A Hinge Moment Alleviation Control Strategy for Morphing Tail Aircraft Based on a Data-Driven Method
Morphing airplane technology is currently a focal point of research. For morphing airplanes, besides effective morphing strategies and control schemes, the hinge moment at the root of the vertical tail during morphing is a critical factor influencing flight safety. To prevent failure in tail morphin...
| 出版年: | Actuators |
|---|---|
| 主要な著者: | , |
| フォーマット: | 論文 |
| 言語: | 英語 |
| 出版事項: |
MDPI AG
2024-09-01
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| 主題: | |
| オンライン･アクセス: | https://www.mdpi.com/2076-0825/13/9/369 |