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- W4312309219 abstract "In this paper, first an overview and explanation of the lateral single-axis Oblique Active Tilting (l-sOAT) control structure is presented. A complete dynamic model of vertical take-off and landing (VTOL) unmanned aerial vehicles (UAVs) having longitudinal rotor tilting mechanism is developed using a Newton-Euler formulation for l-sOAT mechanism. Then, a theoretical analysis of l-sOAT vehicle control response and stability for pitch motion is described and simulated using the derived dynamic model. The validity of the proposed structure and its dynamic model is verified by simulation experiments." @default.
- W4312309219 created "2023-01-04" @default.
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- W4312309219 date "2022-02-01" @default.
- W4312309219 modified "2023-09-27" @default.
- W4312309219 title "A Dual-Fan Aircraft Use l-sOAT for Pitch control: Modelling and Simulation" @default.
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- W4312309219 doi "https://doi.org/10.1109/iscer55570.2022.00025" @default.
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