2022
DOI: 10.1155/2022/2812671
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Design of a Fixed-Wing UAV Controller Combined Fuzzy Adaptive Method and Sliding Mode Control

Abstract: To overcome the complexity of the coupled nonlinear model of a fixed-wing UAV system and the uncertainty caused by a large number of interference factors, a control algorithm combining fuzzy adaptive control and sliding mode variable structure control was proposed. The controller algorithm mainly relies on the sliding mode variable structure control method to solve the control problem of the strongly coupled complex nonlinear system. Based on sliding mode control, a fuzzy adaptive method is introduced to reduc… Show more

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Cited by 6 publications
(3 citation statements)
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“…Other authors have studied adaptive control theory to propose solutions to achieve a stable flight with fixed-wing UAVs; for example, in [1], an adaptive controller based on fuzzy logic and sliding mode control (SMC) is designed, ref. [1] used fuzzy logic to reduce the chattering in the SMC and used the SMC methodology to approximate the uncertain parameters and unknown functions caused by the external perturbations or disturbances. Two types of fuzzy adaptive SMC for different fuzzy ranges are proposed.…”
Section: Introductionmentioning
confidence: 99%
“…Other authors have studied adaptive control theory to propose solutions to achieve a stable flight with fixed-wing UAVs; for example, in [1], an adaptive controller based on fuzzy logic and sliding mode control (SMC) is designed, ref. [1] used fuzzy logic to reduce the chattering in the SMC and used the SMC methodology to approximate the uncertain parameters and unknown functions caused by the external perturbations or disturbances. Two types of fuzzy adaptive SMC for different fuzzy ranges are proposed.…”
Section: Introductionmentioning
confidence: 99%
“…Many nonlinear and linear controls have therefore been established given these circumstances. For instance, adaptive control [4][5][6], backstepping control [7,8], sliding mode control [9][10][11][12][13][14], optimal control [15,16] and intelligent control [17][18][19][20][21] have been deployed.…”
Section: Introductionmentioning
confidence: 99%
“…For the stability of tri-motor UAV, this model reference adaptive control (MRAC) is utilized, which shows this algorithm has better transient performance with zero steady-state and fast convergence towards stability. To overcome the complexity of a coupled nonlinear model of a fixed-wing UAV system, [20] proposed a control algorithm combining fuzzy adaptive control and sliding mode variable structure control. The stability of the controllers was verified using the Lyapunov stability theorem.…”
Section: Introductionmentioning
confidence: 99%