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- W3190496797 abstract "An energy reduction strategy for a fixed-wing drone with classic configuration is presented in this paper. The strategy is developed using the longitudinal non-linear motion equations of the aircraft, considering the stall effects in the determination of lift and drag forces. Our strategy imposes the aircraft to track a special trajectory allowing the vehicle to perform a curve in ascend, acting against the gravity force. As a consequence of this tracking, the angle of attack of the vehicle is increased arriving to critical values that need to be compensated for avoiding the crash of the vehicle. Therefore, a strategy to avoid the stall stage and recovering the flight stability in the vehicle is proposed. The strategy is evaluated in simulations for validating the performance of the whole system." @default.
- W3190496797 created "2021-08-16" @default.
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- W3190496797 date "2021-06-15" @default.
- W3190496797 modified "2023-10-18" @default.
- W3190496797 title "Least Airspeed Reduction Strategy & Flight Recuperation of a Fixed-Wing Drone" @default.
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- W3190496797 doi "https://doi.org/10.1109/icuas51884.2021.9476680" @default.
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