2022
DOI: 10.3390/drones6090229
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Fractional-Order Linear Active Disturbance Rejection Control Design and Optimization Based Improved Sparrow Search Algorithm for Quadrotor UAV with System Uncertainties and External Disturbance

Abstract: This paper presents a generic robust controller that allows applications in various quadrotor unmanned aerial vehicle (UAV) systems effectively even when facing severe system uncertainties and unknown external disturbances. The fractional-order linear active disturbance rejection control (FOLADRC) scheme has combined the advantages of the fractional-order PID (FOPID) with the linear active disturbance rejection control (LADRC). Firstly, the structure of the FOLADRC-based quadrotor UAV is designed. Then, consid… Show more

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Cited by 15 publications
(2 citation statements)
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“…Many existing observers have been previously reported in the literature [14,15,21] for the FJR system. Furthermore, the extended state observer (ESO) has been proven as being a promising observer tool in the active disturbance rejection control techniques for estimating states and disturbance, which have been applied for different systems such as drones [23,24]. However, the estimation error of the states and disturbances in the above observer works can only approach to zero asymptotically and slowly, and they are sensitive to the initial conditions.…”
Section: Introductionmentioning
confidence: 99%
“…Many existing observers have been previously reported in the literature [14,15,21] for the FJR system. Furthermore, the extended state observer (ESO) has been proven as being a promising observer tool in the active disturbance rejection control techniques for estimating states and disturbance, which have been applied for different systems such as drones [23,24]. However, the estimation error of the states and disturbances in the above observer works can only approach to zero asymptotically and slowly, and they are sensitive to the initial conditions.…”
Section: Introductionmentioning
confidence: 99%
“…Under the strong external disturbance, the UAV cannot maintain the desired attitude, which often leads to the failure of the mission. This requires its control system to have strong robustness and anti-interference ability [13].…”
Section: Introductionmentioning
confidence: 99%