2022
DOI: 10.1007/s40815-022-01361-5
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Fuzzy Approximation-Based Adaptive Finite-Time Tracking Control for a Quadrotor UAV with Actuator Faults

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Cited by 11 publications
(1 citation statement)
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“…Compared with the nonlinear calculation, the linearization method is used to calculate the effect of thrust vector increment [16]. Furthermore, the sliding mode control [17], the active disturbance rejection control [18] and the fuzzy control [19] are often used as control algorithms for quadrotor UAV. A dynamic surface-active disturbance rejection control strategy is proposed by Zhang, in which a first-order filter is introduced to obtain the derivative of the virtual control and simplifies the control law of the system.…”
Section: Introductionmentioning
confidence: 99%
“…Compared with the nonlinear calculation, the linearization method is used to calculate the effect of thrust vector increment [16]. Furthermore, the sliding mode control [17], the active disturbance rejection control [18] and the fuzzy control [19] are often used as control algorithms for quadrotor UAV. A dynamic surface-active disturbance rejection control strategy is proposed by Zhang, in which a first-order filter is introduced to obtain the derivative of the virtual control and simplifies the control law of the system.…”
Section: Introductionmentioning
confidence: 99%