2018
DOI: 10.1002/asjc.1981
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Fuzzy adaptive nonlinear sensor‐fault tolerant control for a quadrotor unmanned aerial vehicle

Abstract: In this paper, a novel fuzzy adaptive nonlinear fault tolerant control design scheme is proposed for attitude dynamics of quadrotor UAV subjected to four sensor faults (bias, drift, loss of accuracy, loss of effectiveness). The sensor faults in Euler angle loop are transformed equivalently into a mismatched uncertainty vector, and other unknown items involving faults, uncertain parameters and external disturbances in angular velocity loop are lumped into an unknown nonlinear function vector.Fuzzy logic systems… Show more

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Cited by 19 publications
(20 citation statements)
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“…Assumption 1. (see [40]). For the sensor fault D, there exist corresponding inequality conditions ‖D‖ ≤ τ 0 , ‖ _ D‖ ≤ τ 1 , and…”
Section: Problem Descriptionmentioning
confidence: 96%
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“…Assumption 1. (see [40]). For the sensor fault D, there exist corresponding inequality conditions ‖D‖ ≤ τ 0 , ‖ _ D‖ ≤ τ 1 , and…”
Section: Problem Descriptionmentioning
confidence: 96%
“…We assume that accuracy losses of the airspeed head sensor and the optical camera sensor are considered in this study. e loss of accuracy of two sensors is given as follows [40]:…”
Section: Problem Descriptionmentioning
confidence: 99%
See 1 more Smart Citation
“…Although adaptive fuzzy or backstepping control has become one of the most important design approaches for nonlinear systems without satisfying matching conditions, it has achieved many important results [14]. However, the existing adaptive fuzzy or backstepping controller focuses on nonlinear uncertain systems, which cannot be applied to nonlinear uncertain systems with unmatched disturbances [15].…”
Section: ------------------------------------------------------------mentioning
confidence: 99%
“…The design is based on a control signal combination generated by a set of linear quadratic state feedback controllers. A fuzzy adaptive nonlinear FTC scheme [6] is proposed for attitude dynamics of a quadrotor affected with several sensor faults such as bias, drift, loss of accuracy, and loss of effectiveness. Regarding a FTC for a 3‐DOF helicopter, the stabilization problem considering actuator faults is addressed in [7], by means of the H ∞ methodology.…”
Section: Introductionmentioning
confidence: 99%