Analysis of the influence of transition state control strategy on structural load of quad-tiltrotor
There are complex structural load changes in the rotor during the tilt-transition of quad-tiltrotor aircraft,which can directly affect the life of the rotor. The control strategy analysis is beneficial to reveal the influence law of the rotor structural load, which can provide a conclusion basis for...
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| Main Authors: | HE Yongtao, ZHANG Xiayang, WANG Xin, ZHENG Lixiong |
|---|---|
| Format: | Article |
| Language: | zho |
| Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2025-06-01
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| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2024227 |
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