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• W3148223506 abstract "Research and development have been very active in electric vertical takeoff and landing (eVTOL) aircraft. Tilt-Wing aircraft especially receive significant attention as one of the most efficient configurations; however, they are apt to be unstable during the transition from hover to cruise. The angle of attack (AoA) is a critical parameter for aircraft motion, and with its real-time data, Tilt-Wing aircraft would achieve a more robust transition. Conventional methods of obtaining AoA require either additional sensors or an aircraft model, which is not robust to propeller slipstreams and unsuitable for Tilt-Wing aircraft. In this paper, a new AoA estimation method for Tilt-Wing aircraft is proposed. The proposed method is based on the propeller dynamics model and requires only an existing pitot tube. Wind tunnel tests verify its effectiveness." @default.
• W3148223506 created "2021-04-13" @default.
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• W3148223506 date "2021-03-07" @default.
• W3148223506 modified "2023-10-02" @default.
• W3148223506 title "Observer-based Angle of Attack Estimation for Tilt-Wing eVTOL Aircraft" @default.
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• W3148223506 doi "https://doi.org/10.1109/icm46511.2021.9385670" @default.
• W3148223506 hasPublicationYear "2021" @default.
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