Suppression of falling leaf mode phenomenon for F/A - 18 via L1 adaptive feedback controller
F / A - 18 Hornet aircraft is prone to nonlinear phenomenon known as the fulling leaf mode, which when operating at deep stall is often combined with large side slip and yaw motion resuhs in significant rotation. The resuhant rotation triggers the aircraft to lose ahitude at a very fuster rate. T...
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| 格式: | Theses and Dissertations |
| 語言: | English |
| 出版: |
2017
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| 在線閱讀: | http://hdl.handle.net/10356/72702 |
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