Fault-Tolerant Control of a Variable-Pitch Quadrotor under Actuator Loss of Effectiveness and Wind Perturbations

The actuator fault-tolerant control problem for a variable-pitch quadrotor is addressed under uncertain conditions. Following a model-based approach, the plant nonlinear dynamics are faced with a disturbance observer-based control and a sequential quadratic programming control allocation, where only...

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Published inSensors (Basel, Switzerland) Vol. 23; no. 10; p. 4907
Main Authors Baldini, Alessandro, Felicetti, Riccardo, Freddi, Alessandro, Monteriù, Andrea
Format Journal Article
LanguageEnglish
Published Switzerland MDPI AG 19.05.2023
MDPI
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ISSN1424-8220
1424-8220
DOI10.3390/s23104907

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Abstract The actuator fault-tolerant control problem for a variable-pitch quadrotor is addressed under uncertain conditions. Following a model-based approach, the plant nonlinear dynamics are faced with a disturbance observer-based control and a sequential quadratic programming control allocation, where only kinematic data of the onboard inertial measurement unit are required for the fault-tolerant control, i.e., it does not require the measurement of the motor speed nor the current drawn by the actuators. In the case of almost horizontal wind, a single observer handles both faults and the external disturbance. The estimation of the wind is fed forward by the controller, while the actuator fault estimation is exploited in the control allocation layer, which copes with the variable-pitch nonlinear dynamics, thrust saturation, and rate limits. Numerical simulations in the presence of measurement noise show the capability of the scheme to handle multiple actuator faults in a windy environment.
AbstractList The actuator fault-tolerant control problem for a variable-pitch quadrotor is addressed under uncertain conditions. Following a model-based approach, the plant nonlinear dynamics are faced with a disturbance observer-based control and a sequential quadratic programming control allocation, where only kinematic data of the onboard inertial measurement unit are required for the fault-tolerant control, i.e., it does not require the measurement of the motor speed nor the current drawn by the actuators. In the case of almost horizontal wind, a single observer handles both faults and the external disturbance. The estimation of the wind is fed forward by the controller, while the actuator fault estimation is exploited in the control allocation layer, which copes with the variable-pitch nonlinear dynamics, thrust saturation, and rate limits. Numerical simulations in the presence of measurement noise show the capability of the scheme to handle multiple actuator faults in a windy environment.
The actuator fault-tolerant control problem for a variable-pitch quadrotor is addressed under uncertain conditions. Following a model-based approach, the plant nonlinear dynamics are faced with a disturbance observer-based control and a sequential quadratic programming control allocation, where only kinematic data of the onboard inertial measurement unit are required for the fault-tolerant control, i.e., it does not require the measurement of the motor speed nor the current drawn by the actuators. In the case of almost horizontal wind, a single observer handles both faults and the external disturbance. The estimation of the wind is fed forward by the controller, while the actuator fault estimation is exploited in the control allocation layer, which copes with the variable-pitch nonlinear dynamics, thrust saturation, and rate limits. Numerical simulations in the presence of measurement noise show the capability of the scheme to handle multiple actuator faults in a windy environment.The actuator fault-tolerant control problem for a variable-pitch quadrotor is addressed under uncertain conditions. Following a model-based approach, the plant nonlinear dynamics are faced with a disturbance observer-based control and a sequential quadratic programming control allocation, where only kinematic data of the onboard inertial measurement unit are required for the fault-tolerant control, i.e., it does not require the measurement of the motor speed nor the current drawn by the actuators. In the case of almost horizontal wind, a single observer handles both faults and the external disturbance. The estimation of the wind is fed forward by the controller, while the actuator fault estimation is exploited in the control allocation layer, which copes with the variable-pitch nonlinear dynamics, thrust saturation, and rate limits. Numerical simulations in the presence of measurement noise show the capability of the scheme to handle multiple actuator faults in a windy environment.
Audience Academic
Author Baldini, Alessandro
Monteriù, Andrea
Felicetti, Riccardo
Freddi, Alessandro
AuthorAffiliation Department of Information Engineering, Università Politecnica delle Marche, 60131 Ancona, Italy; a.baldini@univpm.it (A.B.); r.felicetti@univpm.it (R.F.); a.monteriu@univpm.it (A.M.)
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Keywords variable-pitch quadrotors
fault diagnosis
fault-tolerant control
loss of effectiveness
disturbance observer-based control
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Snippet The actuator fault-tolerant control problem for a variable-pitch quadrotor is addressed under uncertain conditions. Following a model-based approach, the plant...
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StartPage 4907
SubjectTerms Actuators
Algorithms
Analysis
Coordinate transformations
disturbance observer-based control
Energy consumption
Fault diagnosis
Fault tolerance
fault-tolerant control
Kinematics
loss of effectiveness
Mathematical models
Numerical analysis
Unmanned aerial vehicles
variable-pitch quadrotors
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Title Fault-Tolerant Control of a Variable-Pitch Quadrotor under Actuator Loss of Effectiveness and Wind Perturbations
URI https://www.ncbi.nlm.nih.gov/pubmed/37430820
https://www.proquest.com/docview/2819483346
https://www.proquest.com/docview/2836877736
https://pubmed.ncbi.nlm.nih.gov/PMC10221893
https://doaj.org/article/87ed6c4819db407397b5e59949a4bd77
Volume 23
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