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CEAS EuroGNC 2024 |
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Improving Pitch Capture for Aircraft Take-Off Rotation Law |
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Abstract: The paper describes the lastest improvements made within Airbus flight control laws for the rotation phase. It explains operational constraints such as delayed signals, non-linearities or limitations and proposes a way to answer to industrial needs. It proposes a way to gain in robustness and performance in case of weight on wheel signal delay by consolidating the ground to flight condition and robustify angle-of-attack signal. It changes anti-tail strike law structure to improve electronic tail bumper protection effectiveness. Non-linear effects are finally detailed and tackled. All the improvements allow a better pitch capture during rotation and therefore good aircraft performance. | ||||
Keywords: Aircraft Take-Off; Rotation Laws; Pitch capture; Non-linear compensations | ||||
Victor Gibert, Stéphane Delannoy: Improving Pitch Capture for Aircraft Take-Off Rotation Law. Proceedings of the 2024 CEAS EuroGNC conference. Bristol, UK. June 2024. CEAS-GNC-2024-068. |
BibTeX entry: @Incollection{CEAS-GNC-2024-068, author = {Gibert, Victor and Delannoy, Stéphane}, title = {Improving Pitch Capture for Aircraft Take-Off Rotation Law}, booktitle = {Proceedings of the 2024 {CEAS EuroGNC} conference}, address = {Bristol, UK}, month = jun, year = {2024}, note = {CEAS-GNC-2024-068} } |