratospheric drones. | - |
| dc.format.extent | 13 | - |
| dc.language | 한국어 | - |
| dc.language.iso | KOR | - |
| dc.publisher | 한국산업융합학회 | - |
| dc.title | 성층권 드론에 적용할 멀티레벨 인버터 회로 분석 및 경량화 분석 | - |
| dc.title.alternative | Multi-Level Inverter Circuit Analysis and Weight Reduction Analysis to Stratospheric Drones | - |
| dc.type | Article | - |
| dc.publisher.location | 대한민국 | - |
| dc.identifier.bibliographicCitation | 한국산업융합학회논문집, v.26, no.5, pp 953 - 965 | - |
| dc.citation.title | 한국산업융합학회논문집 | - |
| dc.citation.volume | 26 | - |
| dc.citation.number | 5 | - |
| dc.citation.startPage | 953 | - |
| dc.citation.endPage | 965 | - |
| dc.identifier.kciid | ART003010262 | - |
| dc.description.isOpenAccess | N | - |
| dc.description.journalRegisteredClass | kci | - |
| dc.subject.keywordAuthor | Stratospheric drone | - |
| dc.subject.keywordAuthor | CHC(Cascaded H-bridge Circuit) | - |
| dc.subject.keywordAuthor | FCC(Flying Capacitor Circuit) | - |
| dc.subject.keywordAuthor | DCC(Diode Clamped Circuit) | - |
| dc.subject.keywordAuthor | ANPC(Active Neutral Point Clamped) | - |
| dc.subject.keywordAuthor | TNPC(T-type Neutral Point Clamped) | - |
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