A fault tolerant control for iced aircraft based on fixed-time incremental dynamic inversion with FTESO
Icing seriously affects the aerodynamic coefficients and flight performance of an aircraft. To address this problem, in this paper a fixed-time incremental nonlinear dynamic inversion(INDI) control method based on a fixed-time dilated state observer(FTESO) is proposed, and a flight controller for a...
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| Main Authors: | , , , , |
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| Format: | Article |
| Language: | zho |
| Published: |
EDP Sciences
2024-12-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2024/06/jnwpu2024426p996/jnwpu2024426p996.html |
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