2021 5th International Symposium on Multidisciplinary Studies and Innovative Technologies (ISMSIT) 2021
DOI: 10.1109/ismsit52890.2021.9604685
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Nonlinear Modeling and Robust Control of a Quadrotor UAV under Uncertain Parameters and White Gaussian Noise

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Cited by 7 publications
(1 citation statement)
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“…The helicopter is a typical single-rotor UAV, which counteracts the main rotor torque with the torque generated by the tail rotor. The four-rotor aircraft controls the lift and torque acting on the airframe by relying on the different rotational speeds of the four rotors to control the movement of the four rotors and simultaneously realizes the role of the balancing torque (Jun et al, 2018;Karahan et al, 2021). Given this feature, the four-rotor aircraft is more accessible to achieve the goal of miniaturization and is more lightweight than the helicopter.…”
Section: Principle Of Motion Of the Quadrotor Uavmentioning
confidence: 99%
“…The helicopter is a typical single-rotor UAV, which counteracts the main rotor torque with the torque generated by the tail rotor. The four-rotor aircraft controls the lift and torque acting on the airframe by relying on the different rotational speeds of the four rotors to control the movement of the four rotors and simultaneously realizes the role of the balancing torque (Jun et al, 2018;Karahan et al, 2021). Given this feature, the four-rotor aircraft is more accessible to achieve the goal of miniaturization and is more lightweight than the helicopter.…”
Section: Principle Of Motion Of the Quadrotor Uavmentioning
confidence: 99%