Aeroservoelastic analysis method for mixed-command fault of flight control system
Large civil aircraft fly-by-wire flight control systems may experience a fault condition where both normal mode and direct mode control commands are output simultaneously. It is necessary to propose a method to demonstrate the airworthiness compliance of the aircraft’s aeroservoelasticity under this...
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| Principais autores: | , , |
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| 格式: | Artigo |
| 語言: | Chinês |
| 出版: |
Editorial Department of Advances in Aeronautical Science and Engineering
2025-12-01
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| 叢編: | Hangkong gongcheng jinzhan |
| 主題: | |
| 在線閱讀: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2025037 |
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