摘要
This paper proposes a kW-level Hardware-in-the-loop (HIL) testbed to validate the performance of the distributed electric propulsion system (DEPS) as part of the all-electric aircraft design. The aircraft's flight dynamics and left-wing onboard power grid are replicated using detailed models in a real-time simulator, while the operating characteristics of DEPS are studied using both controller HIL (C-HIL) and power HIL (P-HIL). Some flight tests have been conducted on the developed testbed for validation.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023 |
| 出版商 | Institute of Electrical and Electronics Engineers Inc. |
| 页 | 1876-1882 |
| 页数 | 7 |
| ISBN(电子版) | 9798350316445 |
| DOI | |
| 出版状态 | 已出版 - 2023 |
| 活动 | 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023 - Nashville, 美国 期限: 29 10月 2023 → 2 11月 2023 |
出版系列
| 姓名 | 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023 |
|---|
会议
| 会议 | 2023 IEEE Energy Conversion Congress and Exposition, ECCE 2023 |
|---|---|
| 国家/地区 | 美国 |
| 市 | Nashville |
| 时期 | 29/10/23 → 2/11/23 |
联合国可持续发展目标
此成果有助于实现下列可持续发展目标:
-
可持续发展目标 7 经济适用的清洁能源
学术指纹
探究 'Development of a Hardware-in-the-Loop Testbed for Distributed Electric Propulsion System in All-Electric Aircraft' 的科研主题。它们共同构成独一无二的学术指纹。引用此
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